Turbocharger system for an engine

Patent metadata

Field	Value
Publication number	US-10054039-B2
Application number	US-201615142920-A
Country	US
Kind code	B2
Filing date	Apr 29, 2016
Priority date	Apr 29, 2016
Publication date	Aug 21, 2018
Grant date	Aug 21, 2018

Abstract

A system having an engine is provided. The system includes a high pressure (HP) turbocharger and a low pressure (LP) turbocharger connected in series with each other. The system also includes a first valve assembly configured to selectively bypass at least a portion of the exhaust from the engine to the LP turbocharger. The system also includes a storage tank configured to store a pressurized fluid and configured to be in fluid communication with the HP turbocharger and the LP turbocharger. The system further includes a second valve assembly in fluid communication with the storage tank, the HP turbocharger and the LP turbocharger. The system also includes a controller operatively coupled to the first valve assembly and the second valve assembly. The controller is configured to selectively operate the first valve assembly and the second valve assembly based on a change in a load requirement on the engine.

First claim

What is claimed is:

1. A turbocharger system having an engine a storage tank, the system comprising:
a high pressure turbocharger including:
a turbine in fluid communication with an the engine to receive an exhaust gas therefrom; and
a compressor;

a low pressure turbocharger connected in series arrangement with the high pressure turbocharger and including:
a turbine in fluid communication with an exhaust bypass valve and the turbine of the high pressure turbocharger; and
a compressor in fluid communication with a compressor bypass valve;
wherein the compressor of the high pressure turbocharger is in fluid communication with the compressor of the low pressure turbocharger via the compressor bypass valve;
wherein the exhaust bypass valve is in fluid communication with the engine, the turbine of the low pressure turbocharger and the turbine of the high pressure turbocharger;
wherein the exhaust bypass valve is configured to selectively bypass the exhaust gas from the engine to the turbine of the low pressure turbocharger without passing through the turbine of the high pressure turbocharger;

wherein the compressor bypass valve is in fluid communication with a switch valve;
wherein the switch valve is connected to the storage tank via a check valve in a charging mode and via a pressure regulator in a discharging mode; and

a controller operatively coupled to the exhaust bypass valve, the compressor bypass valve and the switch valve, the controller configured to selectively operate the exhaust bypass valve, the compressor bypass valve and the switch valve based on a change in a load requirement on the engine.

2. The system of claim 1 further including multiple engines, each of the multiple engines including an associated high pressure turbocharger having a turbine and a compressor, low pressure turbocharger having a turbine and a compressor, exhaust bypass valve, compressor bypass valve, switch valve, check valve and pressure regulator;
wherein the compressor of the high pressure turbocharger and the compressor of the low pressure turbocharger of said each of the multiple engines are fluidly coupled with the storage tank; and
wherein the controller individually controls the exhaust bypass valve, the compressor bypass valve, and the switch valve for said each of the multiple engines based on a change in the load requirement on the system.

3. The system of claim 1 , wherein the controller is configured to operate the exhaust bypass valve, the compressor bypass valve and the switch valve in a charging mode for the storage tank during a steady state condition of the engine, and the controller is further configured to:
operate the exhaust bypass valve to bypass at least a portion of the exhaust from the engine to the turbine of the low pressure turbocharger; and
operate the compressor bypass valve and the switch to allow a pressurized air to flow from the compressor of the low pressure turbocharger to the switch valve, and to a check valve, and finally to the storage tank.

4. The system of claim 1 , wherein the controller is configured to operate the exhaust bypass valve, the compressor bypass valve and the switch valve in a discharging mode for the storage tank during at least one of a startup condition and an increase in load requirement on the engine, and the controller is further configured to:
operate the exhaust bypass valve to block direct fluid communication between the engine and the turbine of the low pressure turbocharger; and
operate the compressor bypass valve and the switch valve to allow pressurized air to flow from the storage tank to a pressure regulator, and to the switch valve, and finally to the compressor of the high pressure turbocharger.

5. The system of claim 1 , wherein the controller operates the exhaust bypass valve, the compressor bypass valve and the switch valve in a disconnected mode for the storage tank based on a capacity of the storage tank, and the controller is further configured to:
operate the exhaust bypass valve to maximize an efficiency of the high pressure turbocharger and the low pressure turbocharger; and
operate the compressor bypass valve to block fluid communication of the switch valve with each of the compressor of the high pressure turbocharger and the compressor of the low pressure turbocharger.

Assignees

• Caterpillar Inc

Inventors

• Ge Xinyu
• Qi Yongli

Classifications

• F02D25/00

  Controlling two or more co-operating engines · CPC title

• F02D41/04

  Introducing corrections for particular operating conditions (F02D41/14 takes precedence) · CPC title

• F02D41/062

  for starting (F02D41/061 takes precedence) · CPC title

• F02D41/0007

  for control of turbo-charged or super-charged engines (control of the pumps per se F02B37/12) · CPC title

• F02B33/44

  Passages conducting the charge from the pump to the engine inlet, e.g. reservoirs · CPC title