- 专利标题: Turbine engine advanced cooling system
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申请号: US14871382申请日: 2015-09-30
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公开(公告)号: US10208668B2公开(公告)日: 2019-02-19
- 发明人: Joseph Clegg , Craig English , Behram Kapadia , Kenneth M. Pesyna , Jason Lee Swindle , Jason Wayne Rector , Christopher Vincent , Nicholas D. Metzger , Daniel G. Edwards
- 申请人: Rolls-Royce Corporation , Rolls-Royce North American Technologies Inc.
- 申请人地址: US IN Indianapolis US IN Indianapolis
- 专利权人: ROLLS-ROYCE CORPORATION,ROLLS-ROYCE NORTH AMERICAN TECHNOLOGIES INC.
- 当前专利权人: ROLLS-ROYCE CORPORATION,ROLLS-ROYCE NORTH AMERICAN TECHNOLOGIES INC.
- 当前专利权人地址: US IN Indianapolis US IN Indianapolis
- 代理机构: Brinks Gilson & Lione
- 主分类号: F02C7/12
- IPC分类号: F02C7/12 ; F01D5/08 ; F01D25/08 ; F02C7/18 ; F01D5/04 ; F01D5/02 ; F01D25/12 ; F02C3/04 ; F02C7/24 ; F04D29/32 ; F04D29/58 ; F02C6/08
摘要:
A cooling system for a gas turbine is provided that may include a drive shaft, a shield of a combustor of the gas turbine engine, and a conduit. The drive shaft may be configured to mechanically couple a compressor of the gas turbine engine to a turbine of the gas turbine engine. The shield may be positioned between the compressor and the turbine. The combustor may be configured to drive the turbine. The conduit may be configured to supply a cooling fluid to a gap between an outer surface of the drive shaft and the shield of the combustor.
公开/授权文献
- US20170089263A1 TURBINE ENGINE ADVANCED COOLING SYSTEM 公开/授权日:2017-03-30