- 专利标题： Fan assembly of a gas turbine engine with a tip shroud
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申请号： US15812331申请日： 2017-11-14
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公开(公告)号： US10584714B2公开(公告)日： 2020-03-10
- 发明人: Jason Husband , James Glaspey
- 申请人： United Technologies Corporation
- 申请人地址： US CT Farmington
- 专利权人： UNITED TECHNOLOGIES CORPORATION
- 当前专利权人： UNITED TECHNOLOGIES CORPORATION
- 当前专利权人地址： US CT Farmington
- 代理机构： Cantor Colburn LLP
- 主分类号： F01D5/22
- IPC分类号： F01D5/22 ; F04D29/32 ; F02K3/06 ; F04D19/00 ; F04D29/66
摘要：
A fan of a gas turbine engine is provided. The fan having: a plurality of fan blades secured to a rotor, each of the plurality of fan blades having an airfoil secured to the rotor at one end and a tip portion that is secured to a shroud that circumscribes the plurality of fan blades.
公开/授权文献
- US10724535B2 Fan assembly of a gas turbine engine with a tip shroud 公开/授权日：2020-07-28
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