Login| Sign Up| Help| Contact|

Patent Searching and Data


Title:
DUAL-SHAFT POWER GENERATION GAS TURBINE
Document Type and Number:
WIPO Patent Application WO/2022/105214
Kind Code:
A1
Abstract:
A dual-shaft power generation gas turbine, comprising a first rotor system and a second rotor system. The first rotor system comprises a first rotating shaft (100), a first motor (200), a compressor (300), a first turbine (400) and a combustion chamber (500). An exhaust end of the gas compressor (300) is in communication with an inlet end of the combustion chamber (500), and an exhaust end of the combustion chamber (500) is in communication with a gas inlet end of the first turbine (400). The second rotor system comprises a second rotating shaft (600), a second turbine (700), and a second motor (800). The first rotating shaft (100) and the second rotating shaft (600) are coaxially arranged. An exhaust end of the first turbine (400) is in communication with a gas inlet end of the second turbine (700).

More Like This:
JP2015524532Dual end drive gas turbine
JPH03500797[Title of the Invention] High-pressure middle cooling turbine engine
Inventors:
JIN XINZHONG (CN)
Application Number:
PCT/CN2021/099968
Publication Date:
May 27, 2022
Filing Date:
June 15, 2021
Export Citation:
Click for automatic bibliography generation   Help
Assignee:
TECHNOLOGIES’ XANADU OF RESONATORY SOLAR SYSTEMED CO LTD (CN)
International Classes:
F02C3/10; F02C6/00; F02C7/00; F02C7/12; F04D29/02; F04D29/057; F04D29/28; F04D29/30; F04D29/42; F04D29/66
Foreign References:
CN112502833A2021-03-16
CN111042921A2020-04-21
CN207080404U2018-03-09
CN111058945A2020-04-24
CN105579690A2016-05-11
CN105909389A2016-08-31
US10047678B22018-08-14
CN104213987A2014-12-17
CN109478861A2019-03-15
CN111042925A2020-04-21
Attorney, Agent or Firm:
BEIJING JIATU PATENT ATTORNEY LAW FIRM (CN)
Download PDF:
View/Download PDF      PDF Help



 
Previous Patent: MULTI-ROTOR MICRO GAS TURBINE, AND STARTING METHOD THEREFOR

Next Patent: MOTOR-EMBEDDED BEARING TYPE MICRO GAS TURBINE