Engine recovery system for engine system

Patent metadata

Field	Value
Publication number	US-10508595-B2
Application number	US-201715653691-A
Country	US
Kind code	B2
Filing date	Jul 19, 2017
Priority date	Jul 19, 2017
Publication date	Dec 17, 2019
Grant date	Dec 17, 2019

Abstract

An energy recovery system for an engine system is disclosed. The engine system includes an engine, an exhaust conduit configured to receive exhaust gases discharged from the engine, and a first turbocharger coupled to the exhaust conduit to receive exhaust gases from the engine and provides compressed air to the engine. The energy recovery system includes a bypass conduit, a second turbocharger, and an accumulator. The bypass conduit is coupled to the exhaust conduit upstream of the first turbocharger, and facilitates a portion of exhaust gases from the exhaust conduit to bypass the first turbocharger. The second turbocharger is coupled to the bypass conduit, and is driven by the portion of exhaust gases bypassing the first turbocharger to compress air received from an ambient to a first pressure. The accumulator is in fluid communication with the second turbocharger, and stores air received from the second turbocharger at the first pressure.

First claim

What is claimed is:

1. An energy recovery system for an engine system that includes an engine, an exhaust conduit configured to receive exhaust gases discharged from the engine, and a first turbocharger, the energy recovery system comprising:
a bypass conduit coupled to the exhaust conduit upstream of the first turbocharger,
the bypass conduit facilitating a portion of the exhaust gases from the exhaust conduit to bypass the first turbocharger;

a second turbocharger coupled to the bypass conduit,
the second turbocharger being driven by the portion of the exhaust gases bypassing the first turbocharger to compress air received from an ambient to a first pressure;

a bypass valve to control an amount of the portion of the exhaust gases passing through the bypass conduit to the second turbocharger,
the bypass valve being controlled based on a maximum capacity of the first turbocharger; and

an accumulator in fluid communication with the second turbocharger and configured to store air received from the second turbocharger at the first pressure.

2. The energy recovery system of claim 1 , further including:
an auxiliary compressor fluidly coupled to the accumulator, and configured to compress air received from the accumulator to a second pressure.

3. The energy recovery system of claim 2 , further including:
an air reservoir configured to store air received from the auxiliary compressor at the second pressure.

4. The energy recovery system of claim 3 , wherein the second pressure is higher than the first pressure.

5. The energy recovery system of claim 1 , wherein the bypass valve is controlled further based on one or more engine parameters.

6. The energy recovery system of claim 1 , wherein the bypass valve is controlled further based on a pressure of air inside the accumulator.

7. An engine system comprising:
an engine;
an exhaust conduit configured to receive exhaust gases discharged from the engine;
a first turbocharger coupled to the exhaust conduit to receive exhaust gases from the engine and configured to provide compressed air to the engine;
a bypass conduit coupled to the exhaust conduit upstream of the first turbocharger,
the bypass conduit facilitating a portion of the exhaust gases from the exhaust conduit to bypass the first turbocharger;

a second turbocharger coupled to the bypass conduit,
the second turbocharger being driven by the portion of the exhaust gases bypassing the first turbocharger to compress air received from an ambient to a first pressure;

a bypass valve to control an amount of the portion of the exhaust gases passing through the bypass conduit to the second turbocharger,
the bypass valve being controlled based on a maximum capacity of the first turbocharger; and

an accumulator in fluid communication with the second turbocharger and configured to store air received from the second turbocharger at the first pressure.

8. The engine system of claim 7 , further including:
an auxiliary compressor fluidly coupled to the accumulator and configured to compress air received from the accumulator to a second pressure.

9. The engine system of claim 8 , further including:
an air reservoir configured to store air received from the auxiliary compressor at the second pressure.

10. The engine system of claim 8 , wherein the second pressure is higher than the first pressure.

11. The engine system of claim 7 , wherein the bypass valve is controlled further based on one or more engine parameters.

12. The engine system of claim 7 , wherein the bypass valve is controlled further based on a pressure of air inside the accumulator.

13. A locomotive comprising:
an engine;
an exhaust conduit configured to receive exhaust gases discharged from the engine;
a first turbocharger coupled to the exhaust conduit to receive exhaust gases from the engine and configured to provide compressed air to the engine;
a bypass conduit coupled to the exhaust conduit upstream of the first turbocharger,
the bypass conduit facilitating a portion of the exhaust gases from the exhaust conduit to bypass the first turbocharger;

a second turbocharger coupled to the bypass conduit,
the second turbocharger being driven by the portion of the exhaust gases bypassing the first turbocharger to compress air received from an ambient to a first pressure;

a bypass valve to control an amount of the portion of the exhaust gases passing through the bypass conduit to the second turbocharger,
the bypass valve being controlled based on a maximum capacity of the first turbocharger;

an accumulator in fluid communication with the second turbocharger and configured to store air received from the second turbocharger at the first pressure;
an auxiliary compressor fluidly coupled to the accumulator, and configured to compress air received from the accumulator to a second pressure; and
an air reservoir configured to store the air received from the auxiliary compressor at the second pressure.

14. The locomotive of claim 13 , wherein the second pressure is higher than the first pressure.

15. The locomotive of claim 13 , wherein the bypass valve is controlled further based on one or more engine parameters.

16. The locomotive of claim 13 , wherein the bypass valve is controlled further based on a pressure of air inside the accumulator.

17. The locomotive of claim 13 , further including:
a brake system configured to receive air from the air reservoir to reduce a speed of the locomotive.

18. The energy recovery system of claim 1 , further including:
an outlet conduit coupled to the bypass conduit; and
a valve disposed in the outlet conduit,
the valve being operated to allow another portion of the exhaust gases from the bypass conduit to the ambient via the outlet conduit.

19. The engine system of claim 7 , further including:
an outlet conduit coupled to the bypass conduit; and
a valve disposed in the outlet conduit,
the valve being controlled to allow another portion of the exhaust gases flowing into the bypass conduit to bypass the second turbocharger and flow through the outlet conduit.

20. The locomotive of claim 13 , further including:
an outlet conduit coupled to the bypass conduit; and
a valve disposed in the outlet conduit.

Assignees

• Progress Rail Locomotive Inc

Inventors

• Pocha Siva Sankara Reddy
• Loya Sudarshan
• Moravec Keith
• Goetzke Michael B

Classifications

• F02M26/05

  High pressure loops, i.e. wherein recirculated exhaust gas is taken out from the exhaust system upstream of the turbine and reintroduced into the intake system downstream of the compressor · CPC title

• F02M26/10

  having means to increase the pressure difference between the exhaust and intake system, e.g. venturis, variable geometry turbines, check valves using pressure pulsations or throttles in the air intake or exhaust system · CPC title

• F02B37/004 Primary

  with exhaust drives arranged in series · CPC title

• F02B37/166

  the auxiliary apparatus being a combustion chamber, e.g. upstream of turbine · CPC title

• F02M26/08

  for engines having two or more intake charge compressors or exhaust gas turbines, e.g. a turbocharger combined with an additional compressor · CPC title