发明名称 |
METHOD TO PILOT USING FLEXIBLE PROFILE |
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. |
申请公布号 |
EP3032047(A1) |
申请公布日期 |
2016.06.15 |
申请号 |
EP20150196647 |
申请日期 |
2015.11.27 |
申请人 |
ROLLS-ROYCE CORPORATION |
发明人 |
LACOMBE, SAMUEL;BAILEY, PATRICK |
分类号 |
F01D25/26;F01D25/28 |
主分类号 |
F01D25/26 |
代理机构 |
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代理人 |
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主权项 |
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地址 |
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