US800684A - Rotary hydrocarbon-engine. - Google Patents
Rotary hydrocarbon-engine. Download PDFInfo
- Publication number
- US800684A US800684A US17672003A US1903176720A US800684A US 800684 A US800684 A US 800684A US 17672003 A US17672003 A US 17672003A US 1903176720 A US1903176720 A US 1903176720A US 800684 A US800684 A US 800684A
- Authority
- US
- United States
- Prior art keywords
- chamber
- piston
- casing
- port
- charge
- Prior art date
- 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
- 239000002360 explosive Substances 0.000 description 6
- 239000007789 gas Substances 0.000 description 4
- 230000002441 reversible effect Effects 0.000 description 4
- 238000010276 construction Methods 0.000 description 2
- 238000004880 explosion Methods 0.000 description 2
- 239000000203 mixture Substances 0.000 description 2
- 239000004215 Carbon black (E152) Substances 0.000 description 1
- 241000005139 Lycium andersonii Species 0.000 description 1
- 230000000881 depressing effect Effects 0.000 description 1
- 229930195733 hydrocarbon Natural products 0.000 description 1
- 150000002430 hydrocarbons Chemical class 0.000 description 1
- 238000012856 packing Methods 0.000 description 1
- 230000002093 peripheral effect Effects 0.000 description 1
- 230000013707 sensory perception of sound Effects 0.000 description 1
- 239000007921 spray 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
- F02C9/00—Controlling gas-turbine plants; Controlling fuel supply in air- breathing jet-propulsion plants
- F02C9/26—Control of fuel supply
- F02C9/42—Control of fuel supply specially adapted for the control of two or more plants simultaneously
Definitions
- Fig. i asection on the line 4 1, Fig. 1; Fig. 5, an elevation showing two engines arranged to secure reversing means.
- the piston has a plurality of explosion-chambers
- the casing A is'cylindrical, with hollow walls forming a water-jacket 2
- the piston has a peripheral circular rib 4: at the edge of a disk 3, with a central hub mounted fixedly on the driving-shaft 5, which extends through bring the chamber 6 opposite the inlet-port 7.
- the piston there is a plurality of explosion-chambers 6, although but a single chamber may be used, the said chambers being tangential and each closed at the inner end and opening at, the periphery of the piston, so as to be brought successively opposite an inlet-port7 andthen opposite one or more outlet-ports 8 in the easingA, and between these two ports is arranged or operated. igniting means whereby the charge introduced into the-chamber through the inlet-portds exploded and thereafter escapes through the outlet port or ports on the further revolution of the piston.
- exhaust-ports are-.radial and arranged so as to permit the complete escape of the gases after they have sufiiciently expanded' and before the piston hasrotated to Specification of Letters Patent. Application filed October 12, 1903- Serial No. 176,720.
- Any suitable means may be employed for forming an explosive mixture, and the same may be introduced into the chamber by any of the usual means for combining and inject: ing a hydrocarbon and air or any other character of explosive charge.
- a supplypipe 10 communicates with a chamber 9, formed in the casing A, and this chamber communicates with the inlet-port 7 through a port 12, controlled by a valve 13. This permits the chamber 9 to receive a proper volume'of mixture under high pressure, which can flow suddenly into the chamber upon opening the valve 13.
- valve 13 is upon a stem 14, which is forced inward on rocking a lever 15, operated in any suitable manner from the shaft 5as, for instance, by cams 16, acting upon a guided rod 17, connected to the lever 15, a spring 18 acting to reverse the rocking of the lever and close the valve.
- the igniting means may be carried either by the piston or casing, the latter arrangement being shown and consistingof an electrical igniter C, extending into the chamber 00 and having electrodes carried out .of contact by means of a cam 20 upon a rock-shaft 21, operated by a cams 22, acting upon a guided rod 23, bearing upon a lug on the shaft. 21, and by rocking the latter depressing one of the electrodes to carry it out of contact with the other suddenly, aspring 24 serving to lift the electrode into contact after the explosion.
- antifriction-balls 27 between the piston and the casing, so arranged as to take the direct bearing of the piston from the casing.
- the chamber may have a rear port 40, which when the chamber is in position to receive anew charge may communicate with the port/11 1n the casing,
- this latter port being of-such a length that the port 40 will be closed before the new charge has. passed entirely to the end of the chamber.
- the engine as thus described is capable of acting only in one direction. in order to reverse,ll make use of a second engine A, Fig. 5,
- the second engine has an inlet-pipe 30, and each inlet-pipe 10 30 has a valve 31, and the stems of the two valves are connected by a link 32 in such manner that when one valve is open the other will be closed. It is therefore only necessary to shift the link 32, which may be done by a hand-lever 33, in order to throw the supply from one engine to the other, when the exploding charges will act with a reverse effect.
- the piston of the engine which is notoperating constitutes practically a iiy-wheel for the shaft 5 and for the engine which is operated.
- compressed air from the pipe 10 may pass to the channel communicating with the port 7, and oil may be admitted to said channel from a pipe 50, communicating with a port 51.
- This port is controlled by a valve 52., moved from the cams 22 through a rod 53 and lever 44, a spring 55 tending to shift the parts to close the valve.
- a motor having a casing, a cylindrical piston mounted to revolve therein and 'provided with a tangential chamber open at the periphery, means for introducing an explosive charge into said chamber at one point of the revolution of the piston, and means for exploding the charge at another point of said revolution, substantially as set forth.
- a motor having a casing, a cylindrical piston mounted to revolve therein and provided with a tangential chamber open at the periphery, means for introducing an explosive charge into said chamber at one point of the revolution of the piston, means for exploding the charge at another point of said revolution, and a recess or recesses in the casing at the point where the charge is exploded, substantially as set forth.
- a motor having a casing, a cylindrical piston mounted to revolve therein and provided with a plurality of tangential chambers open at the periphery, means for introducing w an explosive charge into said chambers in succession at one point of the revolution of the piston, means for exploding each charge at another point of said revolution, and an. ex-
- a motor having a casing, a cylindrical piston mounted to revolve therein and provided with a tangential chamber, open at the periphery, an inlet-port in the casing arranged to communicate with the chamber at one'point of the revolution of the piston, an outlet-port in the casing at another point, and means for exploding the charge in the chamber between said two ports, substantially as set forth.
- a motor having a casing, a cylindrical piston mounted to revolve therein and provided with a tangential chamber open at the periphery,-an inlet-port in the casing arranged to communicate with the chamber at one point of the revolution of the piston, an outlet-port in the casing at another .point, means for ex- .ploding the charge in the chamber between said two ports, and a Valve controlling the advmission of the charge to the inlet-port, substantially as set forth.
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- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Portable Nailing Machines And Staplers (AREA)
Description
No. 800,684. PATENTED OCT. 3, 1905.
W. E. SCHNEIDER. ROTARY HYDROGARBON ENGINE.
APPLICATION FILED 00T.12, 1903.
2 BHEETS-SHEET 1.
No. 800,684. PATBNTED OCT. 3, 1905. W; E. SCHNEIDER.
ROTARY HYDBOGARBON ENGINE.
APPLICATION FILED OGT.12,1903.
2 SHEETS-SHEET 2.
- ifiz f omwagw' iim'rnn srA'r s *iPArnN'r ori ice;-
WILLIAM E. SCHNEIDER, or WASHINGTON, DISTRICT OF COLUMBIA.
RQTARY erosooaeeow eneme.
- No. s'oo,es4.
To aZZ whom, it may concern;
Be it known that LWILLIA E. Sormnmnn,
' a citizen. of the United States, residing at Washington, in the District of Oolu mbia, have invented certain new and useful Improvements in Rotary Hydrocarbon-Engines, of which the following is a specification.
of the valve-operating parts; Fig. i, asection on the line 4 1, Fig. 1; Fig. 5, an elevation showing two engines arranged to secure reversing means. a
- In the preferred form of construction shown the piston has a plurality of explosion-chambers, the casing A is'cylindrical, with hollow walls forming a water-jacket 2, and the piston has a peripheral circular rib 4: at the edge of a disk 3, with a central hub mounted fixedly on the driving-shaft 5, which extends through bring the chamber 6 opposite the inlet-port 7.
hearings in the cylinder." In the piston, as shown, there is a plurality of explosion-chambers 6, although but a single chamber may be used, the said chambers being tangential and each closed at the inner end and opening at, the periphery of the piston, so as to be brought successively opposite an inlet-port7 andthen opposite one or more outlet-ports 8 in the easingA, and between these two ports is arranged or operated. igniting means whereby the charge introduced into the-chamber through the inlet-portds exploded and thereafter escapes through the outlet port or ports on the further revolution of the piston. ;As the chamber is tangential, the explosion of the charge therein acting against the inner end of the chamber and against the opposing face of the interior of the casing tends to force the piston around in the direction of its arrow, and to afford a better abutment for this'a etion I form a recess w in the inner face of the casing with faces so stepped or arranged as to afford abutments or pressure-faces against which the gases may act as the piston rotates.
As' shown, the "exhaust-ports are-.radial and arranged so as to permit the complete escape of the gases after they have sufiiciently expanded' and before the piston hasrotated to Specification of Letters Patent. Application filed October 12, 1903- Serial No. 176,720.
Patented Oct. 3, 1905...
Any suitable means may be employed for forming an explosive mixture, and the same may be introduced into the chamber by any of the usual means for combining and inject: ing a hydrocarbon and air or any other character of explosive charge. As shown, a supplypipe 10 communicates with a chamber 9, formed in the casing A, and this chamber communicates with the inlet-port 7 through a port 12, controlled by a valve 13. This permits the chamber 9 to receive a proper volume'of mixture under high pressure, which can flow suddenly into the chamber upon opening the valve 13. As shown, the valve 13 is upon a stem 14, which is forced inward on rocking a lever 15, operated in any suitable manner from the shaft 5as, for instance, by cams 16, acting upon a guided rod 17, connected to the lever 15, a spring 18 acting to reverse the rocking of the lever and close the valve. i
The igniting means may be carried either by the piston or casing, the latter arrangement being shown and consistingof an electrical igniter C, extending into the chamber 00 and having electrodes carried out .of contact by means of a cam 20 upon a rock-shaft 21, operated by a cams 22, acting upon a guided rod 23, bearing upon a lug on the shaft. 21, and by rocking the latter depressing one of the electrodes to carry it out of contact with the other suddenly, aspring 24 serving to lift the electrode into contact after the explosion.
It will be evident that buta single igniter is required for any number of chambers, it
only being necessary to provide a number of hers.
In order to prevent the escape of gases, the annular head'of the piston 1s recessed to recams 22 corresponding to the number of chamceive annular packings 25, as shown.
In order to-reduce friction, there may be antifriction-balls 27 between the piston and the casing, so arranged as to take the direct bearing of the piston from the casing.
' In some cases it is desirable to allow the spent gases to be forced-out of the rear of the chamber as a new charge is introduced at the front, and to permit this the chamber may have a rear port 40, which when the chamber is in position to receive anew charge may communicate with the port/11 1n the casing,
' this latter port being of-such a length that the port 40 will be closed before the new charge has. passed entirely to the end of the chamber.
The engine as thus described is capable of acting only in one direction. in order to reverse,ll make use of a second engine A, Fig. 5,
of the same character as the first, except that the piston secured to the same shaft 5 has the chamber or chambers 6 open in the opposite direction. The second engine has an inlet-pipe 30, and each inlet-pipe 10 30 has a valve 31, and the stems of the two valves are connected by a link 32 in such manner that when one valve is open the other will be closed. It is therefore only necessary to shift the link 32, which may be done by a hand-lever 33, in order to throw the supply from one engine to the other, when the exploding charges will act with a reverse effect. it will be seen that the piston of the engine which is notoperating constitutes practically a iiy-wheel for the shaft 5 and for the engine which is operated.
In order to start the engine in the first place and bring the chamber 6 into proper position to receive the charge and then into position to cause the charge to be exploded, some means should be provided for readily turning 5 the shaft 5as, for instance, a ratchet 34 on the shaft engaged by a pawl 35, carried by a lever 36, which swings upon a shaft, or any other suitable means may be employed.
When it is desired to spray the oil into the cylinder, compressed air from the pipe 10 may pass to the channel communicating with the port 7, and oil may be admitted to said channel from a pipe 50, communicating with a port 51. This port is controlled by a valve 52., moved from the cams 22 through a rod 53 and lever 44, a spring 55 tending to shift the parts to close the valve.
Without limiting myself to the precise construction shown, I claim- 1. A motor having a casing, a cylindrical piston mounted to revolve therein and 'provided with a tangential chamber open at the periphery, means for introducing an explosive charge into said chamber at one point of the revolution of the piston, and means for exploding the charge at another point of said revolution, substantially as set forth.
2. A motorhaving a casing, a cylindrical piston mounted to revolve therein and provided with a tangential chamber open at the periphery, means for introducing an explosive charge into said chamber at one point of the revolution of the piston, means for exploding the charge at another point of said revolution, and a recess or recesses in the casing at the point where the charge is exploded, substantially as set forth.
3. A motor having a casing, a cylindrical piston mounted to revolve therein and provided with a plurality of tangential chambers open at the periphery, means for introducing w an explosive charge into said chambers in succession at one point of the revolution of the piston, means for exploding each charge at another point of said revolution, and an. ex-
scones hanst-port beyond the point where the charge is exploded, substantially as set forth.
t. A motor having a casing, a cylindrical piston mounted to revolve therein and provided with a tangential chamber, open at the periphery, an inlet-port in the casing arranged to communicate with the chamber at one'point of the revolution of the piston, an outlet-port in the casing at another point, and means for exploding the charge in the chamber between said two ports, substantially as set forth.
5. A motor having a casing, a cylindrical piston mounted to revolve therein and provided with a tangential chamber open at the periphery,-an inlet-port in the casing arranged to communicate with the chamber at one point of the revolution of the piston, an outlet-port in the casing at another .point, means for ex- .ploding the charge in the chamber between said two ports, and a Valve controlling the advmission of the charge to the inlet-port, substantially as set forth.
!mission of the charge to theinlet-port, sub- Z stantially as set forth.
7. The combination with the casing, rotat-' ing piston having a tangential chamber and =i means for supplying a charge to said cham- :ber, of a rear port in the piston and a port in ithe casing arranged to correspond with the 5 port in the piston-when the chamber is receiv i mg a new charge, substantially as set forth.
8. The combination of the casing, shaft, pi-s- I ton having a tangential chamber open at the 6, A motor having a casing, a cylindrical 7 outer end, means for introducing explosive 1 charges into and subsequently exploding them in said chamber, and means for rotating the shaft from'outside the casing, substantially as set forth.
9. The combination in a reversible engine, of a shaft carrying two pistons with tangential explosion-chambers reversely arranged, a
E. Wanninnn.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US17672003A US800684A (en) | 1903-10-12 | 1903-10-12 | Rotary hydrocarbon-engine. |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US17672003A US800684A (en) | 1903-10-12 | 1903-10-12 | Rotary hydrocarbon-engine. |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| US800684A true US800684A (en) | 1905-10-03 |
Family
ID=2869170
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| US17672003A Expired - Lifetime US800684A (en) | 1903-10-12 | 1903-10-12 | Rotary hydrocarbon-engine. |
Country Status (1)
| Country | Link |
|---|---|
| US (1) | US800684A (en) |
Cited By (26)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2517997A (en) * | 1946-04-25 | 1950-08-08 | Charles C Fredericks | Power-driven mixer |
| US2529787A (en) * | 1945-05-12 | 1950-11-14 | Shepelrich Anton | Oil driven turbine motor vehicle wheel |
| US2549308A (en) * | 1945-08-24 | 1951-04-17 | Stanley E Harris | Fluid torque converter |
| US2555314A (en) * | 1946-07-10 | 1951-06-05 | William L Buckley | Mud driven apparatus for treating mud |
| US2608058A (en) * | 1946-06-10 | 1952-08-26 | Leon J Geeraert | Combustion chamber with sliding valve controlling fuel, air, and water admission |
| US2608379A (en) * | 1946-12-14 | 1952-08-26 | Lester C Wales | Water wheel |
| US2643852A (en) * | 1950-01-09 | 1953-06-30 | Us Air Force | High-speed turbine |
| US2898736A (en) * | 1957-05-06 | 1959-08-11 | Robert F Ely | Plural combustion products generators in ring coaxial with a turbine |
| US2942687A (en) * | 1956-11-15 | 1960-06-28 | Melvin M Kollander | Centrifugal separator for exhaust gases |
| US3074687A (en) * | 1960-10-28 | 1963-01-22 | Harry A Garrison | Reversible hydraulic power unit |
| US3082602A (en) * | 1958-06-04 | 1963-03-26 | Hogguer Fredrik Jeremias | Rotary internal combustion engine |
| US3089307A (en) * | 1960-06-17 | 1963-05-14 | Melvin M Kollander | Rotary jet engine |
| US3094840A (en) * | 1959-10-13 | 1963-06-25 | Hogguer Fredrik Jeremias | Internal combustion engine having a rotary piston arranged eccentrically on a shaft |
| US3225539A (en) * | 1962-06-20 | 1965-12-28 | George C Coverston | Explosion inertia turbine engine |
| US3302741A (en) * | 1963-04-08 | 1967-02-07 | Brazuk John | Fluid drive system for vehicles |
| US3463127A (en) * | 1968-01-12 | 1969-08-26 | Gifford W Chester | Rotary combustion engine |
| US3522703A (en) * | 1968-01-02 | 1970-08-04 | Ferenc Toth | Multistage tangential turbine |
| US4027995A (en) * | 1975-07-14 | 1977-06-07 | Berry Clyde F | Steam track turbine |
| US4209983A (en) * | 1979-03-26 | 1980-07-01 | Benjamin Sokol | Internal electric explosion engine |
| AT389569B (en) * | 1988-05-05 | 1989-12-27 | Lukatsch Johann | INTERNAL COMBUSTION ENGINE WITH ROTOR |
| US20060207546A1 (en) * | 2005-03-18 | 2006-09-21 | Bechtel Paul Y | Engine system |
| US20080029059A1 (en) * | 2006-08-03 | 2008-02-07 | Arthur Isbrecht | Rotary Internal Combustion Engine with a Circular Rotor |
| US20080141974A1 (en) * | 2005-03-18 | 2008-06-19 | Bechtel Paul Y | Rotary engine system |
| US20120312274A1 (en) * | 2010-02-24 | 2012-12-13 | Rocco Luigi Bubbico | Rotary type internal combustion engine |
| US10871105B1 (en) * | 2019-05-29 | 2020-12-22 | Maynard MOORE | Rotating internal combustion engine |
| WO2022191728A1 (en) * | 2021-03-12 | 2022-09-15 | Lita Dan Lucescu | Rotative engine |
-
1903
- 1903-10-12 US US17672003A patent/US800684A/en not_active Expired - Lifetime
Cited By (27)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2529787A (en) * | 1945-05-12 | 1950-11-14 | Shepelrich Anton | Oil driven turbine motor vehicle wheel |
| US2549308A (en) * | 1945-08-24 | 1951-04-17 | Stanley E Harris | Fluid torque converter |
| US2517997A (en) * | 1946-04-25 | 1950-08-08 | Charles C Fredericks | Power-driven mixer |
| US2608058A (en) * | 1946-06-10 | 1952-08-26 | Leon J Geeraert | Combustion chamber with sliding valve controlling fuel, air, and water admission |
| US2555314A (en) * | 1946-07-10 | 1951-06-05 | William L Buckley | Mud driven apparatus for treating mud |
| US2608379A (en) * | 1946-12-14 | 1952-08-26 | Lester C Wales | Water wheel |
| US2643852A (en) * | 1950-01-09 | 1953-06-30 | Us Air Force | High-speed turbine |
| US2942687A (en) * | 1956-11-15 | 1960-06-28 | Melvin M Kollander | Centrifugal separator for exhaust gases |
| US2898736A (en) * | 1957-05-06 | 1959-08-11 | Robert F Ely | Plural combustion products generators in ring coaxial with a turbine |
| US3082602A (en) * | 1958-06-04 | 1963-03-26 | Hogguer Fredrik Jeremias | Rotary internal combustion engine |
| US3094840A (en) * | 1959-10-13 | 1963-06-25 | Hogguer Fredrik Jeremias | Internal combustion engine having a rotary piston arranged eccentrically on a shaft |
| US3089307A (en) * | 1960-06-17 | 1963-05-14 | Melvin M Kollander | Rotary jet engine |
| US3074687A (en) * | 1960-10-28 | 1963-01-22 | Harry A Garrison | Reversible hydraulic power unit |
| US3225539A (en) * | 1962-06-20 | 1965-12-28 | George C Coverston | Explosion inertia turbine engine |
| US3302741A (en) * | 1963-04-08 | 1967-02-07 | Brazuk John | Fluid drive system for vehicles |
| US3522703A (en) * | 1968-01-02 | 1970-08-04 | Ferenc Toth | Multistage tangential turbine |
| US3463127A (en) * | 1968-01-12 | 1969-08-26 | Gifford W Chester | Rotary combustion engine |
| US4027995A (en) * | 1975-07-14 | 1977-06-07 | Berry Clyde F | Steam track turbine |
| US4209983A (en) * | 1979-03-26 | 1980-07-01 | Benjamin Sokol | Internal electric explosion engine |
| AT389569B (en) * | 1988-05-05 | 1989-12-27 | Lukatsch Johann | INTERNAL COMBUSTION ENGINE WITH ROTOR |
| US20060207546A1 (en) * | 2005-03-18 | 2006-09-21 | Bechtel Paul Y | Engine system |
| US20080141974A1 (en) * | 2005-03-18 | 2008-06-19 | Bechtel Paul Y | Rotary engine system |
| US20080029059A1 (en) * | 2006-08-03 | 2008-02-07 | Arthur Isbrecht | Rotary Internal Combustion Engine with a Circular Rotor |
| US20120312274A1 (en) * | 2010-02-24 | 2012-12-13 | Rocco Luigi Bubbico | Rotary type internal combustion engine |
| US8763358B2 (en) * | 2010-02-24 | 2014-07-01 | Rocco Luigi Bubbico | Rotary type internal combustion engine |
| US10871105B1 (en) * | 2019-05-29 | 2020-12-22 | Maynard MOORE | Rotating internal combustion engine |
| WO2022191728A1 (en) * | 2021-03-12 | 2022-09-15 | Lita Dan Lucescu | Rotative engine |
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