发明公开
- 专利标题: COMPRESSOR RIM THERMAL MANAGEMENT
- 专利标题(中): 散热管理压缩机花圈
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申请号: EP14885609申请日: 2014-12-18
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公开(公告)号: EP3090163A4公开(公告)日: 2017-01-04
- 发明人: LYONS CHRISTOPHER B
- 申请人: UNITED TECHNOLOGIES CORP
- 专利权人: UNITED TECHNOLOGIES CORP
- 当前专利权人: UNITED TECHNOLOGIES CORP
- 优先权: US201361921823 2013-12-30
- 主分类号: F02C7/12
- IPC分类号: F02C7/12 ; F01D5/08 ; F01D9/06 ; F01D25/12 ; F02C7/18
摘要:
A flow system for use in a gas turbine engine includes a diffuser case strut defining a first opening at a first radial end, a second opening at a second radial end, and a strut passage radially therethrough between the first and second openings. A first chamber wall and a second chamber wall define a first mixing chamber disposed radially inward of the diffuser case strut in fluid communication with the strut passage. A third chamber wall extends between the second flowpath wall and the second chamber wall to define a second mixing chamber disposed between the diffuser case strut and the first mixing chamber. The second flowpath wall and the second chamber wall are shaped to form a venturi in the second mixing chamber.
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