GB1480247A - Combination engine and air compressor - Google Patents

Combination engine and air compressor

Info

Publication number
GB1480247A
GB1480247A GB2718274A GB2718274A GB1480247A GB 1480247 A GB1480247 A GB 1480247A GB 2718274 A GB2718274 A GB 2718274A GB 2718274 A GB2718274 A GB 2718274A GB 1480247 A GB1480247 A GB 1480247A
Authority
GB
United Kingdom
Prior art keywords
valve
cam
engine
cylinders
shaft
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
Application number
GB2718274A
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Individual
Original Assignee
Individual
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Priority claimed from JP48070559A external-priority patent/JPS5020148A/ja
Priority claimed from JP48074536A external-priority patent/JPS5022313A/ja
Priority claimed from JP7626973A external-priority patent/JPS5022909A/ja
Application filed by Individual filed Critical Individual
Publication of GB1480247A publication Critical patent/GB1480247A/en
Expired legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04BPOSITIVE-DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS
    • F04B39/00Component parts, details, or accessories, of pumps or pumping systems specially adapted for elastic fluids, not otherwise provided for in, or of interest apart from, groups F04B25/00 - F04B37/00
    • F04B39/08Actuation of distribution members
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01LCYCLICALLY OPERATING VALVES FOR MACHINES OR ENGINES
    • F01L13/00Modifications of valve-gear to facilitate reversing, braking, starting, changing compression ratio, or other specific operations
    • F01L13/06Modifications of valve-gear to facilitate reversing, braking, starting, changing compression ratio, or other specific operations for braking
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02DCONTROLLING COMBUSTION ENGINES
    • F02D17/00Controlling engines by cutting out individual cylinders; Rendering engines inoperative or idling
    • F02D17/02Cutting-out
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04BPOSITIVE-DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS
    • F04B41/00Pumping installations or systems specially adapted for elastic fluids
    • F04B41/04Conversion of internal-combustion engine cylinder units to pumps
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02BINTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
    • F02B1/00Engines characterised by fuel-air mixture compression
    • F02B1/02Engines characterised by fuel-air mixture compression with positive ignition
    • F02B1/04Engines characterised by fuel-air mixture compression with positive ignition with fuel-air mixture admission into cylinder
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02BINTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
    • F02B75/00Other engines
    • F02B75/02Engines characterised by their cycles, e.g. six-stroke
    • F02B2075/022Engines characterised by their cycles, e.g. six-stroke having less than six strokes per cycle
    • F02B2075/027Engines characterised by their cycles, e.g. six-stroke having less than six strokes per cycle four

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Valve Device For Special Equipments (AREA)

Abstract

1480247 Engines alternatively usable as compressors T UENO 19 June 1974 [22 June 1973 2 July 1973 5 July 1973] 27182/74 Headings F1B and F1N A combination I.C. engine and air compressor has at least one compression chamber able to operate in a first operating mode as a combustion chamber and in a second operating mode as an air compressing chamber for compressing air without admixture of fuel, and means comprising two transmissions between a crank-shaft and one or more respective valve timing cam-shafts of the combination, the transmissions being able to operate in a way in which they do not simultaneously inter-connect the crank-shaft with a common said cam-shaft, there being in the combination a compressed air source and means for connecting the source operatively to at least one said chamber. Engine 1 has an inlet valve cam-shaft 6 and an exhaust valve cam-shaft 7. The cam-shafts are driven at half crank-shaft speed for engine action by a first transmission comprising sprockets 9,10 and 11 each of which is associated with an electromagnetic clutch 12, 13, 14 by which a sprocket can be coupled to its shaft in a predetermined angular relationship. At the other end of the engine/compressor is a second transmission which is similar except that it drives the cam-shafts at the same speed as the crank-shaft, for compressor action and the angular relationship between the crank-shaft and cam-shafts is such that the inlet valve operation is delayed relative to its operation during engine action and the exhaust valve is timed to close at T.D.C. In a modification the valve timing is not altered, the cam-shaft speed merely being increased to that of the crank-shaft. When the unit is running as a compressor, air may be exhausted through the exhaust port and diverted by an electromagnetically-operated valve in the exhaust pipe to a storage tank Fig. 2 (not shown) or an additional automatic exhaust valve 29, Fig. 3, may be provided, connected by duct 45 and check-valve 46 to tank T. The second transmission may drive the cam-shafts at half the crankshaft speed so that the inlet and exhaust valves are opened on alternate down strokes of the piston, or the cam-shafts may be driven at crank-shaft speed so that both inlet and exhaust valves open on each down stroke of the piston. When the combination is operating as an engine the automatic valve 29 is held closed by ley oil or air-pressure or by electromagnetic means. In a further embodiment, Fig. 5, the cylinders are divided into a first set 52 which always operates as an engine and has an axiallydisplaceable cam-shaft 54. The inlet and exhaust cams on this shaft each comprise two sections, a first section providing a normal amount of valve overlap and a section providing an increased amount of valve overlap, the latter section being brought into operation when the cylinders are supercharged. The second set of cylinders, 53, have an axially displaceable cam-shaft 55, carrying inlet and exhaust cams which each have sections which enable this set of cylinders to operate as an engine, as a single or two-stage compressor or in a No-load condition in which air is drawn into the cylinders but not compressed. The facility to use the second set of cylinders as a single or two-stage compressor is used to reduce the load on the first set of cylinders, when these are being started, by compressing the air in two stages at first and then changing to single stage compression. The second set of cylinders are operated in the engine mode when maximum power is required, in the compressor mode to absorb power when the engine is slowing down, the compressed air being stored, or in the compressor mode with the air being used to supercharge the first set of cylinders, either directly or after the air has been expanded in a compressed air machine, such as one providing a cooling action. When the first set of cylinders is idling, the second set of cylinders operate in the No-load mode. The combination is arranged so that the functions of the sets of cylinders can be interchanged at intervals of e.g. 4,000 km. The cylinders can also be operated as air-motors either for starting the set of cylinders operating in the engine mode, or to improve acceleration by supplying compressed air to the cylinders operating in the compressor mode. In a further embodiment, Fig. 13, a residual air valve 83 is provided for exhausting high-pressure air remaining in the cylinder at the end of a compression stroke. The valve is also used to supply compressed air to the cylinders to produce either normal or reverse rotation of the engine. The port 82 controlled by valve 83 is connected to manifold 84 which has a branch 85 leading to atmosphere or a supercharger and a branch 86 connected to highpressure tank containing air at 20-50 kg/sq.cm. An electromagnetically controlled valve 89 controls the direction of flow. Valve 83 is operated by an axially displaceable cam which has (a) a cylindrical portion (92) which is associated with engine action and does not operate the valve, (b) a starting portion (93) for normal rotation as an engine and which opens the valve at about the beginning of the power stroke to admit compressed air, (c) a residual air exhaust portion (94) which acts during compressor mode operation (d) a reverse rotation starting portion (95) which opens the valve at a time corresponding to the end of the compression stroke of the engine mode of operation to admit compressed air and (e) a residual air exhaust section (96) which opens valve 83 which acts during operation in the compressor mode in reverse rotation . The axially displaceable cam for the inlet valve 31 includes (a) a section (102) which is operative during operation in the engine mode in the normal direction of rotation (b) a section (103) which is operative during compressor mode action in the normal direction of rotation (c) a section (104) for engine mode operation in the reverse direction of rotation (d) a section (105) for compressor mode operation in the reverse direction of rotation and (e) a cylindrical section (106) between sections (102) and (104). The cam for the exhaust valve 32 is similar to the inlet valve cam but arranged to produce appropriate timing of the valve. The inlet and exhaust cams are on one cam-shaft and the cam for valve 83 is on a separate cam-shaft.
GB2718274A 1973-06-22 1974-06-19 Combination engine and air compressor Expired GB1480247A (en)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
JP48070559A JPS5020148A (en) 1973-06-22 1973-06-22
JP48074536A JPS5022313A (en) 1973-07-02 1973-07-02
JP7626973A JPS5022909A (en) 1973-07-05 1973-07-05

Publications (1)

Publication Number Publication Date
GB1480247A true GB1480247A (en) 1977-07-20

Family

ID=27300371

Family Applications (1)

Application Number Title Priority Date Filing Date
GB2718274A Expired GB1480247A (en) 1973-06-22 1974-06-19 Combination engine and air compressor

Country Status (1)

Country Link
GB (1) GB1480247A (en)

Cited By (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2142090A (en) * 1983-06-21 1985-01-09 Mtu Friedrichshafen Gmbh A low compression ratio multi-cylinder diesel internal combustion engine
GB2142381A (en) * 1983-06-29 1985-01-16 Mtu Friedrichshafen Gmbh Low compression ratio multi-cylinder diesel internal combustion engine
US6925979B1 (en) 2002-07-26 2005-08-09 Avl List Gmbh Method of operating a multicylinder internal combustion engine
WO2009080211A1 (en) * 2007-12-20 2009-07-02 Knorr-Bremse Systeme für Nutzfahrzeuge GmbH Device for generating compressed air for a vehicle and method for operating a device for generating compressed air
EP2113660A1 (en) 2008-04-30 2009-11-04 Ricoh Company, Ltd. Air Discharging Apparatus and Image Forming Apparatus
NL2007346C2 (en) * 2011-09-05 2012-09-04 Truijens METHOD AND DEVICE FOR STORING AND GENERATING ELECTRICITY.
GB2607657A (en) * 2022-02-25 2022-12-14 Stephen Bell Ian Piston compression pulse spray dryer
CN116400011A (en) * 2023-03-09 2023-07-07 中国环境科学研究院 Regional scale ecosystem carbon flux unmanned aerial vehicle airborne automatic detection equipment

Cited By (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2142090A (en) * 1983-06-21 1985-01-09 Mtu Friedrichshafen Gmbh A low compression ratio multi-cylinder diesel internal combustion engine
GB2142381A (en) * 1983-06-29 1985-01-16 Mtu Friedrichshafen Gmbh Low compression ratio multi-cylinder diesel internal combustion engine
US6925979B1 (en) 2002-07-26 2005-08-09 Avl List Gmbh Method of operating a multicylinder internal combustion engine
WO2009080211A1 (en) * 2007-12-20 2009-07-02 Knorr-Bremse Systeme für Nutzfahrzeuge GmbH Device for generating compressed air for a vehicle and method for operating a device for generating compressed air
US8079344B2 (en) 2007-12-20 2011-12-20 Knorr-Bremse Systeme Fuer Nutzfahrzeuge Gmbh Device for generating compressed air for a vehicle and method for operating a device for generating compressed air
EP2113660A1 (en) 2008-04-30 2009-11-04 Ricoh Company, Ltd. Air Discharging Apparatus and Image Forming Apparatus
US8139973B2 (en) 2008-04-30 2012-03-20 Ricoh Company, Ltd. Air discharging apparatus and image forming apparatus
NL2007346C2 (en) * 2011-09-05 2012-09-04 Truijens METHOD AND DEVICE FOR STORING AND GENERATING ELECTRICITY.
GB2607657A (en) * 2022-02-25 2022-12-14 Stephen Bell Ian Piston compression pulse spray dryer
CN116400011A (en) * 2023-03-09 2023-07-07 中国环境科学研究院 Regional scale ecosystem carbon flux unmanned aerial vehicle airborne automatic detection equipment
CN116400011B (en) * 2023-03-09 2023-09-05 中国环境科学研究院 Regional scale ecosystem carbon flux unmanned aerial vehicle airborne automatic detection equipment

Similar Documents

Publication Publication Date Title
US3958900A (en) Convertible engine-air compressor apparatus mounted on a vehicle for driving said vehicle
US3765180A (en) Compressed air engine
US3786792A (en) Variable valve timing system
EP2347108B1 (en) An exhaust arrangement for an internal combustion engine
US4671226A (en) Supercharged multi-cylinder four-cycle diesel engine
US8490584B2 (en) Air hybrid engine with dual chamber cylinder
CN1004719B (en) Low compression ratio multi-cylinder diesel engine
JP2003518222A (en) Reciprocating internal combustion engine with balancing and supercharging functions
US8622032B2 (en) Internal combustion engine with dual-chamber cylinder
JP5842078B1 (en) Self-igniting large low-speed turbocharged two-stroke internal combustion engine with starting air system
SU969177A3 (en) Engine and air compressor
US3174432A (en) Combustion engine for conveying a hydraulic pressure medium
US4843821A (en) Multicylinder compound engine
WO1999006682A2 (en) Supercharged internal combustion compound engine
GB1480247A (en) Combination engine and air compressor
US4386587A (en) Two stroke cycle engine with increased efficiency
US3269321A (en) Combustion engine for conveying a hydraulic pressure medium
AU713009B2 (en) Internal combustion engines
US4643156A (en) Internal combustion engine with a positive displacement supercharger mechanically driven from the engine crankshaft
CN210239871U (en) Pressurizing device for improving EGR rate
US6293236B1 (en) Breathing system for internal combustion engines, using dual duty (alternatively exhaust-intake) valves and a forced air supply
JPH01116258A (en) Compression top dead center pressure reducing exhaust brake device
US1629530A (en) Multi-cylinder internal-combustion engine
JP3030365B2 (en) Internal combustion engine
US2236634A (en) Method and means for starting diesel engines

Legal Events

Date Code Title Description
PS Patent sealed
746 Register noted 'licences of right' (sect. 46/1977)
PCNP Patent ceased through non-payment of renewal fee