US1340563A - Turbine gas-engine - Google Patents
Turbine gas-engine Download PDFInfo
- Publication number
- US1340563A US1340563A US334590A US33459019A US1340563A US 1340563 A US1340563 A US 1340563A US 334590 A US334590 A US 334590A US 33459019 A US33459019 A US 33459019A US 1340563 A US1340563 A US 1340563A
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- Prior art keywords
- flange
- chambers
- explosion
- head
- cavities
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- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired - Lifetime
Links
- 238000004880 explosion Methods 0.000 description 32
- 230000002093 peripheral effect Effects 0.000 description 16
- 239000000203 mixture Substances 0.000 description 11
- 239000004215 Carbon black (E152) Substances 0.000 description 9
- 229930195733 hydrocarbon Natural products 0.000 description 9
- 150000002430 hydrocarbons Chemical class 0.000 description 9
- 238000002485 combustion reaction Methods 0.000 description 8
- 238000010276 construction Methods 0.000 description 5
- 238000001816 cooling Methods 0.000 description 4
- 238000007599 discharging Methods 0.000 description 4
- 240000000233 Melia azedarach Species 0.000 description 2
- 238000004140 cleaning Methods 0.000 description 2
- RLQJEEJISHYWON-UHFFFAOYSA-N flonicamid Chemical compound FC(F)(F)C1=CC=NC=C1C(=O)NCC#N RLQJEEJISHYWON-UHFFFAOYSA-N 0.000 description 2
- 239000002184 metal Substances 0.000 description 2
- 238000003287 bathing Methods 0.000 description 1
- 230000015572 biosynthetic process Effects 0.000 description 1
- CVSVTCORWBXHQV-UHFFFAOYSA-N creatine Chemical compound NC(=[NH2+])N(C)CC([O-])=O CVSVTCORWBXHQV-UHFFFAOYSA-N 0.000 description 1
- 230000005484 gravity Effects 0.000 description 1
- 239000000314 lubricant Substances 0.000 description 1
- 230000001050 lubricating effect Effects 0.000 description 1
- 238000005461 lubrication Methods 0.000 description 1
- 239000000047 product Substances 0.000 description 1
- 230000001105 regulatory effect Effects 0.000 description 1
- 230000008439 repair process Effects 0.000 description 1
- 239000013589 supplement Substances 0.000 description 1
Images
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
- F02C5/00—Gas-turbine plants characterised by the working fluid being generated by intermittent combustion
- F02C5/12—Gas-turbine plants characterised by the working fluid being generated by intermittent combustion the combustion chambers having inlet or outlet valves, e.g. Holzwarth gas-turbine plants
Definitions
- the object of this invention is to provide a rotating head which moves in one direction continuously, and is driven by gas explosions at alternate diametricall opposite sides of the head so as apply t e riving impulses in rapid succession, but with maximum cooling intervals in the respective explosion chambers, to prevent disintegration of those parts by the action of the great heat to which the are subjected.
- Another o ject is so to construct and house the rotary head that it will draw the air in and discharge it after the manner of a rotary blower, and cool the walls of the explosion chambers by constantly bathing them with a current of outside air of a much lower temperature.
- a further object is to form the parts so the will be easy to construct and. assemble, andY so they will be readily accessible afterward for cleaning, adjustments and repairs, and the object is to provide for the thorough lubrication of the rotary head.
- FIG. 1 is a view in side elevation of our assembled invention, a part of the housing being broken away to show the driving gears inside.
- Fig. 2 is a vertical section at right angles to the main driving shaft,.on the line 2-2 of Fig. 3.
- Fig. 3 is a vertical section on the line 3-3 of Figs. 1 and 2.
- Fig. 4 is a horizontal section on the line 4.-4, of Figs. 1 and 2.
- Fig. 5, is a detail in side elevation of one of the explosion chambers and its housing.
- the rotary head 8 is mounted on a main drive-shaft 9, which shaft is mounted in suitable journals 10, of usual construction, which, in turn, are supported by a base 11, within which there is a chamber with ti lit sides and bottom within which the hea 8 and a more immediate housing for said head, are suspended.
- the rotary head 8 comprises a hub mounted in a fixed manner on shaft 9 a rim 12, and a web 13, connecting the hul) and rim.
- Formed equi-distant from each other in the rim are five expansion pockets 14, into which expanding gas from exploded gas mixtures in appropriately located explosion chambers, is admitted at predetermined positions of the head.
- the walls 15, of the pockets present surfaces toward the direction of travel of the head which are adapted to convert the expansive force of the gas into rotary energy against the head, a concave shape being here shown, which is approached by a plane surface 16, in a chord of the peripheral circle of the head.
- the rim 12 is also provided with an integral radial lange 17, having a port 18, between each pair of adjacent pockets 14. This ange shuts olf the supply of gas to the explosion chambers except at proper sitions when admission of gas is provide for by a suitably located port of the rotating ange coming into register with a port of a stationary explosion chamber.
- the periphery of the rotary head 8 makes a close running lit in an annular band 19, of a fixed housing comprising also a radial flange 20, having a close running fit against the flange 17 of the head.
- the lian e 20 is bolted to a removable disk 21, whic closes that side of a housing for the rotary head.
- a web 22, on the other side of the head, is integral with the band 19.
- the web 22 has a series of openings 23, for the admission of air to the interior of the housing for the purpose of air-cooling the metal of the rotary head surrounding its expansion pockets 14.
- a positive air-current is insured by the formation of openings in the web 13, each having similarly oblique radial edges 24, 25, which act as vanes, on the principle of a blower to draw in the air and discharge it when the head is rotated.
- the explosion chambers 26, here shown as two in number, are located diametrically opposite each other in the angle between the casing-members 19 ad 20, and are pref- Vlatter are successively brought into position opposite an open end of one of said explosion chambers 2G.
- the driving impulses will be exerted on the rotary head at alternate diametrically opposite intervals; and a maximum cooling time will be afforded to the parts which are heated as an accompanying result of the explosions.
- the explosion chambers 26 are closed at their outer ends by removable heads 2S, which support sparking-plugs 29, of usual construction; and, to insure the maximum obtainable air-coolin f efficiency we surround the major portion o' said chamber 26 with a casing 30, having entrance ports from the main housing and discharge ports 31 near their outer ends.
- a fan in housing 30 of usual construction, which is driven by spur gears 32 and r,33.fr om shaft 9. Gas enters the housing through pipe 34 and is discharged through pipe 35 into manifold 36. The latter has two branches each leading to a respective explosion chamber 26, on each side of the engine. A'damper 35 affords means for regulating the supply of air to the housing 30.
- a pop-valve 37 takes from the pipe 25 and has a pipe 38 to return the excess gas mixture to the pipe 34 so none will be wasted.
- a magneto 39 operated by gears 40, 41 and 42, from shaft 9, is wired, in the usual ⁇ manner to the spark-plugs 29.
- the magneto has the usual timing device (not shown) for furnishing the required spark at the right time and place.
- Oil cups 43 are provided in suitable proximity to the rotary head 8. These have oilsaturated wicks which wipe the peripher of the head, and the lubricant thus deposited is carried and distributed by the rotating head.
- This periphery has annular channels 44, in which the surplus oil is drained and deposited by gravity in the lower part of the housing for the rotary head, as shown in Fig. 3. From there it is taken by a pump 45.
- the pump is driven from the arbor of gear wheel 41, by a belt as shown in Fig. 1.
- the pump returns the oil to the cups 43, through pipes 46, and any additional quantity needed is taken from an oil tank 47.
- the journals for shaft 9, and other shafts and rubbing parts are accessible and may be lubricated in any usual and suitable manner.
- the exhaust is to chambers 48, 48, on diametrically opposite sides of the rotary head 8, when the respective charged heads reach them, and the spent gas is taken thence through suitable pipes 49 to a muffier (not shown) or wherever desired.
- the hydrocarbon mixture is in the branches of the manifold pipe ready to charge one of the explosion chambers when one of the ports in the rotary flange registers and provides the required opening. Then the supply is cut off by the travel of the liange and the charge in the explosion chamber is fired just as the next expansion chamber reaches the opening in the small end of the explosion chamber. The expanding gas enters the expansion chamber as the latter moves on and a further rotation of the head brings the' expansion chamber opposite the exhaust chamber where the spent gas escapes.
- a rotatable member having a plurality of expansion chambers, relatively stationary explosion chambers, means comprising a flange on the rotatable member with ports to supply a hydrocarbon mixture to the explosion chambers, means to ex lode the mixture, means for discharging t e expanding product into the expansion chambers, and means for discharging the spent roduct,
- a rotatable member having a plurality of peripheral cavities and a radial flange with a port opening between each peripheral cavity
- a stationary member having an annular band in which the periphery of said rotatable member makes a close running lit, said stationary member also having a fixed radial ange maln'ng a close running fit against the fiange of the rotatable member, one or more explosion chambers fixed in the angle between the annular band and its flange, each chamber having an inlet opening through its ad] acent flange adapted to register with successive port-openings of the rotatable flange and said explosion chambers each having an outlet opening through the annular band of the stationary member whereby communication is established between an explosion chamber and a peripheral cavity when one of said cavities is brought opposite the outlet opening of that chamber by the movement of the rotatable member, means for supplyingi a hydrocarbon mixture to an explosion c amber when the openings in the two flanges register
- a rotatable member having a plurality of peripheral cavities and an adjacent radial flange, said iiange having a transverse portopening between each two of said cavities, a fixed explosion chamber having an inlet port closed by said flange except when in registration with a port of the flange and having an outlet opening closed by the rotatable member except when in register with one of the peripheral cavities of said rotatable member, a manifold pipe supplying a hydrocarbon mixture and closed by the rotatable ange except when its openin is in register with a port of the flange, an means for exploding a mixture in the explosion chamber.
- a rotatable flange having a plurality of portopenings, an explosion chamber having an inlet port closed by the flange except when in register with a port of the flange, a manifold pipe su plying a hydrocarbon mixture and close by the rotatable flange except when its opening is in register with a port of the flange, and pacln'ng between the flange and explosion chamber and between the flange and manifold pipe to prevent hydrocarbon leakage.
- rotatable member having peripheral cavities forming explosion chambers and having an adjacent peripheral liange with transverse orts between said cavities, a fixed member aving an annular band and a radial ⁇ iange both maln close running fit with the periphery an flange of the rotatable head, respectively, and means for automatically lubricating the rubbing parts.
- a rotatable member having peri heral cavities forming expansion chambers, xed explosion chambers, means for creatin air currents by the rotation of the rotatab e member and means for subjecting said chambers to the cooling action of the air currents.
- a rotary member for internal combustion engines having peripheral cavities forming explosion chambers and a peripheral flange with transverse ports between the cavities in combination with a fixed member having expansion chambers discharging into the cavities of the rotary member as the cavities come opposite, and means for supplying a hydrocarbon element to the expansion chambers through the ports in the peripheral flange.
- a rotary member for internal combustion'engines. having peripheral cavities formexplosion chambers, annular peripheral oilruns, and a peripheral lian e with transverse ports between the cavities in combination with va fixed member having ex ansion chambers discharging into the cavities of the rotary member as the cavities come opposite, and means for supplying a hydro carbon element to the expanslon chambers throulgh the ports in the peripheral flange.
- fixed member for internal combustion engines having one or more explosion chambers and one or more exhaust outlets, in combination with a rotary member having peripheral cavities which are successively brought into communication with said explosion chambers, and a flange with transverse ports between said cavities through which a hydrocarbon element is supplied to said explosion chambers.
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- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Lubrication Details And Ventilation Of Internal Combustion Engines (AREA)
Description
G. F. AND K. 0.-scHM|D.
TURBINE GAS ENGINE.
APPLlc/Tlon man ocr so, 1919.
G. F. AND K. 0. SCHMID.
TURBINE GAS ENGINE.
APPLICATION FILED ocr so. 1919.
1,340,563, Patented May 18, 1920.
2 SHEETS-SHEET E.
UNTTED sTATEs PATENT oEEicE.
GOTTLOB I'. SOB'JIID AND KARL 0. SCHHID, 0F INDIANAPOLIS, INDIANA.
TUBBINE GAS-ENGINE.
Speoication of Letters Patent.
Patented May 18, 1920.
To all 'whom it may concern.'
Be it known that we, Go'i'rLoB F. Somali and KARL O. ScHMiD, citizens of the United States, residing at Indiana olis, in the county of Marion and State of diana, have invented a new and useful Turbine Gas- Engine, of which the following is the specication.
In reciprocating-piston gas-engmes the driving impulse is exerted only every fourth stroke, the three other strokes being consumed in cleaning out the cylinder, drawing in a fresh mixture of air and gas, and in compressing the latter before ex losion. Moreover the chan e in direction o travel of the piston resu ts in lost inertia and causes a pounding strain on the mechamsm which is damaging.
The object of this invention is to provide a rotating head which moves in one direction continuously, and is driven by gas explosions at alternate diametricall opposite sides of the head so as apply t e riving impulses in rapid succession, but with maximum cooling intervals in the respective explosion chambers, to prevent disintegration of those parts by the action of the great heat to which the are subjected.
Another o ject is so to construct and house the rotary head that it will draw the air in and discharge it after the manner of a rotary blower, and cool the walls of the explosion chambers by constantly bathing them with a current of outside air of a much lower temperature.
A further object is to form the parts so the will be easy to construct and. assemble, andY so they will be readily accessible afterward for cleaning, adjustments and repairs, and the object is to provide for the thorough lubrication of the rotary head.
We accomplish all of the above, and other objects which will hereinafter appear, by the mechanism illustrated in the accompanying drawings, in which- Figure 1, is a view in side elevation of our assembled invention, a part of the housing being broken away to show the driving gears inside. Fig. 2, is a vertical section at right angles to the main driving shaft,.on the line 2-2 of Fig. 3. Fig. 3, is a vertical section on the line 3-3 of Figs. 1 and 2. Fig. 4 is a horizontal section on the line 4.-4, of Figs. 1 and 2. Fig. 5, is a detail in side elevation of one of the explosion chambers and its housing.
The rotary head 8, is mounted on a main drive-shaft 9, which shaft is mounted in suitable journals 10, of usual construction, which, in turn, are supported by a base 11, within which there is a chamber with ti lit sides and bottom within which the hea 8 and a more immediate housing for said head, are suspended.
The rotary head 8 comprises a hub mounted in a fixed manner on shaft 9 a rim 12, and a web 13, connecting the hul) and rim. Formed equi-distant from each other in the rim are five expansion pockets 14, into which expanding gas from exploded gas mixtures in appropriately located explosion chambers, is admitted at predetermined positions of the head. The walls 15, of the pockets present surfaces toward the direction of travel of the head which are adapted to convert the expansive force of the gas into rotary energy against the head, a concave shape being here shown, which is approached by a plane surface 16, in a chord of the peripheral circle of the head.
The rim 12 is also provided with an integral radial lange 17, having a port 18, between each pair of adjacent pockets 14. This ange shuts olf the supply of gas to the explosion chambers except at proper sitions when admission of gas is provide for by a suitably located port of the rotating ange coming into register with a port of a stationary explosion chamber.
The periphery of the rotary head 8, makes a close running lit in an annular band 19, of a fixed housing comprising also a radial flange 20, having a close running fit against the flange 17 of the head. The lian e 20 is bolted to a removable disk 21, whic closes that side of a housing for the rotary head. A web 22, on the other side of the head, is integral with the band 19. The web 22 has a series of openings 23, for the admission of air to the interior of the housing for the purpose of air-cooling the metal of the rotary head surrounding its expansion pockets 14. A positive air-current is insured by the formation of openings in the web 13, each having similarly oblique radial edges 24, 25, which act as vanes, on the principle of a blower to draw in the air and discharge it when the head is rotated.
The explosion chambers 26, here shown as two in number, are located diametrically opposite each other in the angle between the casing-members 19 ad 20, and are pref- Vlatter are successively brought into position opposite an open end of one of said explosion chambers 2G. By providing an odd number of equally spaced expansion chambers with a port 18 between each, and two explosion chambers at opposite sides of the engine, all as here shown, the driving impulses will be exerted on the rotary head at alternate diametrically opposite intervals; and a maximum cooling time will be afforded to the parts which are heated as an accompanying result of the explosions.
By placing the ports in flange 17 of the rotating head proper timing is secured; and leakage between the flange and adjacent gas-passages is prevented by forming an nula-r sockets in the side members bearing said passages, inf which are close-fitting split spring-metal packingrings 2'?, 27, (see Figs. 2 and 4) which bear agalnst said flange 17.
The explosion chambers 26 are closed at their outer ends by removable heads 2S, which support sparking-plugs 29, of usual construction; and, to insure the maximum obtainable air-coolin f efficiency we surround the major portion o' said chamber 26 with a casing 30, having entrance ports from the main housing and discharge ports 31 near their outer ends.
To supplement the ordinary carbureter, or as a substitute in some instances, we provide a fan, in housing 30 of usual construction, which is driven by spur gears 32 and r,33.fr om shaft 9. Gas enters the housing through pipe 34 and is discharged through pipe 35 into manifold 36. The latter has two branches each leading to a respective explosion chamber 26, on each side of the engine. A'damper 35 affords means for regulating the supply of air to the housing 30.
A pop-valve 37 takes from the pipe 25 and has a pipe 38 to return the excess gas mixture to the pipe 34 so none will be wasted.
A magneto 39, operated by gears 40, 41 and 42, from shaft 9, is wired, in the usual `manner to the spark-plugs 29. The magneto has the usual timing device (not shown) for furnishing the required spark at the right time and place. l
Oil cups 43, are provided in suitable proximity to the rotary head 8. These have oilsaturated wicks which wipe the peripher of the head, and the lubricant thus deposited is carried and distributed by the rotating head. This periphery has annular channels 44, in which the surplus oil is drained and deposited by gravity in the lower part of the housing for the rotary head, as shown in Fig. 3. From there it is taken by a pump 45. The pump is driven from the arbor of gear wheel 41, by a belt as shown in Fig. 1. The pump returns the oil to the cups 43, through pipes 46, and any additional quantity needed is taken from an oil tank 47. The journals for shaft 9, and other shafts and rubbing parts are accessible and may be lubricated in any usual and suitable manner.
The exhaust is to chambers 48, 48, on diametrically opposite sides of the rotary head 8, when the respective charged heads reach them, and the spent gas is taken thence through suitable pipes 49 to a muffier (not shown) or wherever desired.
ln the operation of our engine the hydrocarbon mixture is in the branches of the manifold pipe ready to charge one of the explosion chambers when one of the ports in the rotary flange registers and provides the required opening. Then the supply is cut off by the travel of the liange and the charge in the explosion chamber is fired just as the next expansion chamber reaches the opening in the small end of the explosion chamber. The expanding gas enters the expansion chamber as the latter moves on and a further rotation of the head brings the' expansion chamber opposite the exhaust chamber where the spent gas escapes.
Vile have shown and described the construction embodying the principles of our invention now thought to be the best for the purpose intended, but we do not limit ourselves to such construction; on the contrary we hold ourselves at liberty to make such changes as fairly fall within the scope of our invention, and therefore claim as our invention:
1. ln an internal combustion engine, a rotatable member having a plurality of expansion chambers, relatively stationary explosion chambers, means comprising a flange on the rotatable member with ports to supply a hydrocarbon mixture to the explosion chambers, means to ex lode the mixture, means for discharging t e expanding product into the expansion chambers, and means for discharging the spent roduct,
2. In an internal com ustion engine, a rotatable member having a plurality of peripheral cavities and a radial flange with a port opening between each peripheral cavity, a stationary member having an annular band in which the periphery of said rotatable member makes a close running lit, said stationary member also having a fixed radial ange maln'ng a close running fit against the fiange of the rotatable member, one or more explosion chambers fixed in the angle between the annular band and its flange, each chamber having an inlet opening through its ad] acent flange adapted to register with successive port-openings of the rotatable flange and said explosion chambers each having an outlet opening through the annular band of the stationary member whereby communication is established between an explosion chamber and a peripheral cavity when one of said cavities is brought opposite the outlet opening of that chamber by the movement of the rotatable member, means for supplyingi a hydrocarbon mixture to an explosion c amber when the openings in the two flanges register, and means for exploding the mixture.
3. In an internal combustion engine, a rotatable member having a plurality of peripheral cavities and an adjacent radial flange, said iiange having a transverse portopening between each two of said cavities, a fixed explosion chamber having an inlet port closed by said flange except when in registration with a port of the flange and having an outlet opening closed by the rotatable member except when in register with one of the peripheral cavities of said rotatable member, a manifold pipe supplying a hydrocarbon mixture and closed by the rotatable ange except when its openin is in register with a port of the flange, an means for exploding a mixture in the explosion chamber.
4. In an internal combustion engine, a rotatable flange having a plurality of portopenings, an explosion chamber having an inlet port closed by the flange except when in register with a port of the flange, a manifold pipe su plying a hydrocarbon mixture and close by the rotatable flange except when its opening is in register with a port of the flange, and pacln'ng between the flange and explosion chamber and between the flange and manifold pipe to prevent hydrocarbon leakage.
5.In an internal combustion engine, a
rotatable member having peripheral cavities forming explosion chambers and having an adjacent peripheral liange with transverse orts between said cavities, a fixed member aving an annular band and a radial {iange both maln close running fit with the periphery an flange of the rotatable head, respectively, and means for automatically lubricating the rubbing parts.
6. In an internal combustion engine, a rotatable member having peri heral cavities forming expansion chambers, xed explosion chambers, means for creatin air currents by the rotation of the rotatab e member and means for subjecting said chambers to the cooling action of the air currents.
7 A rotary member for internal combustion engines having peripheral cavities forming explosion chambers and a peripheral flange with transverse ports between the cavities in combination with a fixed member having expansion chambers discharging into the cavities of the rotary member as the cavities come opposite, and means for supplying a hydrocarbon element to the expansion chambers through the ports in the peripheral flange.
8. A rotary member for internal combustion'engines. having peripheral cavities formexplosion chambers, annular peripheral oilruns, and a peripheral lian e with transverse ports between the cavities in combination with va fixed member having ex ansion chambers discharging into the cavities of the rotary member as the cavities come opposite, and means for supplying a hydro carbon element to the expanslon chambers throulgh the ports in the peripheral flange.
9. fixed member for internal combustion engines having one or more explosion chambers and one or more exhaust outlets, in combination with a rotary member having peripheral cavities which are successively brought into communication with said explosion chambers, and a flange with transverse ports between said cavities through which a hydrocarbon element is supplied to said explosion chambers.
In wltness whereof we have hereunto set our hands at Indianapolis, Indiana, this 25th day of October, 1919.
GOTTLOB F. SCHMID.` KARL Q.. SCHMID.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US334590A US1340563A (en) | 1919-10-30 | 1919-10-30 | Turbine gas-engine |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US334590A US1340563A (en) | 1919-10-30 | 1919-10-30 | Turbine gas-engine |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| US1340563A true US1340563A (en) | 1920-05-18 |
Family
ID=23307905
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| US334590A Expired - Lifetime US1340563A (en) | 1919-10-30 | 1919-10-30 | Turbine gas-engine |
Country Status (1)
| Country | Link |
|---|---|
| US (1) | US1340563A (en) |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2479143A (en) * | 1944-12-07 | 1949-08-16 | Jr Samuel W Traylor | Gas turbine |
| US2680949A (en) * | 1951-10-18 | 1954-06-15 | Butler Frank David | Internal-combustion turbine having rotating combustion chambers |
| US3040530A (en) * | 1959-05-14 | 1962-06-26 | Yalnizyan Puzant | Rotary external combustion engine |
-
1919
- 1919-10-30 US US334590A patent/US1340563A/en not_active Expired - Lifetime
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2479143A (en) * | 1944-12-07 | 1949-08-16 | Jr Samuel W Traylor | Gas turbine |
| US2680949A (en) * | 1951-10-18 | 1954-06-15 | Butler Frank David | Internal-combustion turbine having rotating combustion chambers |
| US3040530A (en) * | 1959-05-14 | 1962-06-26 | Yalnizyan Puzant | Rotary external combustion engine |
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