- 专利标题： Method to pilot using flexible profile
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申请号： US16531828申请日： 2019-08-05
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公开(公告)号： US11035241B2公开(公告)日： 2021-06-15
- 发明人: Samuel J. Lacombe , Patrick E. Bailey
- 申请人： Rolls-Royce Corporation
- 申请人地址： US IN Indianapolis
- 专利权人： Rolls-Royce Corporation
- 当前专利权人： Rolls-Royce Corporation
- 当前专利权人地址： US IN Indianapolis
- 代理机构： Barnes & Thornburg LLP
- 主分类号： F01D5/02
- IPC分类号： F01D5/02 ; F01D11/00 ; F01D9/04 ; F01D25/28 ; F01D25/26
摘要：
A fan assembly for use in a gas turbine engine of an aircraft includes a fan disk having a number of fan blades and a windage shield coupled to the fan disk to move therewith. The fan assembly supplies air for use in the engine. The windage shield rotates with the fan disk during operation of the gas turbine engine and directs air supplied by the fan blade.
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