发明申请
- 专利标题： Aircraft engine, fan thereof and fan stator vane thereof
- 专利标题（中）： 飞机发动机，风扇和风扇定子叶片
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申请号： US10796065申请日： 2004-03-10
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公开(公告)号： US20050008494A1公开(公告)日： 2005-01-13
- 发明人: Naoki Tsuchiya , Dai Kato
- 申请人： Naoki Tsuchiya , Dai Kato
- 申请人地址： JP Tokyo
- 专利权人： Ishikawajima-Harima Heavy Industries Co., Ltd.
- 当前专利权人： Ishikawajima-Harima Heavy Industries Co., Ltd.
- 当前专利权人地址： JP Tokyo
- 优先权： JP2003-091501 20030328
- 主分类号： F01D5/14
- IPC分类号： F01D5/14 ; F04D29/54 ; F04D29/66 ; B63H1/26
摘要：
A fan of an aircraft engine is provided with a rotating fan rotor for feeding air aftward as a spiral flow and a stator vane for rectifying the spiral flow to be an axial flow. The fan stator vane is provided with a hub end portion extending radially relative to a rotating axis of the fan rotor and a tip end portion leaning toward a suction side. Leading edges of the hub end portion and the tip end portion have sweepback angles of from 27 degrees to 33 degrees relative to a radial direction defined by the rotating axis.
公开/授权文献
- US07101145B2 Reduced noise aircraft stator vane 公开/授权日：2006-09-05