Supercharging system for an internal combustion engine

• US 4,696,165 A
• Filed: 11/21/1985
• Issued: 09/29/1987
• Est. Priority Date: 11/28/1984
• Status: Expired due to Term

• Current Assignee: Man - B&W Diesel GmbH A Limited Liability Company of Germany
• Original Assignee: Man - B&W Diesel GmbH
• Inventors: Bucher, Jakob
• Primary Examiner(s): KOCZO JR, MICHAEL
• Application Number:
  US06/800,520
• Time in Patent Office: 677 Days
• Field of Search: 60/609, 60/610, 60/611, 60/612, 60/606, 123/559
• US Class Current: 60/609
• CPC Class Codes: F02B 37/04 Engines with exhaust drive and other drive of pumps, e.g. with exhaust-driven pump and mechanically-driven second pump
• CPC Class Codes: F02B 37/14 Control of the alternation between or the operation of exhaust drive and other drive of a pump, e.g. dependent on speed
• CPC Class Codes: F04D 25/024 the driving means being assisted by a power recovery turbine
• CPC Class Codes: F04D 27/0238 Details or means for fluid reinjection
• CPC Class Codes: F05D 2220/40 in turbochargers
• CPC Class Codes: Y02T 10/12 Improving ICE efficiencies

Abstract

Auxiliary compressed air is supplied to an inlet manifold (3) of an internal combustion engine (1) by an auxiliary compressor (8), driven from the main shaft of the ICE. A controlled clutch (17) is interposed between the engine (1) and the auxiliary compressor, the clutch being controlled by a memory and controller (18) receiving inlet manifold pressure signals (P) and fuel quantity signals (F) and providing output control signals to the controlled clutch (17) based on stored functions or tables within the memory and controller to provide for desired and optimum operation of the engine with appropriate charge air in view of injected fuel quantity. The compressed air derived from the auxiliary compressor (8) is injected into the main compressor to impinge on the vanes or blades (15) of the main compressor (6).

Claims

1. Supercharging control system for an internal combustion engine (ICE) (1) having

an exhaust gas turbine (5) driven by exhaust gases from the ICE (1);

a main air compressor (6) driven by the exhaust gas turbine (5) and providing compressed air to an inlet manifold (3) of the ICE (1),

an auxiliary air compressor (8) driven by rotary power derived from the ICE to provide additional air to said main compressor (6);

a controlled clutch (17) drivingly connected to the auxiliary compressor (8) and the ICE (1) to selectively establish or disconnect rotary drive power between the ICE (1) and the auxiliary compressor (8);

fuel quantity sensing means (21) for sensing quantity of fuel being supplied to the ICE (1) and providing a fuel quantity signal (F);

air pressure sensing means (19) coupled to an air inlet (3) of the ICE for sensing charging air pressure and providing an air pressure signal (P);

and comprising ;

a memory and controller (18) coupled to control, selectively, establishment and disconnection of the rotary drive power between the ICE and the auxiliary compressor, and

wherein

said memory and controller is coupled to receive the air pressure signal (P) and the fuel quantity signal (F) and storing the relationship between air supply pressure and fuel quantity for desired performance of the ICE;

said memory and controller (18) provides an output signal coupled to and controlling the controlled clutch (17) to obtain said desired performance;

and wherein said main compressor (6) comprises a centrifugal compressor including nozzles (14) positioned about the outer circumference of a chamber within which rotary blades (15) of the centrifugal compressor operate, said nozzles (14) receiving compressed air from the auxiliary compressor (8) and being oriented to apply additional drive power to the main compressor (6).

2. System according to claim 1, wherein the memory and controller (18) stores said relationship relating air supply pressure and fuel quantity, and provides operating control signals to the controlled clutch (17) to provide said desired performance by selectively causing additional air from the auxiliary compressor to be supplied to the air inlet manifold of the ICE if the air pressure signal (P) and the fuel quantity signal (F) do not meet the stored characteristics of the engine which result in said desired performance.

3. System according to claim 1, wherein the pressure sensing means (19) comprises a pressure transducer coupled to the inlet manifold (3) of the engine and provides said air pressure signal (P), and the fuel quantity sensing means (21) comprises a position transducer, independently sensing the quantity of fuel being supplied to the ICE (1) and providing said fuel quantity signal (F), said air pressure signal (P) and said fuel quantity signal (F) being independently connected to said memory and controller (18).

4. System according to claim 1, wherein the auxiliary air compressor (8) provides compressed air at a pressure of between about 2 to 4 bar.

5. System according to claim 1, wherein said memory and controller compares operation supply parameters of the engine comprising air charge pressure (P) and fuel supply (F) with the stored relationships and, selectively,

(1) upon detecting excess fuel, controls said clutch (17) to engage and

(2) upon detecting excess air pressure, controls said clutch (17) to disengage.

6. System according to claim 4 wherein said nozzles (14) are in air flow communication with said compressor chamber or manifold (11).

7. System according to claim 6 wherein said nozzles (14) have an angle of inclination of between about 15°

to 30°

with respect to the plane of rotation of the compressor wheel.

8. System according to claim 4 wherein a check valve (10) is provided, connected to receive compressed air from said auxiliary air compressor (8);

and

wherein connection means are provided to connect the compressed air from the auxiliary compressor to a compressor chamber or manifold (11) of said main compressor (6).