# US 4,391,098 A · Turbo-compound internal combustion engine

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- Number: US 4,391,098 A
- Document ID: US4391098A
- Status: Granted
- Kind: A
- Application number: 06/300,115
- Filed: 1981-09-08
- Granted: 1983-07-05
- Earliest claimed: 1980-09-17
- Assignees: Nissan Motor Co., Ltd.
- Inventors: Hideaki Kosuge
- Web page: https://patentgrep.com/patent/US4391098A

## CPC

- F02B 41/10: in exhaust turbines (use of exhaust turbines for charging F02B37/00)
- F02B 37/005: {Exhaust driven pumps being combined with an exhaust driven auxiliary apparatus, e.g. a ventilator}
- F02B 37/025: {Multiple scrolls or multiple gas passages guiding the gas to the pump drive}
- F02B 37/16: by bypassing charging air
- F02B 37/18: by bypassing exhaust {from the inlet to the outlet of turbine or to the atmosphere}
- Y02T 10/12: Improving ICE efficiencies
- F02B: INTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL (gas-turbine plants F02C; hot-gas or combustion-product positive-displacement engine plants F02G)
- Y02T: CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION

## Abstract

First and second waste gates respectively control the supercharging pressure of an engine supercharger and the pressure fed to an auxiliary turbine from the engine turbo-charger turbine. The scroll of the auxiliary turbine is divided by a partition into first and second passages which respectively receive the exhaust gases by-passed by the first waste gate and the exhaust gases from the turbo-charger turbine. The first waste gate prevents over pressurization of the engine cylinders while the second prevents the build up of excessive back pressure downstream of the turbo-charger turbine, thus maintaining the efficiency and torque output of the engine while still deriving benefit from the operation of the auxiliary turbine.

## Claims

### Claim 1

In a engine system including a internal combustion engine equipped with a turbo-charger and an auxiliary turbine integrated with said engine, the combination comprising:
an exhaust passage leading from a combustion chamber of said engine to a turbine of said turbo-charger;
a transfer passage leading from the turbo-charger turbine to a scroll of said auxiliary turbine;
a first by-pass passage leading from said exhaust passage to said scroll;
a second by-pass passage leading from said transfer passage to an exhaust conduit of said engine;
a first waste gate responsive to the discharge pressure of a compressor of said turbo-charger which controls the communication between said exhaust passage and said first by-pass passage, said first waste gate being adapted to open upon the discharge pressure of said turbo-charger compressor reaching a first predetermined value;
a second waste gate responsive to the pressure prevailing in said transfer passage which controls the communication between said second by-pass passage and said transfer passage, said second waste gate being adapted to open upon a second predetermined pressure prevailing in said transfer passage; and
means defining first and second passages within said scroll which exclusively communicate with said first by-pass passage and said transfer passage, respectively.

### Claim 2 (depends on 1)

A combination as claimed in claim 1, wherein said first waste gate comprises a first valve and a first pressure differential responsive motor which has a first atmospheric chamber and a first pressure chamber, said first pressure chamber fluidly communicating with an induction passage leading from said compressor to said combustion chamber.

### Claim 3 (depends on 1)

A combination as claimed in claim 1, wherein said second waste gate includes a second valve and a second pressure differential responsive motor which has a second atmospheric chamber and a second pressure chamber, said second pressure chamber fluidly communicating with said transfer passage.

### Claim 4 (depends on 1)

A combination as claimed in claim 1 wherein said first and second passage defining means is a partition formed within said scroll, and wherein said first and second passages are so shaped as to direct the exhaust gases flowing therein against blades of said auxiliary turbine with the optimal angle of incidence and with the minimum of interference between the respective flows.