ガスタービンシステムおよびそれを備えた移動体

Title:

ガスタービンシステムおよびそれを備えた移動体

Document Type and Number:

Japanese Patent JP7297574

Kind Code:

B2

Abstract:

A gas turbine system includes: a compressor configured to compress external air to generate compressed air; a combustor configured to burn the compressed air together with fuel to generate a combustion gas; a turbine configured to be driven by the combustion gas; an exhaust unit configured to guide the combustion gas, which has passed through the turbine, to outside; a shell having a cylindrical shape and extending along an axis line about which the turbine is configured to rotate and being arranged so as to cover the compressor, the combustor, the turbine, and the exhaust unit; and an exit unit configured to guide the combustion gas, which has passed through the turbine, to a discharge port in the surface of the shell.

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Inventors:

Yuichi Nakaya
Yuki Morisaki
Yasuhiro Saiki

Application Number:

JP2019130169A

Publication Date:

June 26, 2023

Filing Date:

July 12, 2019

Export Citation:

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Assignee:

MITSUBISHI HEAVY INDUSTRIES,LTD.

International Classes:

F02K1/82; B64D27/24; F01D15/10; F01D25/08; F01D25/30; F02C6/00; F02C7/00; F02K1/34

Domestic Patent References:

JP2008144764A
JP2006205755A
JP2009512807A
JP201396414A
JP2010223167A

Foreign References:

US4215536
US4958489
US5203164
US4099375

Attorney, Agent or Firm:

Takaharu Fujita
Takaori Mitoma
Miki Kawakami
Daisuke Nagata

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