- 专利标题: Modular fan for a gas turbine engine
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申请号: US14943058申请日: 2015-11-17
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公开(公告)号: US10436151B2公开(公告)日: 2019-10-08
- 发明人: Brandon Wayne Miller , Randy M. Vondrell , Darek Tomasz Zatorski , Daniel Alan Niergarth
- 申请人: General Electric Company
- 申请人地址: US NY Schenectady
- 专利权人: General Electric Company
- 当前专利权人: General Electric Company
- 当前专利权人地址: US NY Schenectady
- 代理机构: Dority & Manning, P.A.
- 主分类号: F02K3/06
- IPC分类号: F02K3/06 ; F02C3/04 ; F02C7/36 ; F01D5/06
摘要:
A gas turbine engine includes a core and a tie shaft. The tie shaft is rotatable about an axial direction of the gas turbine engine by the core of the gas turbine engine. The gas turbine engine additionally includes a modular fan having a plurality of fan blades and a frame. The plurality fan blades are attached to the frame and the frame is slidably received on the tie shaft of the gas turbine engine. The modular fan additionally includes an attachment member removably attaching the frame to the tie shaft of the gas turbine engine to removably install the modular fan in the gas turbine engine.
公开/授权文献
- US20170138307A1 MODULAR FAN FOR A GAS TURBINE ENGINE 公开/授权日:2017-05-18
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