Twin scroll turbocharger device with bypass

Patent metadata

Field	Value
Publication number	US-9874138-B2
Application number	US-201514858231-A
Country	US
Kind code	B2
Filing date	Sep 18, 2015
Priority date	Sep 26, 2014
Publication date	Jan 23, 2018
Grant date	Jan 23, 2018

Abstract

A twin scroll turbocharger device for an internal combustion engine includes a turbine and a compressor, wherein the turbine comprises a first turbine scroll and a second turbine scroll, and wherein at least the first turbine scroll is provided with a turbine scroll inlet valve such that the exhaust gas flow through the first turbine scroll is controllable. The twin scroll turbocharger device is further characterized in that a bypass conduit is provided between a compressor and at least the first turbine scroll. The bypass conduit is provided with a bypass conduit valve such that a flow through the bypass conduit is controllable.

First claim

What is claimed is:

1. A twin scroll turbocharger device for an internal combustion engine, the twin scroll turbocharger device comprising:
a turbine with a turbine wheel configured to be driven by exhaust gas guided from the internal combustion engine, the turbine further comprising a first turbine scroll and a second turbine scroll,
wherein the first turbine scroll is provided with a first turbine scroll inlet valve at a first turbine scroll inlet to control the exhaust gas flow through the first turbine scroll inlet of the first turbine scroll; and
wherein the second turbine scroll is provided with a second turbine scroll inlet valve at a second turbine scroll inlet to control the exhaust gas flow through the second turbine scroll inlet of the second turbine scroll;

a compressor with a compressor wheel connected to and configured to be driven by the turbine wheel to pump compressor gas to the internal combustion engine;
a turbocharger housing enclosing the turbine and the compressor; and
a bypass conduit that connects a pressurized portion of the compressor with the first and second turbine scrolls at a respective portion of each turbine scroll provided downstream, in relation to the exhaust gas flow, of a respective turbine scroll inlet valve,
wherein the bypass conduit is configured to allow fluid communication between the compressor and the first and second turbine scrolls; and
wherein the bypass conduit is provided with a bypass conduit valve that is configured to control fluid flow from the pressurized portion of the compressor through the bypass conduit if the compressor is in fluid communication with the first turbine scroll and/or the second turbine scroll.

2. The twin scroll turbocharger device according to claim 1 , wherein the first and second turbine scrolls are arranged side by side with reference to a rotational direction of the turbine wheel.

3. The twin scroll turbocharger device according to claim 1 , wherein the first turbine scroll is arranged outwardly in a radial direction with reference to the turbine wheel of the second turbine scroll.

4. The twin scroll turbocharger device according to claim 1 , wherein the first and second turbine scrolls have equal cross sectional flow areas.

5. The twin scroll turbocharger device according to claim 1 , wherein the first turbine scroll has a larger cross sectional flow area than the second turbine scroll.

6. The twin scroll turbocharger device according to claim 1 , wherein the second turbine scroll has a larger cross sectional flow area than the first turbine scroll.

7. A method of controlling a twin scroll turbocharger device for an internal combustion engine, wherein the twin scroll turbocharger device comprises:
a turbine with a turbine wheel driven by exhaust gas guided from the internal combustion engine,
wherein the turbine further comprises a first turbine scroll and a second turbine scroll;
wherein the first turbine scroll is provided with a first turbine scroll inlet valve at a first turbine scroll inlet, and the first turbine scroll inlet valve is controllable to be between an open position and a closed position to control the exhaust gas flow through the first turbine scroll; and
wherein the second turbine scroll is provided with a second turbine scroll inlet valve at a second turbine scroll inlet to control the exhaust gas flow through the second turbine scroll inlet of the second turbine scroll;

a compressor with a compressor wheel connected to and driven by the turbine wheel to pump compressor gas to the internal combustion engine;
a turbocharger housing enclosing the turbine and the compressor; and
a bypass conduit provided between a pressurized portion of the compressor and each of a portion of the first turbine scroll provided downstream, in relation to the exhaust gas flow, of the first turbine scroll inlet valve, and a portion of the second turbine scroll provided downstream, in relation to the exhaust gas flow, of the second turbine scroll inlet valve, the bypass conduit allowing fluid communication between the compressor and at least one of the first turbine scroll and the second turbine scroll,
wherein the bypass conduit is provided with a controllable bypass conduit valve that is controllable to be in a closed position or in a position open to at least one of the first scroll inlet valve and the second scroll inlet valve to control the exhaust gas flow through the bypass conduit;

the method comprising:
when an exhaust gas flow from the internal combustion engine is equal to or less than a predetermined low flow,
via an engine control unit,
closing the first turbine scroll inlet valve; and
opening the bypass conduit valve such that fluid flows from the pressurized portion of the compressor to the first turbine scroll, while the exhaust gas flow flows through the second turbine scroll.

8. The method according to claim 7 ,
wherein the bypass conduit is provided between the pressurized portion of the compressor and each of the portion of the first turbine scroll provided downstream, in relation to the exhaust gas flow, of the first turbine scroll inlet valve and a portion of the second turbine scroll provided downstream, in relation to the exhaust gas flow, of a second turbine scroll inlet valve, wherein the bypass conduit allows fluid communication between the compressor and the first and second turbine scrolls; and
wherein the bypass conduit valve is configured to control fluid flow from the pressurized portion of the compressor through the bypass conduit if the compressor is in fluid communication with at least one of the first turbine scroll and the second turbine scroll;
wherein the second turbine scroll is provided with the second turbine scroll inlet valve at a second turbine scroll inlet;
wherein the second turbine scroll inlet valve is controllable to be between an open position and a closed position to control the exhaust gas flow through the second turbine scroll; and
wherein the method further comprises:
when the exhaust gas flow from the internal combustion engine increases to be higher than the predetermined low flow but lower than a predetermined high flow,
via the engine control unit,
opening the first turbine scroll inlet valve;
closing the second turbine scroll inlet valve; and
opening the bypass conduit valve such that fluid flows from the pressurized portion of the compressor through the bypass conduit to the second turbine scroll, while the exhaust gas flow flows through the first turbine scroll.

9. The method according to claim 8 further comprising:
when the exhaust gas flow from the internal combustion engine is equal to or exceeds the predetermined high flow,
via the engine control unit,
opening all turbine scroll inlet valves, and
closing the bypass conduit valve,

while the exhaust gas flow flows through the first and second turbine scrolls.

10. The method according to claim 7 ,
wherein the bypass conduit is provided between the pressurized portion of the compressor and each of the portion of the first turbine scroll provided downstream, in relation to the exhaust gas flow, of the first turbine scroll inlet valve and a portion of the second turbine scroll provided downstream, in relation to the exhaust gas flow, of a second turbine scroll inlet valve;
wherein the bypass conduit valve is configured to control a flow through the bypass conduit and to control if the compressor is in fluid communication with the at least one of the first turbine scroll and the second turbine scroll;
wherein the second turbine scroll is provided with the second turbine scroll inlet valve at a second turbine scroll inlet, wherein the second turbine scroll inlet valve is contr

Assignees

• Volvo Car Corp

Inventors

• Almkvist Goran

Classifications

• F02B37/18

  by bypassing exhaust {from the inlet to the outlet of turbine or to the atmosphere} · CPC title

• F02B37/025 Primary

  Multiple scrolls or multiple gas passages guiding the gas to the pump drive · CPC title

• F02B2037/125

  Control for avoiding pump stall or surge · CPC title

• F02B37/168

  into the exhaust conduit (F02B37/166 takes precedence) · CPC title

• F05D2220/40

  in turbochargers · CPC title