- 专利标题: Ducted fan and aircraft
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申请号: US17177678申请日: 2021-02-17
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公开(公告)号: US11530034B2公开(公告)日: 2022-12-20
- 发明人: Yuki Morisaki , Kazuhiro Imai , Kai Karikomi , Yasuhiro Saiki
- 申请人: MITSUBISHI HEAVY INDUSTRIES, LTD.
- 申请人地址: JP Tokyo
- 专利权人: MITSUBISHI HEAVY INDUSTRIES, LTD.
- 当前专利权人: MITSUBISHI HEAVY INDUSTRIES, LTD.
- 当前专利权人地址: JP Tokyo
- 代理机构: Wenderoth, Lind & Ponack, L.L.P.
- 优先权: JPJP2020-051196 20200323
- 主分类号: B64C27/20
- IPC分类号: B64C27/20 ; B64C29/00
摘要:
A ducted fan includes a fan and a cowl having a cylindrical shape and including an introduction port configured to introduce air from a first end portion side. The fan includes a compressor blade provided on an outer circumferential side and a thrust blade provided on an inner circumferential side of the compressor blade. The cowl includes a housing portion configured to accommodate the compressor blade in an interior thereof, an outlet configured to allow air flowing through the housing portion to be blown therethrough by the compressor blade, and an inlet configured to suck air blown out. The outlet is provided inwards in a radial direction of the cowl and near the introduction port of the cowl, and the inlet is provided inwards in the radial direction of the cowl and between the outlet and the compressor blade in an axial line direction.
公开/授权文献
- US20210291973A1 DUCTED FAN AND AIRCRAFT 公开/授权日:2021-09-23
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