18/952,324

 

OES ENGINE 2

Patent 18/ 952,324

A continuation of patent 18/944,161

Both are:  /JAMES FRANK OSTERBUR/ inventor-owner

 

 

 

abstract:

this is the architecture, continuation: for the basic industrial engine design 18/952,324; expected; to be used in electrical generation. Originating patent is Patent #18/944,161      confirmation #4057       

its originating illustration is a modeling design, consistent with the originating OES engine, created for understanding this purpose. But without the architecture of distinguishing drawings; the patent is considered to be critically supported in an environment where any tiny change is considered to be an alternate invention; regardless of how similar it is. Modeling allows for experimentation of the design, without the investment of major funding.

Application # missing parts: confirmation number 5133  to correct the required brief descriptions and subsequent proper substitute specifications required is presented. An illustration further defining the purposes of this patent are used. Originating drawings are returned; with better descriptions detailed in the specs. (a suitable drafting professional was sought/ but failed to appear).  You have not provided a response written by mail or email of any kind/ you have failed to inform, confirm, or acknowledge;  that my registration as you required by mail was received. Including oaths for both patents along with  micro entity status. You did not resent proper billing as you are required to do: it is your job/ not mine. You did not return the postcard used to provide increased spacing in patent 18/944,161; confirmation number 4057. Nor acknowledge the other forms, which were notarized and  sent with US certified mail 9589 0710 5270 0593 6225 94. Even though you did send a customer number 203442 back to me; which proves you received the material/ as that request was within it. Your staff claimed the cost would be $364 dollars/ and you failed that, and presented over $8000.00 instead. You did not create the means to provide you with an oath, micro entity or other on your electronic website. You did not allow me to use that site again; stating I had to mail you for registration. You created failed in the documentation originating as the language used did not indicate line spacing was the only problem on 18/944,161. Which is the only cause for mailing;  consequently, the maze of failure you instigated exists. But not due to me.  Correct your elements of business, and I will provide you with a new drawing. I will remind you that having collected over $2,000 for 18,944,161 you are considered guilty of “grand theft”/ should you elect to claim it is abandoned; and various forms of media will be involved. As the criminal intent begins to conceive of:  “let’s steal it”/ and sell it to another.  Which can only mean:  there are others in higher positions involved.

18/952,324

Confirmation #

5133

Patent center #

68024057

Received

11/19/2024 3:05:37

Should another form or other be required for the continuation of patent:  I REQUIRE YOU; TO SEND IT, TO ME.  YOU DO have my address and more.

            My job is as the inventor!  YOUR JOB IS TO FACILITATE THAT, WITH ALL REALISTIC PURPOSES.  NOT HINDER IT; WITH MAZES AND FAILURES AND BETRAYAL BY CLAIMS OF POWER.  You are again reminded:  this is my property not yours. YOUR JOB is to functionally provide what I need in order to provide for humanity what they need; with realistic haste.  Your claim is 18 months before you get to it/ therefore my claim is:  I will change it as I desire:  until that time arrives. YOUR JOB, is to date those changes; as I file them.

 

BACKGROUND:

to establish the fundamentals, rather than the mechanical disciplines needed to align the basic parts into a common use machine. Therefore, attention to detail is considered to be of limited value. While the basic compilation of parts; is granted a value which would otherwise be considered obvious. Limited complexity is used so the majority will not get lost.

the critical question is: if the design intent will be lost without a specific type of illustration, needed for design instruction. That being the basic design is expected to be roughly fifty cylinders (dependent upon size_) around the same rotating wheel valving system; to produce roughly 12,000 horsepower, which can be manipulated, through the various stages of: disconnecting individual cylinders through clutching of some sort; to reduce that down to 1000 hp for less need usage; if desired.

SUMMARY:

to construct what is ultimately the starting stepping stones, for basic conceptions; so that all can be certain this is what was intended for this particular function, in this particular way. Whereas other versions of this OES engine remain untouched, and are as they are described.

The reconstruction required by the patent office of the drawing sent; which were construed to be: as a method of testing the understanding.

Are functionally abandoned; as to the actual purpose of full-scale electrical generation. That drawing “OES industrial; electric generation” by /James Frank Osterbur/; is now, sent as its replacement.

The complexity of the functioning development of this machine is fundamental, and requires significant engineering to attain the critical realities needed. NO SUCH THING is required of the inventor-owner. Therefore, attention to significant detail is abandoned; and the basic illustration layout of the machine is offered as my only “engineering detail”; to aid in your work.

 

 

 

 

 

 

 

OES ENGINE 2 /JAMES FRANK OSTERBUR/ inventor-owner

patent 18/952,324 a continuation of patent 18/944,161

 

SPECIFICATIONS and claims: are enlarged from the originating 4 cycle model, primarily intended for experimentation. To include illustration of the new OES industrial electrical generation 2-cycle engine

SPECIFICIATIONS: for the industrial design of this drawing; defined by, electrical generation, follow beneath.  

The “pet/ climate” forum created by government; to enlarge “green house alternative machines”; is abandoned. Elements of tying the claims together are abandoned; and further claims specific to this design function are added. As is my right to do.

the foundation for this invention is to further identify the basic architecture of larger than possible engines of this time. Machines capable of greatly increased horsepower require specialized, structural design work. Floor mounting/ ring structure suspension/ and so on. Machines that include “once it starts/ it will not be stopped”; unless something breaks. Machines that must be confined to realistic space limits. Are all versions of a secondary elevation; which allows the drafting of distinct conceptions. Which includes how we use the combustion gases to control that speed of process. With various vanes which can be manipulated to achieve both higher and lower speeds of rotary wheel valving.

WE BEGIN with the top view drawing; of a 4-cycle machine: which identifies the basic layout of the machine for electrical generation. This machine sets out as a horizontal conception, and is anchored to the floor by the one of four lower-level structural members #11 which contain its movement with upper cross beams #10 for holding the basic machine in place. The upper primary bearing #2 is used to provide sustainable motion within the machine.

#1 is the core structural shaft. Representing a base core shaft for revolving of the valve; critical to the machine. The core shaft represents a straight pipe or drilled rod, upon which the machine rotates to create the revolving motion needed by industry. Bearings are fed along this pipe by pumping oil into the top of the pipe and letting that oil distribute itself throughout critical oiling holes #25 in the piping. Oil, is then recollected in the sump area #36. piping back to the top, follows the structure.

#3 in this drawing is the exhausting turbine/ a port #12 detours around the bearing so as not to overheat it. #4 represents the vanes of a common turbine. Exhausting gases are shielded and contained within the housing #5

#6 is an exposed view of the rotating wheel valve: for an understanding of placement.

#7 is the ring structure, upon which machinery containment interfaces with its pistons; but illustration, top view; does not contain any gate valve 19 & 21 descriptions.

#8 and #26 represent 2 of 4 piston cylinders perpendicular to each other; as are present in this drawing. #13 & # 31 represent a piston rod heading for a crankshaft/ not shown. In accordance with the piston cylinder (well known) as would be mounted to the ring structure or onto the floor; preferably on slides. #9 represents 2 of 4; the basic gearing/ clutching attached to the crankshaft; as you desire it to be. A drawing too small, does not sufficiently help.

#14 represents the spacing between rotatory valving and ring structure for labyrinth seals.

#22 represents a cutout to understand the valving/ and duct work itself is under this shield.

 

THE SIDE CUTAWAY VIEW OF OES, engine 2

 

in this drawing of a 4 cycle OES engine: we look into the engine to discover the various parts at work. Numbers correspond to the top view above.

The structural supports; simplified line and basic framework elements, as designated by #10 upper elements. #11 support posts; Identify the common structural components being used. Reality knows the size of the machine will dictate how many along with design needs.

We begin at the base of the machine which is an electrical generator attached to the primary output shaft 9 by various means at #15 a bolt on flange. suitable methods for replacement of that component should be engineered in.

we then rise to examine the collection point for oiling; as would be dumped onto a flat plate that spins so the oil can be recycled and cooled before going back to the top. Or it can be used in the other direction; but will require sealing surfaces. Spinning the disk will separate out foreign particles; suitable methods for cleaning, housing, etc. should be used. A potential, non-pressurized system; pump oil up and let it flow down.

#35 represents one of the structural components used in this machine, and it holds the rotating valve and spinning turbine, of the machine itself. Through/ or upon, a bearing support #17. Which in this design; may or may not function to control the spinning rotatory valve as well.

What has not been adequately defined in this design until now is the use of position changing vanes #23 one of two shown, top of rotating valve. Operated by linkage #24 to engage the pressures being generated by the pistons. Collar #34 is being forced up and down, while spinning on slides 32 by the hydraulic cylinders as needed #33. it uses a rotating guide to interface the rotating and non-rotating parts (rather like a common vehicle clutch bearing is). More likely than a mechanical linkage along with its parts; is the use of an electrical drive of some kind to actuate the vanes going up or down as needed to vary the speed of rotation; with exhausting gases. These vanes are straight, curved, coiled over, hooked or whatever is deemed suitable to the job. Required although unneeded with constant work/ when the horsepower is altered so is the speed of valving rotation. Because primary power is generated through the gear box. Turbine is secondary; rotary valve speed is influenced by exhaust gases. Some degree of regulation may or may not be necessary.

#31 is a starter motor; and it is not properly placed or designed with a v-belt: because it is considered to be an almost irrelevant part. Once the machine is started it is not expected to be shut down in electrical generation for years. A starter rope/ the generator at the bottom/ gearing or whatever you desire is your choice.

#38 structural collar; upon which the rotating valve is built. Speed of the rotating valve is different than the output shaft therefore they are not attached, except through the exhaust recovery turbine. and are separated by bearings #16 which is supporting the core shaft off the triangular form not labeled. And bearing #17 which supports the machine and valve separately off of support 35. This machine uses “half valving”. WHICH MEANS; the lower rotating valve divided in half #30 vane like inlet; is different than the upper half #29 vane like outlet. They are divided in the middle; separated from each other by shielding #31. Which does enter the ring structure to form at least in part; a labyrinth seal. The lower inlet turbine for forcing combustion air into the cylinder #26 begins at the lower shield suction inlet (#39 crossed out; bottom of valve). combustion air is then forced into the cylinders as the circular valve line opens.

To shut off a cylinder a rotating or slide gate is used as shown in this version: operational motors #20 and 18 actuate the valve positioning (shown one up and one down). Valve plate is #21 & #19 shuts the hole. The housing #39 & #40 are used to contain loss of pressure.

Combustion gases are exhausted through circular valve opening #29 into the upper duct work area the valving structure #28, and expelled through turbine #4 at opening 12

the use of a stiffener truss #41 (as needed), may be required to support and restrain the rotary wheel valving surfaces against explosive events; same basic area as operation vanes. Along with stiffening for weight control over this part of the machine as well. Only one is shown.

 

Because the primary horsepower of a 4-cycle machine is through gearing and crankshaft; it is not considered best for electrical generation/ or its extremely high horsepower requirements. But it added for understanding and experimentation of the basic principles. However, it is potentially suited to such things as trains, trucks, helicopters, by combining vertical OES engines together; clutching to separate or use together/ gearing to offset rotational torque/ combining air inlets together; etc. plus, even smaller or larger examples of rotational force.

In this model; is an oiling table and collection area. Fitted onto the primary shaft; oil, that is flooded into the top of the primary shaft and fills the piping that extends through the machine; bearings are lubricated and cooled by this oil/ through various one of four holes 25 shown, in the cut away side view. Drilled in the piping, for that specific purpose of bearing lubrication. Once oil is released at the top, a gravity flow oiling should be enough/ but if not, it can be pressurized. At the bottom of the primary shaft when the oil is being released. It falls onto this plate, 36; is spun by centrifugal force; to help collect and eliminate contaminants. If an enclosure is created/ the forces applied could be gained by adding suitable vanes; to be used to pump the oil back to the top. Oil is collected in the circular gutter built for that purpose. It then flows out to the various filters/ and back into the circulatory oiling system. Pumping will require seals and so on/ if gravity is not used. Its purpose is to eliminate as many “sealing surfaces” as possible/ as these surfaces, are in hard to replace areas.

The basic structure modeling fig drawn; side view/ top view; of the 4-cycle revolving portion used in this engine valve train. In this medium sized OES engine. It is built with a flat plate 31 in the center that is not attached to the primary shaft of the OES engine. Instead, it revolves independently on its own bearings, which are lubricated through the primary shaft 1. The entire assembly is supported from the bottom structure on its weight bearing 17/ which sits on the structural support 34, above oiling table15. Oil is delivered through holes 25 (4 shown) On the flat plate 31, the circumference of the valve, piston facing surface. Are the actual valve fittings which engage the piston cylinder locations through corresponding elements created in the ring structure/ and on the rotating valve. Curved surface encloses the piston/ cylinder, to create close tolerances. Air inlet Openings in the bottom vertical valving structure; divided by the flat plate horizontal structure; provide the inlet air for fuel mixing. While openings on the top valving vertical surface allow for exhausting of combustion gases (not shown). The flat plate 31 keeps these systems separate. Labyrinth seals (not shown): created by laminating appropriately sized materials; on “top, bottom, and middle” provide extra sealing beyond close tolerance; for the half valving areas in the ring structure, mating surfaces top and bottom. Directional vanes 29 and 30, are used in both inlet and outlet areas to aid in the purposes intended. A turbo charger arrangement (not shown) located next to the exhaust opening/ along with ducting to further pressurize the inlet air preceding final closure of the piston cylinder may also be used. Oiling for a turbocharging element, however requires specialized design, off the revolving valve primary shaft structure; not suited to this work. As the inventor/ it is not my job to provide every detail; adapting what is, already in production. Trussing elements as needed are used/ which does include the “additional circumference blocking” to ensure adequate strength to withstand the exploding gas piston pressures.

Again, cut away shows the revolving valve structure, on top “exhaust”/ the bottom air inlet fan view. The optional speed controllers open and 23 closed views. The bottom view shows the vertical center structure on bearing 17; secondary is the operational sleeve 38 of the valve, and its air inlet source circle 27. not shown are the “ring and pinion gears or stops” used to create the necessary valve timing adjustments, in 4 cycle engines. This combined with the fan itself and combustion holding areas/ magnetic or other versions of timing location singles on the bottom edge of the lower labyrinth valve seal. Make up the bottom side of the revolving valve inlet structure. On top of the flat plate 31 dividing the revolving valving is the exhaust area. We find speed controllers 23 built onto the trussing methods in this design (various methods are known to exist). They are simply fan blades of suitable design/ that can be pushed in an out; or around in a circle fashion, or whatever is found useful; in the exhaust area. To the purpose: to aid the rotation of the rotational valve for timing advance or retardation of the cylinders, in piston firing as is constant in common piston engines; for this valve. The ability to regulate different arrangements by isolating piston/ cylinders as seen by isolating breaks/slide doors 19, 21; to shut off individual cylinders; as on the original drawing. Means there will be a need to regulate how the gases flow to achieve a constant speed in the OES machine, as needed. The speed controllers 23; are changed in position in this scenario: because a rotational valve holds mass; it needs help to alter its position. by push rods 24 and its linkage 34; coming through the dividing flat plate 32 operated with slides, from the stationary structure to the revolving valve. Not shown are the ring gear attached to the core shaft 1/ and the corresponding angle gears attached to 38 the valve structural sleeve. Or its linkage operated from the raising and lowering of linkage sleeve,34 and its push rod to turn the angle gears thus moving the rotational valve against the core shaft 1 to change its position. Or hydraulically pushing the linkage sleeve 34, can simply push it against an inclined ramp/ on the core shaft; so long as the sleeve is holding position against the rotating valve. A 4-cycle speed controller (you decide) aids this movement; in an environment of pulsing pressures and their effects. However, in 2 cycles with major turbine vanes; too much pressure will be present to change valve position.

IN THE MODELING, 4 cycle VERSION: there is a need to identify the method being used to operate the speed controllers 23; on the revolving valve. A simple operational sleeve 34 is fitted to the bottom half of the rotating valve. Push rods activating movements then go up and down based upon the position of this operational sleeve 34, to control positioning of the movable fan elements being used; and change the position of timing associated with the 4-cycle event of piston use. The sleeve rotates with the valving/ therefore an elemental transference of motion to a fixed position must be formed as are the elements 32. This is done with a common “bearing (mating surfaces which allow bearing slide elements, to displace movement)” and transfer motion from a stable position to one that is moving at different speeds; in this style arrangement 32. In this plain arrangement, it is shown without, what would be a beveled surface to avoid circumference issues, where surfaces meet. Starting methods; which includes the potential v-belt pulleys or gearing, used by the motor(s) 31, to engage force/or may be used at startup, in conjunction with disengaging all but one piston cylinder; so that startup of the mass in motion can be of limited torque.

Hydraulic cylinders 33 provide up and down movement as the simplest form of speed control. But they are built onto a stable surface; to interface with a moving up or down platform 32, along with motor drives for starting, 31 if needed. Starting the valve in rotation or modulating the speed of the rotating valve, through electrical inferences. Not properly drawn, the speed controller sleeve 34 interferes in this arrangement: better the v-belt or other should attach to the inlet area as is crossed out area 39. The bearing 17 which isolate movement of the primary shaft, also provide the functional positioning for cylinder placement and rotating valve isolation through gearing ratios, not shown.

Built onto the structural framework 35, with supports 10. The intent is to create the necessary elements to begin putting the engine in motion/ or regulating, in addition to heat exhaust operations; its valving speed.

Illustration, shows a top view of the LARGE SIZED; OES engine ring structure 7/ primary mounting surface for this machine. It is built of laminated plates cut according to need, which then allow for simple labyrinth extensions as required. Each cylinder hookup is aided by at least 4 bolts. The vertical slide plates to shut each cylinder off, and an optional compartment style fitting placed between the piston cylinder and its ring mounting area. Suitable enclosures are used to isolate individual piston cylinder combinations. Are used to encapsulate/ enclose the areas between the ring, its piston, and revolving valve if needed. The ring is where the housing mounts too. The housing identifies more than one type of final exhausting chimney can be used in the housing, to direct gases into the turbine(s) if separate. As well as a central area opened to aid in cooling the bearings of the primary shaft, rotating valve, and its parts. The housing does not move.

 

 

 

THE CLAIMS: OES Engine #2 James Frank Osterbur/ inventor-owner

 

1.     CLAIM: Combining units/”stacking parts” to increase horsepower; by altering units to create more compact or specialized, configurations IN THE OES designs or definitions of this machine, in any and all ways; are as described and defined by the potentials; whether horizontal or vertical expressions, of this machine.

2.     A device according to claim #1; a machine which incorporates a divided rotating valve wheel that uses a labyrinth style intrusion into the ring structure to accomplish that fact.

3.     A device according to claim #1; a machine which can be built with sectioned bolt on, inlet and outlet valving surfaces; to accomplish building bigger machines.

4.     A device according to claim #1; A machine which potentially, uses a spinning disk to create the filtering effect of oil in a combustion engine.

5.     A device according to claim #1; a machine which incorporates a stiffening truss as needed into the valving structure, which uses #31, the dividing shield to build off of.

6.     A device according to claim # 1; a machine which directs the flow of combustion gases into the turbine, either directly: as shown in the cut away side view or by moving the turbine to “off structure” work; not shown. As would be let the exhaust be duct ed to a separate turbine machine/ generator

7.     CLAIM: A machine which uses a directional vane located within the combustion gas duck work of the rotating wheel valve; to regulate speed and potentially, position changing vanes; to further regulate speed, within the combustion process.

8.     A device according to claim #7; A machine which incorporates mechanical activation of those position changing vanes to lower, turn, raise, shape, or whatever is required to regulate the speed produced by varying forces; to turn and control the combustion process/ by regulating valve speed.

9.     A device according to claim #7; which incorporates valve timing advance or retardation/ along with position changing vanes to assist in that turn.

10.  A device according to claim #7; A machine which can use electrically/ mechanically controlled changes in position changing vane dimensions; either by commutator means or some function of providing current from the generator through the main shaft.

11.  A device according to claim #7; A machine which can use various forms and means of starting its operational process.

12.  A device according to claim #7; A machine which houses the gate valving partitions, to contain pressures.

13.  A device according to claim #7; A machine, which protects the bearings from excess heat by placing them appropriately outside the primary heat, where possible.

14.  CLAIM: that units, complete machines; can be stacked together to form larger horsepower units working in tandem or not/ creating multi-layer valving.

15.  A device according to claim # 13; whether face to face/ or back-to-back/ or in sequence, a line of units functioning as the same; has no effect on the fundamental of design outcome by unit work.

16.  A device according to claim # 13; a machine which incorporates a muffler, insulating housing by building it off the structural components of the unit itself, or in tandem as required.

17.  A device according to claim #13; a machine used in operation, 4- cycle, that presents primary gearing for the operational aspects of tying it together into one primary power output shaft: which is locked together to power the generator first; turbine is secondary in this arrangement.

18.  A device according to claim #13; a machine used in 2-cycle which uses the turbine as primary revolving input power; for the output shaft, turning the generator.

19.  A device according to claim #13; a machine which uses alternate power sources to create the necessary influx of combustion air/ providing duct work to accomplish that goal.

/James Frank Osterbur/ inventor-owner

 

 

 

 

 

 

THE OES INDUSTRIAL, electric generation engine;

extending/ continuing, the patent 18/944,161 in this architecture of another, primary element; in patent continuation or extension: 18/952,324

 

Floor 1: is the generating body of electrical generation, by conversion; and is constant and unchanged here from current methods; (first floor). Therefore, a simple box 7 is used to identify it. As well as a simple bolt on interconnect or other as manufacturer decides, ties it to the core primary shaft 6. Generator sits at the bottom to avoid excess heat.

And is cooled, to a limited degree; by the center of its own primary shaft 28, open for water passage: thereby extending water into the primary shaft of the core OES machine. This shaft is hollow to allow for water, to pass through. The hollow shaft connecting through gearing and generator, are then the primary conduit for first stage cooling throughout the machine itself. Water in tank 1, (lower level) is pumped 2 into the bottom of the generator shaft 6 and extends up into the outlet 26 and 27 , that feeds cooling frameworks 23 in the revolving valve, starting at reinforcing sleeve 52. The interface , where pump meets the core primary shaft; pumping water into that shaft; will be the only rotating; sealing surface of this machine. Water for this purpose is found in the lower-level floor which represents a tank 1 and pumping methods 2; along with “outside drainage”, if the water level gets too high. Thereby protecting the generator.

 

Illustration labeled industrial OES : ONE OF ONE. Showing all necessary configuration, for the purposes of basic design.

then constructs the basic layout for machinery gearing 8 (floor 2) as would be suited to the purpose of an OES engine for electrical generation 7. options for gearing are; It can sit on the bottom of the primary shaft, with the electrical generation next in line/ or above it. As is, it can be placed on top of the electrical generator being second in line. Matters not to the power structure of the device. However various maintenance elements of working on the OES engine or its components would go better with the gearing: “pto (removable) shafts 9 (four shown/ drive line 11 goes up to flywheel 12)” over a: removable lowering of the support structure. To remove the generator/ allows, for lowering the core primary shaft, and potentially gearing through the floor. Construction of lifting devices, etcetera is not shown. Nothing is being designed other than basic layout of the gearing. Consequently, nothing is otherwise noted or explained. Generally, this gearing; would be several beveled ring gears with numerous pinion gears engaged as needed. Two, or even more; bevel gears tied on each ring spaced around or, on top of each other, as different ring gears allow/ with pinion gearing engaged in each one. Would double the horsepower in a similar, but slightly larger size box. Gear housing would contain a large “weight, bearing” at the bottom to capture and hold some of the forces involved. The piston crankshafts/flywheel shown 12; generally, have two pistons to a drive line. These are basically hooked to a truck differential 10 (4 shown) axle; which turns in reverse of its normal operations. Has two clutching devices one on each independent crankshaft are used.

In four stroke operations: the crankshaft is turning the engine as the piston is compressed and the explosion drives/ pushing the force out to turn the crank; which turns the gearing. This relates as a common power stroke which then turns the generator as its primary source of geared power. Secondary power is duct-ed through the turbine, which captures the exhaust before it is allowed to exit; to turn an auxiliary generator, or other.

In two stroke operations: the crankshaft is being pushed by the gearing to create timing and to force the explosive event and its combustion gases out into the turbine 29, which turns the primary shaft/ which then turns the generator 7 as its primary turbine power source.

 

Floor 2: the machinery gearing 8, as is the timing factor used to properly engage each and every piston cylinder being used; functions with the rotating valve at its machine in motion/ by rotating the primary core shaft 6. Ring gearing, Is a “triple or more” concentration of gearing. Which keeps the ring and pinion gearing arrangement, at each level speed controlled; as is form and function of timing (same sizes, throughout/ or not if desired). The concentration of power used to aid in turning, both the primary shaft of the machine itself, and the tools of piston and cylinder as well as turbine and generator; are forms of that conversion. In this stacked gearing each gear is keyed to its own position on the primary shaft; because in this arrangement we can add as many operational pinions created “drive shafts 9”; as we choose. By adding more ring and pinion gears to the stacked method; and the primary shaft turns at higher RPM with smaller diameter gear rings; thereby accepting the power being applied to a single output shaft 6. This is necessary, because of the size being used in the OES revolving engine valve. Proper sizing is up to you. Speed variations can occur at any place along the drive line. Each drive shaft the final device connecting the crankshaft of each piston cylinder and its flywheel 12, that is being used should contain a fluid shock collar to absorb errant forces. In the illustration; “the crankshaft moved forward”/ represents a much shorter drive line: when the piston connecting rod is “guided at the back 49 and 50”. Fluid Clutching distributes and engages the timing, controls engagement; as well as associated shocks being distributed down the line. The removal of independent piston cylinders from the operation of the whole machine; is through clutching or its alternate forms of repositioning “timed elements”. Engagement points which functionally align in true timing of the operation/ are then used to disconnect and then reconnect; along with electric motors, sensors and so on; as used to create the necessary movements. As simple as a drop in pin, once in-time placement, has been accomplished; “so to speak”.

(Floor 1): This merely represents a packaged generator 7, and is inserted into the OES engine for the purpose of making electricity. It can be added to the top/ or the middle in a stacked unit; your design. At the bottom area, as shown: its bearings function to aid the primary forces being applied to the machine itself. However primary weight and stresses of lifting frame 4, the machine rotating valve are transferred into the bottom bearing 5; as is support 4 for the primary shaft 6 and rotating valve 52. Although the primary shaft may or may not extend through, and independent generator gearing may or may not be added to attain different RPM levels.

 

Floor 3 and 7: there are two distinct forms of oiling in large scale operations. The primary bearing at the bottom of the machinery gearing, which is incorporated into the gear box; sustains rotational forces. Separate or used in conjunction with the bearings of the generator and geared housing; are “manufacturer oiled” from inside those housings. By fitting the upper geared housing with an additional bubble frame (space extending up is used in conjunction with labyrinth seals), housing non pressurized oil, on top of the bearing for holding oil/ not shown), to the primary shaft with a labyrinth seal above: any oil being pushed up through the bearing: will then fall back down into the bubble space, and drain back into the gearing house below, being firmly seated to not leak below. Eliminating a wear seal. The top bearing of the primary shaft is lubricated at the top of the machine and needs no further description. However, if the turbine is deemed necessary to SPEED, by gearing up (not shown) that will add an additional two bearings or more to support the “steam like, turbine” vanes in movement; and will be oiled by letting oil drain from the top down through the bearings. Which will then be collected by another “bubble framework housing; with labyrinth seals” at the bottom of the turbine; a space used to collect the oil. Which then transfers that oil to: A stationary pipe, with common fittings, and the attached impeller; to pump the oil back up to the top, while the primary shaft turns. A suitable means of directing oil into the impeller is used (not shown)/ and a plug 25 is introduced in the primary shaft to ensure cooling water below does not extend upwards beyond its intended point of release. Pressurized oiling requires seals; standard seals, which do not work well, in hot environments.

Floor 3: the revolving valve requires in large scale operations, a throttling addition; which is steam generation “box 24” (floor 4). Therefore, it is more complex than that associated with smaller versions of the same basic core engine. We begin with the floor tank 43 holding “initial water, as is warmed; limited steam”. This sits under the revolving valve 52; which holds a small second tank 19 at the bottom of “turbine like vanes 45, 46, 47; being used to initiate power into the machine”; these vanes are welded into the rotating valve face to provide stability against forces being applied. And engages a liquid flow from drain opening 21, from the structural tubing 17. water held by the first valve tank 19, drains through the bottom facing labyrinth seals 20, used by the first valve tank to lower or drain water 43, into: the second-floor tank 42. Being used to create a means of transfer, within these labyrinth seals: to isolate and contain the transfer of water being used to cool the valve: draining thereby, to place it in the second-floor tank. As now heated water. The path is simply: Water is directed through the core assembly primary shaft 6( from the pumping station at the lower level 1 under the generator), and it is exited through that shaft holes 26, 27 as a waterfall intent (not pressurized) into the structural tubing 17, being used to facilitate the lift and movement of the revolving valve. Direct flow into the first revolving valve tank as is combined with the machine vanes being used; and aids in cooling the closed valve sections. By using heat as its pumping method: water falls from tubing 17 and is forced upward by heat into stand piping within the exhaust first turbine vanes 47. Those power vanes can be structurally transferred into the bottom of that tank, for stability/ and cooled if needed by pumping water into them (not shown). This is incorporated from within that tank, into the vanes and then drained out the bottom labyrinth seals 20. From water in the valve tank, used within the vanes, and behind valve explosive piston barriers. Alternately, by pumps being operated with “turbocharging” methods; or by direct gearing or electrical means; from outside the machine.

 

floor 4; engages with the upper valve, second tank structure 54; which is attached and held in place by the ring structure 22, of the primary core machine. The basic circle framework for containing the intensity of motion, from all aspects outside of the primary shaft 6. By incorporating forged ports used by the piston, cylinder arrangements; with u-shaped enclosures in between. Or by laminating with “flat steel modified to create the ports and other facets of “seals, locks, and openings” needed. The upper style second vane tank 54 is the second functional element in steam rise; it too is in the way of exhausting gases. While this can be forged elements for cylinder hookup; with u-shaped elements to house the labyrinth seals of the outer revolving valve, and thereby contain pressures otherwise lost. The more basic method is to build this ring structure by laminating structural plate steel into the form needed to do the work of both lifting and holding the structure of the machine and its components, which includes the second vane tank 54. In large scale, the housing for this work extends from the valve upwards to the ceiling above. Thereby forming a steam generator pocket 24 above each release of heat. The upper valve tank contains the vanes 46 which will remain stationary; and these vanes in combination with the revolving valve consist, to produce the common turbine style power functions. Which then participate in turning the machine. Steam piping extends upward from this second valving/ vane tank. The piston combustion exhaust is released beyond this tank, and is directed according to your own desires. Pressure will find its way out, or through the maze/ or as a directed flow; being largely separated from its heat source “piston”; which will rise. Your choice.

 

Floor 3; the significant difference between the large-scale production of this machine and the smaller scale versions is; an operational air inlet 14 valve on the outside of the piston cylinder 13 itself. As described, it moves back and forth in time/ or is moved circularly, or in steps around the cylinder or back and forth; in place to open slots. In the cylinder 13 to introduce air for combustion. In a timed circle there is no stopping or starting; making it less vulnerable to wear. However, it can be moved in a stepped motion if you desire. Rams used to create a back-and-forth motion; create, the closure can be more significant; but will include faster wear. Both versions, are operated or incorporated with, or by known methods already in use (not shown). These methods, with appropriate machinery operating elements including; rams or chains and such (spring assist closure) work in time; with the crankshaft/flywheel 12.

Thereby in time with the explosive event; to produce the fuel/air mixture needed to allow for that event to occur. Forced air 37, turned by 36, to aid in this endeavor is allowed by ducting appropriately from the outside. What is not covered previously is the expectation of in 2-cycle operation; roughly twenty degrees before the crankshaft hits maximum out. Is probably the correct timing “to start”, for that explosion to occur? We want the explosive event to participate in moving the piston back into the path of the explosion as it returns to move in the opposite direction and push the energy out into the core of the machine to move both turbine vanes and critical steam turbine at the primary shaft top. More distinctly prior to bottom out extension; center force is applied to insure by timing; would need the “padded for stress, flywheel”. This has the energy needed to provide a stabilized synergy, by coupling mass in motion with gearing 8 input. Of value in this arrangement is the construction of ignition, patent 18/944,161: which allows for the initial exploding value of primarily coal; with the additional reconstruction of pushing the “glowing particles” together, to aid in the completion of that explosion burn. Thereby we leave the revolving valve exhaust door closed; until the cycle of pushing the combustion gases into each other, has achieved its goal of a; “cleaner burn”. Piston; Probably around 60% returned. Which can be further controlled by shaping the revolving valve exhaust outlet design; in a more tear drop fashion.

The piston design extends to close the valve gate when fully extended in this large-scale version: to shut off this piston/ valve interface/ which does require a lock against movement of the piston. And will need a suitable door to hinge down or be wheeled into place (not shown); while the piston cylinder is out. Which means to sustain the most pressure; the cylinder, and its piston; must extend up to: the revolving valve; “least space lost”. A collar style inlet on the cylinder/ within a taper setting 15, forged or created by lamination’s matching the cylinder; to provide room for air flow, is likely. Design choices not shown. Timing of explosive events should be “opposite side cylinders; same”. Critical here is how oiling is achieved and that requires a redesign of the piston, so that oiling remains behind the slots for intake air. The lamination areas of the ring structure; openings in the forge, creating these air inlet slots (not shown) as close to the ring structure as possible. Laminating allows for grinding of each individual labyrinth seal, in place; thereby reducing manufacturing errors. The floor 3 holds the ring structure 22, and individual threaded supports allows for close tolerance to be achieved. Grind the revolving valve first/ THEN create the ring structure. Adding the increased area for inlet of combustion air; to that valving support in the lamination process requires specialized machining. This would then occur on or in, the ring structure surface; moving the valve itself, either as in and out/ or by circular motion; dependent upon space. A balanced piston (leading edge does not touch. with replaceable slides (not shown) at the back to insure it does not gouge, the cylinder walls. Or a combination.

 

Floor 3; establishes the steam transfer of energy to the primary shaft turbine 29; by creating a “flat plate/ or other 18” in the lower rotating valve (closing the hole). Heated by or from exhaust to the water supply being used to create steam, that starts in the first valving tank 19; is transferred to the second-floor tank 42. Is then pumped into the stationary vane valving tank 54; and is not being released into the main steam extraction system 24; which ends at the turbine.

Because this is a round OES machine; the steam sections are cut like a pie; with barriers (not shown) so that if some of the pistons are not working; steam pressures will not suffer; even though horsepower will. Exact elements are not provided; as the extraction of steam from heat transfer methods; have been used for over two hundred years. Pick what you like. The end result however is that along with the expulsion of combustion gases/ there will be steam jets to accomplish an intensified power push; as is directed and used by common steam turbine methods. The unfortunate reality of this assembly is speed of rotation; which includes the steam turbine itself. As such an appropriate elevation of gearing (not shown) to the top of the primary shaft 6 may need to be used to both accelerate the functioning speed vanes of the turbine, and keep it tied completely to the primary core shaft of the machine itself. Or separated from the OES machinery; as is an alternate method of turbine generation common to all power plants of the day. Which leaves the power of the turbine/ generator combination/ divided by duct work: from the primary shaft and its lower generator. To allow for a secondary generator powered entirely from the turbine and its flow of both steam and exhausting gases as created by the core OES machine in motion.

The energy being released by fossil fuels: is the expansion of space, as is the law of thermodynamics: more heat/ more space or pressures. The law of an action will produce a reaction adds in motion; as the 4-cycle engine produces a “hammer like” force/ which dissipates quickly, but is transferred to piston displacement. In this primarily two cycle method; we use the expansion of space by heat to create the force being pressure in motion from the piston into the revolving valve; to push “turbine style vanes”; along with heat. To participate by using steam to intensify that push formed by heat release, in the secondary turbine 34; (floor 6) an auger 31 like device is used to separate pressure being pushed by exhaust and steam; to alleviate back pressure. Motor aided 33, or driven by secondary turbine direct forces.

 

Floor 6; we then come to the exit of primary forces; to engage with secondary forces. As is another turbine 34/ generator in the exhaust plume beyond the first law primary turbine 29. There is still heat and its forces to be used. A larger (more torque_) diameter turbine, with smaller vanes and appropriate duct work; which is dividing the exhausting stream into two (not shown) to allow the top of the primary core shaft out; and reduce its bearing heat. The ducts can then be rejoined, as is probable. But in between the first law turbine 29 and the second law turbine 34, is a turn in the duct work of exhaust being released. That houses an auger 31 (shown for effect; much smaller) like method of separating pressures being released from the first law turbine 29. So that it is unaffected by operations of the second law turbine 34. The auger 31 turns with pressure from the exhausting gases; but is aided by an electric motor to insure there is no feed back into the primary turbine. From there the exhaust my hit a turbocharging fan 36 to force incoming combustion air fan 37; for the pistons. What is left of water heat and exhaust can be directed to “third form” work; which is to use the heat for “citizen purposes” such as recycling plastics into “Lego like, house bricks; for building”, or other. Pollutants gathered along the way are collected for injection into abandoned oil reservoirs.

Illustration shows a side cutaway view of the industrial electric generation OES engine, ring structure and its rotating valve. Primary to this design is its cooling properties. Steam piping is used, lacing back and forth in the area 24 claimed by each piston or otherwise/ as a heat source. To cool the machine, and create pressures at lower temperatures than exhausting gases. Water is pumped through the piping beginning at tank 1, up through pipe 6, core 28; to remove extreme heat from what will go through the turbine. Releasing that heat to create steam: into the turbine to generate force; with the exhausting gases; in a controlled manner. This is used as a heat regulating method, because materials do have limits. The turbine 29 is attached to the primary OES shaft 6, to turn the generator 7/ gearing 8 as is attached to that shaft. Or the turbine is located/ duct-ed beyond the shaft to be independent apart from pressures released into it. If the turbine is tied to the shaft; that shaft is sent outside the duct; through an opening to facilitate, cooling for the bearing(s, if gearing is added) are located to avoid as much excessive heat as is possible.

This machine incorporates a backstop exhaust auger 31 (floor 6)/ spun by whatever method is most useful/ generally turbine. Which is a new claim: being these are very large machines considerable energy remains in the pressure flow past the primary turbine 29. Therefore, the flow is turned to avoid heating motor auger drives and bearings as much as possible; an auger style device 31, rather than fan is more likely to retain pressures with less work. The purpose is: to retain the pressure loss from the primary turbine/ but separate that loss from its “next in line” back pressure turbine 34. For secondary power generation; or more. Thereby reclaiming as much, functional heat energy as possible; without affecting primary operations. Primary structure components (not shown other than floors) as are needed to support the housing and more are fundamental to the process; and are noted merely to suggest they exist.

 

FIG 9; primary to all operational methods of making the machine work; is startup; of the major components; which allows for the order and discipline of motion to continue. Because these are intended to be large machines with major amounts of mass to place in motion: that run for months at a time. The most consistent method of starting all that mass is “with a rope (common to all small engines)”. In this case however; at the top of the primary shaft; we will extend that shaft upwards to allow for wrapping with cable. A suitable winch anchored to the building: is then activated and pulls the cable to initiate motion. It can release the cable to a catching method/ or like small engines which use cogs to stop the engagement from a winch; it simply remains stationary until needed next time. A much smaller winch can be used to “wrap it back up”. If you disengage it.

The illustration; of a cutaway section; for a super large OES engine. It primitively shows a piston cylinder and crankshaft/ potential for a water jacket, or air release of heat (not shown); along with floor anchor installation. Functionally this Depicts a piston using an independent intake air valving system. Which is simply a collar 14, that moves along the cylinder to open and close the air inlet holes in the cylinder itself. Air Can be; supercharged or not with some simple duct work. Piston/ cylinder, shows slides on back side/ end of cylinder; with guides for stability of the piston rod, in this very large cylinder arrangement. If only one flywheel crank is used; it will need to be assisted with a “rack and pinion gearing”; to keep or apply pressures from both sides to the piston rod. In line the guides/ slides, holding these gearing methods of straight-line transfer to turning a shaft; requires a bearing to be used in the piston connecting rod. Oil is sprayed in from the back/ suctioned up to be recycled by the pump. The cylinder can be extended for applying guides with slots, but requires suitable drains.

The revolving valve as is used throughout the OES engine elements remains as designed for other versions. However, in this industrial version it does not include any option for air intake into the cylinder, through the rotating valve. The rotational valve; Merely closes for ignition and opens for exhausting as it turns to engage each cylinder separately; allowing for multiple engagements: for ignition, per revolution are obvious. Primary setup of the engine is in multiple floor tiers. And is best suited to a 2-cycle operation so as to limit gearing sizes. Magnetic reference, is the common way; to create valving locations for the piston, as used to trigger ignition. Generator on floor/ pistons another floor/ one or both turbines another floor/ a second set of pistons (different tier/ not shown) third floor and so on. height will provide the means to incorporate a cooling tower for fluids generated by the process. Careful work is required to limit sound, as best you can/ which might involve putting the entire machine underground/ or building a soil berm around it to focus sound upward. Numerous elements for sound control are required.

FIG 10; in the super large, industrial OES machine; there can be: a rotating valve, doubled in size as one row of piston cylinders are deemed not enough; thereby forming the double sized; rotating valves. Which then allow for two levels of piston cylinder arrangements. THIS however needs the leading edge of intersection between valve and each level of cylinder: to be governed by “guide wheels, which then control oscillation or movements of the valve as its spinning (bearings obviously outside the exhaust gas chamber/ shaped to run on a circular path). Slides can be used, but will encounter more wear (changing the rotating valve to incorporate a wider surface for slides is mandatory; thereby limiting the required, “more maintenance”. Labyrinth seals need stable paths. An adaption that might be necessary on smaller versions as well.

Alternating versions require; two distinct or combined ring structures; with the stationary tank 54 and its vanes in between; rising up and down; for both sides (not shown). Thereby adding another set of turbine vanes like 45, 46, 47; to the overall performance of the machine. This adds heat; but does not allow for the collection of heated water within a top valve tank; unless the valve is incorporated with duct work. That water in a tank which revolves on top; can be released into the environment of exhaust; as steam. And will be only enough to cool the valve sufficiently in this area. Steam is being released into the turbine; and the machinery must be adapted to allow; for this “free steam”. No water is likely to be drained, as the heat will not allow it.

It is an option/ where simply building an entirely separate machine seems less desirable. Bear in mind; once built, if successful: these are machines which will be in use; “for a hundred years”. The removal of combustion “debris” left behind during this process of fossil fuel burning: requires the separation of the valve once in a great while. Attention should be paid; to making that possible. it would involve taking out enough structural components (wedges in the gaps, between the valve tanks): to move out or in, the now sectioned pieces of the smaller valve tank 19. after removing floor tank 42. Then opening the gap, to remove the labyrinth entanglement. By adjusting the framework to a smaller diameter; so that it disengages from the labyrinth seals. This requires a loosening (movement) of the pipes which support the valve tank and deliver the water; your choice. Hydraulics can then move the rotating valve; down if you have allowed for the spacing/ and move it back up for return to use. If you remove the outer half stationary part, of the primary turbine 29. That would be functionally aided: by removing the generator (on tracks) to provide the room.

But critical elements of steam direction must enable the machine to go down; a design criterion.

Outer Clean-outs along the labyrinth seals; for insertion of spring-loaded tooling to periodically scrape away residual debris in the tiny gaps/ should be enough to keep the machine running for lengthy periods of time. Compensating for water debris, inside tanks and piping; is left to the “line of people”, who have been investigating and running steam engines for over two hundred years. They are reminded: this partition for intensifying power from heat; is far more like a steam locomotive/ than a power plant version of piping. Best method, is left up to you. Best method for construction: allows for the primary core shaft to be placed into position first: lowered, through the floors, into the lower-level tank/ then raised when needed, by winching from the top. Stabilized, by structural support off the machine gearing housing; or, from floor to floor; to allow for the opening to be created. When settled into position, with suitable locks; it should be safe.

 

We then come to the last version:

this illustration presented, provides parts and pieces; of a cutaway side view of a super large OES machine: that is separated from the turbine it feeds. The revolving valve assembly remains the same as for 2 cycle; but, is built in a slightly different way than. Piston/ cylinders; and ring structure is arranged in the same ways. The revolving valve contains no elements for air introduction in 2 cycle into the cylinders; same as industrial version. Combustion Air inlet is accomplished “outside” the primary revolving valve; on the cylinder as before; a back-and-forth circular motion is likely best, so that it can be moved slightly out for disconnect, and in for a better seal. So, the appropriate rotating valve structures; continue to contain the explosive event and releases the exhausting gases into the center area; as in 2 or 4 cycle. The housing (not shown) of this machine, contains the heat of combustion gases; and ducts or extends those gases through the floor to the next story where the turbine as with 29 exists, and is supported off the floor. The housing is designed to include sections of exhaust specific to each individual piston cylinder, or not. Combustion gases will be released through the housing duct work; just prior to the turbine; to make it turn.

The primary shaft 6 in this alternate “no steam” version; does not extend through the floor, but merely represents a stand pipe: for containment and control over the revolving valve. Control over the primary turbine is separate; as with common designs used in purely steam driven turbines. The bottom area of the rotating valve is enclosed to contain pressures; with a cone shaped area to direct exhaust heat; (not shown) surrounding the main axle structural sleeve; to strength the rotating valve 52. Primary shaft 6 (similar) to the illustration; is showered with water spray to keep heat down.

The rotating valve is attached too, and spins on the primary shaft; which sits in a depression in the floor. To contain the water spray, used to cool the shaft; it drains into the floor and water jets, are used to direct cooling steams onto the shaft to cool the parts which would otherwise get too hot. Shaft bearings are contained lower on the shaft, as would be wise. That cooling water is collecting in a drain in the floor and recycled. In this alternate: let the full heat of combustion, run the turbine/ rather than steam.

HOWEVER, steam generation is now located in the chimney beyond the turbine. After exhaust gases run through the turbine/ this heat is used to create steam. That steam is then redirected into the turbine with exhaust gases by piping. Water is pumped to the top of the chimney, flows down the various piping methods used to generate steam, and is introduced into the turbine to intensify horsepower as steam jets located just prior to the turbine hot entrance. Various methods of water cooling the piston cylinders. Various methods of sustaining the cooling of the rotating valve may be necessary/ or more distinct selections of materials can be used to build the various “hot parts”; along with a redesign of OES rotating valve vanes; to accommodate higher temperatures can be used. The “hot top housing”, can be used to contain some limited steam piping to accelerate the steam, prior to release. And with proper design that hot top housing can be removed for clean-out purposes.

This is now: instead of the “steam locomotive style generator” as seen in the illustration. A much larger power plant like steam generator; used to facilitate higher horsepower in the primary turbine. Energy; Which can then be isolated as secondary; is redirected into secondary turbines as allowed. Your choice.

Retrofit of existing power plants means to replace the burners with these motors/ whereas building new would see them arranged like spokes of a wheel surrounding a central steam generator tower. The upper housing of the “cone style engine”; merely represents the duct work required to direct pressures into the turbines being used. In addition to heat for steam: these motors provide a direct drive to electrical generation; thereby multiplying the energy output.

Oiling of the pistons being used; may be aided and abetted by a second oiling ring. One on either side of the piston rod pin. For balance in large diameter pistons. Appropriate slides on the back side would also be useful.

Oiling of the primary shaft bearings should be fully contained; as the water being applied to the piping should be enough to cool the oil. This is a 2-cycle arrangement; intended for large piston cylinder arrangements. Although it can be used in 4 cycle/ far less heat for steam is involved. The pistons producing force either on the crankshaft or, along with the heat presenting pressures, enforcing a push onto the turbine blades. Which uses a constant flow of combustion gases, through OES turbine vanes, to create the necessary speed within the revolving valve.

But uses a secondary transfer of power needed to start the machine from whatever method you choose; as is adding the interconnecting belt of chain or whatever to the bottom of the rotating valve. There is no need to identify what already exists in common steam turbine/ generator motion. Electric motors or whatever you choose can turn the crankshafts, which move the piston in accordance with timing created by the valve in 2 or 4 cycle.

In 2 cycle; Fired with the piston cylinder open, requires only enough push lost, to get the force needed to push pressures of combustion out. Which are leaving anyway once the valve opens the door. A flywheel on each crank; should be used to modulate piston motions. Suitable methods should be used to get the mass going; before the motor takes full control.

 

Items specified by the drawing entitled primary,

INDUSTRIAL OES ENGINEERING.

Item

1.     lower-level tank for cooling water to be pumped up the core primary shaft 6. by pumping 2 water, through the sealing shaft coupling 3 into the hollow primary shaft area 28. which is plugged at 25 to contain the water.

2.     Items 26 showing two holes for pushing water through the hollow core shaft and item 27 showing a cutaway of 4 holes in the primary shaft for pushing cooling water through. There are many.

3.     The water transfer box 23 sits above the rotating valve shown in cut away, which is built as a unit structure onto the structural sleeve reinforcement 52.

4.     water extends from the lower-level tank 1 through the hollow core primary shaft 28. out into the water transfer box and down the structural tubing 17 which forms the upper-level support for the rotating valve/ lower supports 16; are below the enclosure of the bottom valving 18. shaft and valve rotate together.

5.     Water flows down the pipe into the inner turbine vanes being used to power the turning of the machinery; which ends with turning the stacked gear box 8; turning the drive lines 9. which turns the secondary gear boxes 10 (there are many in the spider web like design)/ which turns the drive line 11 which turns or is turned by the flywheel 12 of the piston/ cylinders being used. These all function to turn the generator 7 and is aided by the primary exhaust turbine 29.

6.     exhausted gases and steam rise from the turbine into the duct work 30 which then encounters the exhaust auger section to divide the pressure/ and sustain the secondary turbine 35; without affecting the pressures 34 being released by the primary turbine 29. auger like design is rotated by pressures and a motor 33 on shaft 32. a suitable auger change at 42 would be consistent with the blocking of back pressures (you decide).

7.     After gases and steam flow through the secondary turbine it is duct ed into the “turbo fan”/ to use the last energy available for generating fan forced input combustion air. Through duct work not shown; a helping motor is likely necessary.

8.     water flowing through the inner third section of valve turbine vanes or beside it 21 flows into 19 the lower valve water tank which collects that water. Water 43 is then directed either into the vanes or enclosure box behind the closure that contains the explosive forces (not shown). And falls through the lower valve rotating tank; through the labyrinth seals, 20 and into the lower floor tank 42.

9.     we then turn to the piston cylinders 13. identify the taper fit 15. consider the inlet of combustion air collar 14 (you decide if it turns, steps, or goes back and forth). As it interfaces with the ring structure (laminated or otherwise) 22. labyrinth seals 53 both lower and upper, along with close tolerances; form the interface between explosive event and its result. And we recognize the flywheel 12 is turning the Pittman arm 51 and 48 ; to push the piston rod back and forth along the guide rails 49 and 50. the combustion gases are pushed through the ring structure 22/ and the valving position. by the piston not shown. Where it encounters the basic curved or otherwise turbine vanes. 47 is moving vane. 46 is stationary vane. 45 is moving with 47, and it is twisted to aid in the directional intent to produce force in the primary turbine 29 above. In a timed method of rotation and sequential ignition; to engage combustion gases with the rotating valve.

10.  Heated water flows from the first floor tank by piping and pumping not shown into the upper stationary tank 54 which holds the middle or more turbine vanes 46. that water turned to steam is found rising through the appropriate piping for the purpose of adding horsepower; by adding a steam generator 24 into the engine. Steam elements are not shown.

11.  At the top of the core primary shaft is the bearing 38; built into the structure of this 7-floor building; with a lower level. The starter winding 39 for “cable 40 starting” the machinery in motion by winch 41; is represented.

 

 

The property of fully saturated steam at atmospheric pressures is: at 500 degrees F steam has 700 psi/ at 700 degrees F steam has 3200 psi. horsepower released into the turbine, is then adjusted by steam/ based upon what you choose. Which is why nuclear reactors being capable of extreme instant temperature rise (then explode, when water is too low, or re-added). EITHER water supplies, should only be constructed over the reactor in some form. So that gravity flow, can cool them! Requires: Raised pools of water that exist above the reactor which insures a pipeline, gravity feed/ or reactors beneath the lake. Providing NO alternate source of power required. Gravity, will occur. Critical valving and sensors; is a constant, and needs backup plans.

 

This industrial OES MACHINES, as illustrated is essentially, a round machine with piston/ cylinders sticking out in a spoke fashion. To facilitate the building, and maintenance itself: running the piston cylinders in and out on a track “like a train” would produce the least headaches. A roundhouse building would allow for opening the side wall, and taking these devices in or out on these tracks; with the least amount of effort. Producing with a forklift and means; the reality to move them to an alternate site for maintenance or repair. As will be needed because of the noise and heat. Consequently, attention should be paid to simplify, or automate that process; for the sake of the workers. Such as a tapered cylinder that seals itself, once in place/ locks on the track to keep it in place/ and a fold down or out; interlock for gearing. A larger building would cost more and provide no relief from heat, danger, or noise. Which means: particular attention to detail, as to noise production must be limited as much as possible. Thanks to transmission of electricity; remote locations/ or underground; are best. Centering it inside of “dirt walls” can be done. Concrete transmits noise, even at unexpected, thickness. If successful: THIS WILL be in operation over generations of time.

The alternate version with steam generated in the chimney exhaust and piped in front of the turbine; requires ducting of that exhaust. Which means individual machines can be used as spokes of a wheel in individual buildings which then surround a chimney for creating steam. The potential to create these engines as vertical instead of horizontal is allowed; to reduce the duct work required, as is conducive to higher pressures; but probably not worth the trouble.

 

WE THEN ADD: to the claims of this machine, the 2-cycle industrial OES engine, and its architecture detailing a primary use; to generate electricity. Experimenting with its 4-cycle predecessor, initial model; adds the necessary “limited expense” version of use. Which, as do all OES machines; uses a revolving valve to achieve its purpose of fossil fuel induced motion. As this is, in continuation of my invention 18/944,161; it is subject to the various claims made in that patent. As is consistent with the continuation of this patent; both modeling of the basic design and discovery of what is elemental to the industrial generation of electricity by an OES engine..participating with steam; is involved in patent 18/952,324

19.  CLAIM: The addition of steam, generated and released into the primary power turbine; used to create higher horsepower, in the OES engine; either as a separate entity or in combination with the rotating valve.

20.  CLAIM: The addition of pressure separating “auger like devices”; so that secondary turbines may not influence or back pressure the function or horsepower of the primary turbine.

21.  CLAIM: The addition of a starting winch driven cable; to put the machine in motion; by Redefining the “starter rope” system.

22.  CLAIM: The addition of a gearing assembly; which allows for multiple ring gears of the same size stacked; to then be keyed to the same shaft; in order to create multiple pinions, turning the same shaft, at the same speed; with much higher horsepower/ as is needed, in a spiderweb like, assembly.

23.  A device according to claim #22; which can add an additional ring gear to the top for the purpose of changing speeds for something else

24.  A device according to claim #22; which can be added to the primary turbine, turned by the primary shaft, for speed acceleration as needed.

25.  CLAIM: The cooling of a rotating valve; by flow characteristics as designed and detailed in this patent.

26.  CLAIM: A core primary shaft supported by one weight loading, bearing and its supports/ Located at the bottom of the shaft; where it can be replaced; without significant trouble; one upper bearing for control of the primary shaft (separated from the primary heat source), and guide wheels or slides to further isolate and control movements of the rotating valve; for stability in labyrinth seals.

27.  Oiling of the very large pistons being used; may be aided and abetted by a second oiling ring/ One on either side of the piston rod pin: For balance in large diameter pistons, with Appropriate wear slides on the back side of the piston, would also be useful; to maintain position stability.