发明公开
EP2811144A1 FAN ROTOR BLADE OF JET ENGINE FOR AIRCRAFT
有权
GEBLÄSEROTORSCHAUFELEINES FLUGZEUGTRIEBWERKS
- 专利标题: FAN ROTOR BLADE OF JET ENGINE FOR AIRCRAFT
- 专利标题(中): GEBLÄSEROTORSCHAUFELEINES FLUGZEUGTRIEBWERKS
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申请号: EP13744077.2申请日: 2013-01-30
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公开(公告)号: EP2811144A1公开(公告)日: 2014-12-10
- 发明人: YAGI, Hiroyuki , KUROKI, Hiroshi , OBUCHI, Kenro
- 申请人: IHI Corporation
- 申请人地址: 1-1, Toyosu 3-chome Koto-ku Tokyo 135-8710 JP
- 专利权人: IHI Corporation
- 当前专利权人: IHI Corporation
- 当前专利权人地址: 1-1, Toyosu 3-chome Koto-ku Tokyo 135-8710 JP
- 代理机构: Lamb, Martin John Carstairs
- 优先权: JP2012017134 20120130
- 国际公布: WO2013115207 20130808
- 主分类号: F02K3/06
- IPC分类号: F02K3/06 ; F02C7/00 ; F04D29/38
摘要:
A fan rotor blade (1) includes a blade body (10) made from a composite material of a resin and fibers, and having a pressure surface (10a) facing one side in a rotation direction and a suction surface (10b) facing the other side in the rotation direction. The blade body is provided with a sheath (20) which is more rigid than the blade body and is fixed to the blade body in a state where the sheath covers a leading edge portion of the blade body, which is located on an upstream side in the direction of intake of external air, and the vicinity thereof. A tip end portion (21b) of the sheath extends from the leading edge portion side of the blade body to a trailing edge portion side of the blade body. An end portion of the tip end portion (21b) of the sheath is flush with the trailing edge portion of the blade body.
公开/授权文献
- EP2811144B1 FAN ROTOR BLADE OF AIRCRAFT JET ENGINE 公开/授权日:2018-05-23
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