US1653877A - Explosion engine - Google Patents
Explosion engine Download PDFInfo
- Publication number
- US1653877A US1653877A US77586A US7758625A US1653877A US 1653877 A US1653877 A US 1653877A US 77586 A US77586 A US 77586A US 7758625 A US7758625 A US 7758625A US 1653877 A US1653877 A US 1653877A
- Authority
- US
- United States
- Prior art keywords
- pressure
- cylinders
- piston
- maximum
- admission
- 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
- 238000004880 explosion Methods 0.000 title description 3
- 210000000038 chest Anatomy 0.000 description 7
- 238000002485 combustion reaction Methods 0.000 description 3
- 230000000694 effects Effects 0.000 description 2
- 239000000446 fuel Substances 0.000 description 2
- 239000007789 gas Substances 0.000 description 2
- 230000006835 compression Effects 0.000 description 1
- 238000007906 compression Methods 0.000 description 1
- 230000001276 controlling effect Effects 0.000 description 1
- 230000001419 dependent effect Effects 0.000 description 1
- 230000001105 regulatory effect Effects 0.000 description 1
- 239000011435 rock Substances 0.000 description 1
Images
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02D—CONTROLLING COMBUSTION ENGINES
- F02D9/00—Controlling engines by throttling air or fuel-and-air induction conduits or exhaust conduits
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02D—CONTROLLING COMBUSTION ENGINES
- F02D2700/00—Mechanical control of speed or power of a single cylinder piston engine
- F02D2700/02—Controlling by changing the air or fuel supply
- F02D2700/0217—Controlling by changing the air or fuel supply for mixture compressing engines using liquid fuel
- F02D2700/0225—Control of air or mixture supply
- F02D2700/0228—Engines without compressor
- F02D2700/023—Engines without compressor by means of one throttle device
- F02D2700/0235—Engines without compressor by means of one throttle device depending on the pressure of a gaseous or liquid medium
Definitions
- This invention relates to means for restricting automatically the supply of fuel in internal combustion engines, more particularly those of aircraft.
- Some aircraft engines are either designed and constructed for normal running above a certain altitude, or are provided, for the same purpose, with special accessories such as supercharging compressors, but they cannot, without inconvenience, be run under full admission, or with the full supercharg'e of the compressor, at altitudes lower than the normal running, altitudes; and they are, therefore, fitted with means for automatically restricting the supply of fuel, in order to avoid excessive strain on their members when the engines are running at such lower altitudes.
- the present invention has for its object to enable much greater variations in energy to be accomplished, for which purpose the a ,maximum admission into the cylinders is regulated by the maximum pressure prevail ing therein, so that said pressure cannot ex ceed a certain value, whatever be the conditions under which the engine is running.
- the rod '11 of the piston 97 is connected with the admis- S1011 members (not shown) of the cylinders by any suitable mechanism.
- the piston 9 may, of course, be replaced by any other member adapted to move under the action of the pressure. After a short running time, the pressure in the chests a assumes a constant value de pendent of the maximum pressure set up, at each cycle,'in the cylinders Z), since the valves 0 allow the gases under pressure to enter the chests a, but prevent their return to the cylinders 6.
- the pressure in the latter after a short running time, will also assume the maximum pressure in the cylinders b.
- the very small orifice 7, through which the gases escape to the outside, enables a balance to be attained between the pressures in the chamber 6 and chests a and the ma: imum pressure in the cylinders b, in the event of a drop in the normal workmg pressure in the latter.
- the stem 2' 1s connected, by means of a rock lever 7' and a link 70, with a lever Z attached to a valve m placed in the conduit a leading from the carburetter (not shown) to the admission valves 39 of. the cylinders.
- the lever j is also connected by a lever g to the hand lever 9" which is of any well known type adapted to be operated by the driver.
- an intake manifold 21 throttle valve therein and a control member for said throttle valve responsive to the maximum pressure in said cylinders, including a cylinder, 9. piston therein operatively connected to said throttle valve, a constant tension spring on one side of said piston biasing the latter in the direction to open said throttle valve, the other side of said piston being biased in the opposite direction by the maximum cylinder pressure.
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- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Output Control And Ontrol Of Special Type Engine (AREA)
Description
Dec. 27, 1927. 1,653,877
A. SCHAFF EXPLOSION ENGINE Filed Dec. 24. 1925 Patented Dec. 27, 1927.
UNITED STATES ALBERT SCHAFF, OF PARIS,
EXPLOSION ENGINE.
Application filed December 24, 1925, Serial No. 77,586, and in France September 11, 1925.
This invention relates to means for restricting automatically the supply of fuel in internal combustion engines, more particularly those of aircraft. Some aircraft engines are either designed and constructed for normal running above a certain altitude, or are provided, for the same purpose, with special accessories such as supercharging compressors, but they cannot, without inconvenience, be run under full admission, or with the full supercharg'e of the compressor, at altitudes lower than the normal running, altitudes; and they are, therefore, fitted with means for automatically restricting the supply of fuel, in order to avoid excessive strain on their members when the engines are running at such lower altitudes.
For effecting the automatic restriction of the maximum admission, most of the ap* plianccs constructed for this purpose employ an apparatus which is sensitive to variations in atmospheric pressure, but these only produce variations in energy which are relatively slight and, in certain cases, are incapable of overcoming the passive resistance of the devices controlling the admission to the engine.
The present invention has for its object to enable much greater variations in energy to be accomplished, for which purpose the a ,maximum admission into the cylinders is regulated by the maximum pressure prevail ing therein, so that said pressure cannot ex ceed a certain value, whatever be the conditions under which the engine is running.
The accompanying drawing illustrates, diagrammatically and by way of example, a device for carrying out the invention shown in plan view and partly in section.
For carrying out the invention, use is made of apparatus of known type arranged in such a way as to be subjected to the maxi mum pressure produced in an internal combustion engine running under normal conditions. These known apparatus consist of small chests a, each of which is in communication with the compression chamber of a cylinder Z) by means of a valve 0, or similar member, opening outwardly of the cylinder 6, against the pressure of a spring 0 Tubes connect the chests a with one another and with a cylindrical chamber e formed with an orifice f opening into the atmosphere, said chamber e having slidable therein a piston g balanced by a spring h,
a value dependent on of the piston g regulate the of such a kind that the maximum movements the plston is intended to describe will have no notable effect on its tension. The rod '11 of the piston 97 is connected with the admis- S1011 members (not shown) of the cylinders by any suitable mechanism. The piston 9 may, of course, be replaced by any other member adapted to move under the action of the pressure. After a short running time, the pressure in the chests a assumes a constant value de pendent of the maximum pressure set up, at each cycle,'in the cylinders Z), since the valves 0 allow the gases under pressure to enter the chests a, but prevent their return to the cylinders 6. Owing to the communication between these chests and the cylindrical chamber 6, the pressure in the latter, after a short running time, will also assume the maximum pressure in the cylinders b. The very small orifice 7, through which the gases escape to the outside, enables a balance to be attained between the pressures in the chamber 6 and chests a and the ma: imum pressure in the cylinders b, in the event of a drop in the normal workmg pressure in the latter. The movements admission to the engine cylinders b. For this purpose, the stem 2' 1s connected, by means of a rock lever 7' and a link 70, with a lever Z attached to a valve m placed in the conduit a leading from the carburetter (not shown) to the admission valves 39 of. the cylinders. The lever j is also connected by a lever g to the hand lever 9" which is of any well known type adapted to be operated by the driver.
When the stem 2' moves to the right under of piston g the effect of the maximum pressure in the cylinders b causing a certain pressure to prevail in the cylinder e, the valve m can no longer be moved, by means of the hand lever r, to a position parallel to the axis of conduit n. and therefore the maximum admission of the combustiblemixture through conduit n to the valves of the cylinders 25 is reduced. The reverse occurs when the stem 2' of the piston 'g'moves to the left. The control of the maximum admission by the pressure in the cylinder 6 is thus obtained.
The above connections were only given by way of illustration and may be modified it the control device formed by the chests a and the cylinder e is employed with any other system of admission to the engine cylinders. The device is of course applicable to any number of cylinders.
What is claimed is:
1. In a multi-cylinder internal combustion engine, an intake manifold, 21 throttle valve therein and a control member for said throttle valve responsive to the maximum pressure in said cylinders, including a cylinder, 9. piston therein operatively connected to said throttle valve, a constant tension spring on one side of said piston biasing the latter in the direction to open said throttle valve, the other side of said piston being biased in the opposite direction by the maximum cylinder pressure.
stant pressure on one side of the piston biasing it in a direction to open said throttle valve, the other side of said piston being biased in the opposite direction by the maximum cylinder pressure.
In testimony whereof I have signed my name to this specification.
ALBERT SCHAFF.
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| FR1653877X | 1925-09-11 |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| US1653877A true US1653877A (en) | 1927-12-27 |
Family
ID=9679923
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| US77586A Expired - Lifetime US1653877A (en) | 1925-09-11 | 1925-12-24 | Explosion engine |
Country Status (1)
| Country | Link |
|---|---|
| US (1) | US1653877A (en) |
Cited By (9)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3822681A (en) * | 1972-09-05 | 1974-07-09 | Townsend Engineering Co | Rotary internal combustion engine |
| US3857372A (en) * | 1972-09-05 | 1974-12-31 | Townsend Engineering Co | Rotary internal combustion engine |
| US4023536A (en) * | 1972-09-05 | 1977-05-17 | Townsend Engineering Company | Method of controlling the timing of ignition in an internal combustion engine |
| US4322948A (en) * | 1978-09-30 | 1982-04-06 | Volkswagenwerk Aktiengesellschaft | Internal combustion engine with an exhaust-driven turbocharger |
| US4372119A (en) * | 1979-10-29 | 1983-02-08 | Saab-Scania Aktiebolag | Method of avoiding abnormal combination in an internal combination engine and an arrangement for carrying out the method |
| US4426985A (en) | 1980-09-26 | 1984-01-24 | Kanesaka Technical Institute Ltd. | Supercharged internal combustion engine |
| US4446833A (en) * | 1981-12-07 | 1984-05-08 | Yamaha Hatsudoki Kabushiki Kaisha | Fuel injection apparatus for an internal combustion engine |
| US4516401A (en) * | 1983-11-04 | 1985-05-14 | General Motors Corporation | Supercharged engine charge control |
| US5284118A (en) * | 1991-12-12 | 1994-02-08 | Yamaha Hatsudoki Kabushiki Kaisha | Fuel injection control system for internal combustion engine |
-
1925
- 1925-12-24 US US77586A patent/US1653877A/en not_active Expired - Lifetime
Cited By (9)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3822681A (en) * | 1972-09-05 | 1974-07-09 | Townsend Engineering Co | Rotary internal combustion engine |
| US3857372A (en) * | 1972-09-05 | 1974-12-31 | Townsend Engineering Co | Rotary internal combustion engine |
| US4023536A (en) * | 1972-09-05 | 1977-05-17 | Townsend Engineering Company | Method of controlling the timing of ignition in an internal combustion engine |
| US4322948A (en) * | 1978-09-30 | 1982-04-06 | Volkswagenwerk Aktiengesellschaft | Internal combustion engine with an exhaust-driven turbocharger |
| US4372119A (en) * | 1979-10-29 | 1983-02-08 | Saab-Scania Aktiebolag | Method of avoiding abnormal combination in an internal combination engine and an arrangement for carrying out the method |
| US4426985A (en) | 1980-09-26 | 1984-01-24 | Kanesaka Technical Institute Ltd. | Supercharged internal combustion engine |
| US4446833A (en) * | 1981-12-07 | 1984-05-08 | Yamaha Hatsudoki Kabushiki Kaisha | Fuel injection apparatus for an internal combustion engine |
| US4516401A (en) * | 1983-11-04 | 1985-05-14 | General Motors Corporation | Supercharged engine charge control |
| US5284118A (en) * | 1991-12-12 | 1994-02-08 | Yamaha Hatsudoki Kabushiki Kaisha | Fuel injection control system for internal combustion engine |
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