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公开(公告)号:EP1479605A3
公开(公告)日:2008-05-07
申请号:EP04252900.8
申请日:2004-05-19
发明人: Shiraishi, Takayuki c/o Fuji Jukogyo Kabushiki K. , Tsuura, Seiichi c/o Fuji Jukogyo Kabushiki Kaisha , Kuramochi, Kenji c/o Fuji Jukogyo Kabushiki K.
摘要: A helicopter (1) having: a flow control device (8) provided at one of a lower portion of a side surface (2a) of a fuselage (2) and a portion on a lower surface (2a) of the fuselage (2) near the side surface (2a) and extending downward.
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公开(公告)号:EP1479605B1
公开(公告)日:2010-06-09
申请号:EP04252900.8
申请日:2004-05-19
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公开(公告)号:EP1479605A2
公开(公告)日:2004-11-24
申请号:EP04252900.8
申请日:2004-05-19
发明人: Shiraishi, Takayuki c/o Fuji Jukogyo Kabushiki K. , Tsuura, Seiichi c/o Fuji Jukogyo Kabushiki Kaisha , Kuramochi, Kenji c/o Fuji Jukogyo Kabushiki K.
摘要: A helicopter (1) having: a flow control device (8) provided at one of a lower portion of a side surface (2a) of a fuselage (2) and a portion on a lower surface (2a) of the fuselage (2) near the side surface (2a) and extending downward.
摘要翻译: 一种直升机(1),其具有:设置在机身(2)的侧面(2a)的下部和机身(2)的下表面(2a)的一部分中的一方的流量控制装置(8) 靠近侧面(2a)并向下延伸。
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