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Title:
GAS TURBINE STARTING DEVICE AND GAS TURBINE SYSTEM
Document Type and Number:
WIPO Patent Application WO/2016/135831
Kind Code:
A1
Abstract:
Provided is a gas turbine starting device (4) comprising the following: a planetary gear mechanism (11) that includes a sun gear (16), a planetary carrier (18) disposed on the outer circumference of the sun gear (16), and an inner gear (19) disposed on the outer circumference of the planetary carrier (18), the sun gear, planetary carrier, and inner gear serving as rotating bodies (12) rotating about an axis (O1), and that includes planetary gears (17) which are supported by the planetary carrier (18) and mesh with the sun gear (16) and the inner gear (19); and a variable speed power source (10) that has a rotor (23) which is connected to any one of the rotating bodies (12) in the planetary gear mechanism (11). A rotating shaft (2a) of a gas turbine (2) is connected to any one of the rotating bodies (12) other than the rotating body to which the variable speed power source (10) is connected. A rotating shaft (2a) of a pressurizing device (3) is connected to the one remaining rotating body (12) other than the rotating bodies to which the rotor (23) of the variable speed power source (10) and the rotating shaft (2a) of the gas turbine (2) are connected.

Inventors:
KOBAYASHI MASAHIRO (JP)
MORI YASUSHI (JP)
Application Number:
PCT/JP2015/055067
Publication Date:
September 01, 2016
Filing Date:
February 23, 2015
Export Citation:
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Assignee:
MITSUBISHI HEAVY IND COMPRESSOR CORP (JP)
International Classes:
F02C7/268; F01D15/12; F01D17/20
Foreign References:
JP2004506116A2004-02-26
JP2002155760A2002-05-31
JPS5741427A1982-03-08
GB2390871A2004-01-21
US2845776A1958-08-05
Attorney, Agent or Firm:
MORI Ryuichirou et al. (JP)
Woods Ryuichiro (JP)
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