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Title:
TWO-STAGE COMPRESSION TYPE EXHAUST TURBINE SUPERCHARGER
Document Type and Number:
Japanese Patent JP2008208734
Kind Code:
A
Abstract:

To provide a two-stage compression type exhaust turbine supercharger capable of performing two-stage supercharging and reducing the size of the supercharger.

The two-stage compression type exhaust turbine supercharger 1 includes a turbine part 3 driven by exhaust gas 2 introduced from an internal combustion engine, and a low pressure stage compressor part 5 and a high pressure stage compressor part 6 driven by the turbine part 3 for pressure feeding outside air to the internal combustion engine. The turbine part 3 and a rotary shaft 9 of the low pressure stage compressor part 5, or the turbine part 3 and a rotary shaft 12 of the high pressure stage compressor part 6, are coupled to the rotary shaft 12 of the high pressure stage compressor part 6, or the rotary shaft 9 of the low pressure stage compressor part 5, and are rotated as one rotary shaft.


Inventors:
SHIRAISHI KEIICHI
Application Number:
JP2007044026A
Publication Date:
September 11, 2008
Filing Date:
February 23, 2007
Export Citation:
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Assignee:
MITSUBISHI HEAVY IND LTD
International Classes:
F02B37/00; F02B41/10
Attorney, Agent or Firm:
Noriharu Fujita
Kunio Ueda