Turbocharger with compressor operable in either single-stage mode or two-stage serial mode

Patent metadata

Field	Value
Publication number	US-9869237-B2
Application number	US-201514829802-A
Country	US
Kind code	B2
Filing date	Aug 19, 2015
Priority date	Aug 19, 2015
Publication date	Jan 16, 2018
Grant date	Jan 16, 2018

Abstract

A turbocharger includes a two-stage serial compressor having first and second impellers, with a crossover duct for leading air from the first impeller into the second impeller for further compression. The compressor housing also defines a bypass duct from the crossover duct to the air discharge duct from the compressor, and a bypass valve disposed in the bypass duct. Under certain operating conditions (such as high-flow, low-pressure-ratio conditions) the bypass valve can be opened to bypass the second impeller, such that the compressor behaves like a single-stage compressor. At other operating conditions, the bypass valve is closed so that the compressor provides two-stage compression for higher pressure ratios.

First claim

What is claimed is:

1. A turbocharger operable in either single-stage compression mode or two-stage serial compression mode, comprising:
a turbine comprising a turbine wheel and a turbine housing, the turbine wheel being affixed to one end of a rotatable shaft, the turbine housing defining an axial bore therethrough in which the turbine wheel is disposed, an exhaust gas inlet, a annular turbine volute surrounding the turbine wheel, and a nozzle leading from the turbine volute into the turbine wheel;
a compressor comprising a compressor wheel and a compressor housing, the compressor wheel being affixed to an opposite end of the rotatable shaft and being disposed in the compressor housing, the compressor wheel comprising a first impeller and a second impeller, the compressor housing defining a first air inlet for leading air into the first impeller, a second air inlet for leading air into the second impeller, a first compressor volute surrounding the first impeller and configured for receiving air pressurized by the first impeller, a crossover duct configured to lead pressurized air from the first compressor volute into the second air inlet, and a second compressor volute surrounding the second impeller and configured for receiving air pressurized by the second impeller, and an air discharge duct configured to lead air from the second compressor volute and out of the compressor housing for delivery to an intake manifold of an internal combustion engine;
the compressor housing further defining a bypass duct extending from one of the first compressor volute and the crossover duct, to the air discharge duct; and
a bypass valve disposed in the bypass duct, the bypass valve being movable between a closed position and an open position, the closed position preventing pressurized air in the first compressor volute from proceeding along the bypass duct so as to bypass the second impeller, the open position allowing pressurized air in the first compressor volute to proceed along the bypass duct so as to bypass the second impeller.

2. The turbocharger of claim 1 , wherein the bypass valve comprises a butterfly valve.

3. The turbocharger of claim 1 , wherein the first and second impellers are arranged in a back-to-back configuration.

4. The turbocharger of claim 3 , wherein the first air inlet leads air into the first impeller in a first axial direction and the second air inlet leads air into the second impeller in a second axial direction opposite to the first axial direction.

5. The turbocharger of claim 4 , wherein the crossover duct is configured to lead pressurized air out of the first compressor volute, then along the first axial direction past the second compressor volute, then into the second air inlet, the second air inlet being configured to lead the pressurized air radially inwardly and then to turn the pressurized air to proceed along the second axial direction into the second impeller.

6. The turbocharger of claim 5 , wherein the bypass duct extends between the crossover duct and the air discharge duct.

7. The turbocharger of claim 1 , wherein the nozzle of the turbine further comprises a variable-vane assembly regulating exhaust gas flow into the turbine wheel.

Assignees

• Honeywell Int Inc

Inventors

• Houst Vit
• Turecek Daniel
• Kares Vaclav
• Nejedly Milan
• Lednicky Ondrej
• Mokos Michal
• Oslejsek Zbynek

Classifications

• F02C6/12

  Turbochargers, i.e. plants for augmenting mechanical power output of internal-combustion piston engines by increase of charge pressure · CPC title

• F04D29/4206

  especially adapted for elastic fluid pumps · CPC title

• F02B37/013 Primary

  with exhaust-driven pumps arranged in series · CPC title

• F01D5/02

  Blade-carrying members, e.g. rotors (rotors of non-bladed type F01D1/34; stators F01D9/00 {; selecting particular materials F01D5/28}) · CPC title

• F04D17/14

  with means for changing the flow-path through the stages, e.g. series-parallel, e.g. side-loads, (surge control F04D27/02) · CPC title