Supercharged internal combustion engines

• US 4,077,219 A
• Filed: 04/23/1976
• Issued: 03/07/1978
• Est. Priority Date: 04/24/1975
• Status: Expired due to Term

• Current Assignee: Etat Francais
• Original Assignee: Etat Francais
• Inventors: Melchior, Jean, Andre, Thierry
• Primary Examiner(s): Freeh, William L.
• Assistant Examiner(s): Casaregola, L. J.
• Application Number:
  US05/679,589
• Time in Patent Office: 683 Days
• Field of Search: 60/599, 60/604, 60/605, 60/606, 60/39.51 R, 60/611, 123/119 CD
• US Class Current: 60/599
• CPC Class Codes: F01N 5/02 the devices using heat
• CPC Class Codes: F02B 29/0412 Multiple heat exchangers arranged in parallel or in series
• CPC Class Codes: F02B 29/0418 the intake air cooler having a bypass or multiple flow paths within the heat exchanger to vary the effective heat transfer surface
• CPC Class Codes: F02B 37/00 Engines characterised by provision of pumps driven at least for part of the time by exhaust
• CPC Class Codes: F02B 37/11 driven by other drive at starting only
• CPC Class Codes: F02B 37/166 the auxiliary apparatus being a combustion chamber, e.g. upstream of turbine
• CPC Class Codes: F02B 39/10 electric
• CPC Class Codes: F02B 39/12 Drives characterised by use of couplings or clutches therein using fluid slip couplings for varying gear ratio F02B39/08
• CPC Class Codes: Y02T 10/12 Improving ICE efficiencies

Abstract

A power unit comprises an internal combustion compression ignited engine having variable-volume combustion chambers and supercharged by a turbocompressor having a turbine which receives the engine exhaust gases. A bypass pipe which is permanently open during operation of the engine returns the air not absorbed by the engine to the turbine with a pressure drop which, if appreciable, is independent of the flow rate and increases with the compressor outlet pressure. The power unit comprises a heat exchanger between the gas flow leaving the turbine and the air flow leaving the compressor. An air cooler is disposed in the path of the air travelling from the heat exchanger to the engine.

Claims

1. A power unit comprising:

an internal combustion engine having variable volume combustion chambers,

a supercharging turbocompressor unit having a compressor and a turbine, the inlet of said turbine being connected to receive the exhaust gas of said engine,

pipe means connecting the outlet of said compressor to the intake of said engine,

bypass conduit means having an inlet and and outlet always connected and open during operation of said turbocompressor unit to flow the air delivered by said compressor and not drawn by said engine to the inlet of said turbine with a pressure drop which, if appreciable, is substantially independent of the flow rate in the bypass conduit and increases with the output pressure of said compressor,

heat exchanger means located upstream of the junction of the inlet of said bypass conduit means with said pipe means and operable to exchange heat between the pressurized air flow from said compressor to the engine and to said bypass conduit means and the gas flow from the turbine outlet to atmosphere,

and air cooling means located in the air path between said compressor and the intake of said engine downstream of the junction of the inlet of said bypass conduit means with said pipe means so as to be flown only by the air drawn by said engine.

2. A power unit comprising:

an internal combustion engine having variable volume combustion chamber,

a supercharging turbocompressor unit having a compressor and a turbine, the inlet of said turbine being connected to receive the exhaust gas of said engine,

pipe means connecting the outlet of said compressor to the intake of said engine,

bypass conduit means having an inlet and an outlet always connected and open during operation of said turbocompressor unit to flow the air delivered by said compressor and not drawn by said engine to the inlet of said turbine with a pressure drop which, if appreciable, is substantially independent of the flow rate in the bypass conduit and increases with the output pressure of said compressor,

an auxiliary combustion chamber connected to receive air from said bypass conduit means and to deliver combustion gas to said turbine,

heat exchanger means located upstream of the junction of the inlet of said bypass conduit means with said pipe means and operable to exchange heat between the pressurized air flow from said compressor to said engine and to said bypass conduit means and the gas flow from the turbine outlet to atmosphere,

and air cooling means located in the air path between said compressor and the intake of said engine downstream of the junction of the inlet of said bypass conduit means with said pipe means so as to be flown only by the air drawn by said engine.

3. A power unit according to claim 2, wherein said engine is a diesel engine having a compression ratio lower than 12, wherein said compressor has a high compression ratio and efficiency and wherein said turbocompressor unit is matched to said engine to operate along a characteristic line in the zone of maximum efficiency thereof, and wherein the air cooling means are undersized as compared with the air cooling means which would be necessary in the absence of said heat exchanger means.

4. A power unit according to claim 3, wherein said compressor has a nominal pressure ratio in excess of 6 and an isentropic efficiency of about 0.8.

5. A power unit according to claim 2, wherein said air cooling means is provided with control means responsive to the speed of the engine and operable to adjust the dissipated thermal flow substantially proportional to the speed of said engine and to the pressure of the air drawn by said engine.

6. A power unit according to claim 5, wherein said control means comprises means responsive to the conditions which prevail during cranking, idling and low power operation of the engine for rendering said cooling means inoperative under such conditions.

7. A power unit according to claim 6, wherein said control means are arranged to render the air cooling means inoperative as long as the pressure of the air in the intake of the engine is lower than a predetermined value.

8. A power unit according to claim 6, wherein the control means are responsive to the ambient temperature for increasing the dissipated thermal flow responsive to an increase of said ambient temperature.

9. A power unit according to claim 3, wherein said engine and said air cooling means are cooled with atmospheric air, further having blower means driven by the engine through transmission means having an adjustable transmission ratio and control means for adjusting said transmission ratio as a function of the pressure of air in the intake of the engine.

10. A power unit according to claim 2, further comprising means for cranking said turbocompressor, which cooperate with said auxiliary combustion chamber for bringing the turbocompressor to self-sustaining operation prior to engine cranking.

11. A power unit according to claim 10, further having a branch circuit connected between the intake and the exhaust of the engine for circulating a restricted flow of pressurized air from the outlet of the heat exchanger across the air cooling means to heat the same prior to cranking said engine for starting.

12. A power unit according to claim 5, wherein said air cooling means comprises a second heat exchanger defining a path in said pressurized air flow from said compressor to said engine, fluid moving means for circulating a cooling fluid across said second exchanger means, said fluid moving means being drivably connected to said engine, and means for controlling the flow of fluid delivered from said fluid moving means to said second heat exchanger comprising a probe delivering a signal representative of the pressure of the air charged into the engine and adjusting said flow in proportion to the said pressure.

13. A power unit according to claim 12, wherein said fluid moving means comprises rotary fan means for circulating atmospheric air to thereby provide said cooling fluid, said flow controlling means comprising a speed variator having an adjustable transmission ratio and operably interconnecting said fan means to said engine, said probe being operable to deliver said signal to control said ratio of said variator transmission.