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专利名称：Rocket launcher发明人：増田 純一申请号：JP2015123463申请日：20150619公开号：JP6576703B2公开日：20190918
摘要：PROBLEM TO BE SOLVED: To provide a rocket launching device not only cableof being applied to a heavy weight airframe [from a middle type to a large type] but alsoshowing low air resistance applied to the airframe during its flight, showing no shockcaused by shearing or explosive devices at the time of launching, no increasing of inertmass of the airframe and the number of component elements, but capable of increasingreliability.SOLUTION: There are provided a side surface metal fitting 12 fixed to a sidesurface 3 of a rocket for generating thrust force in a single thrusting direction, a rail 14adjacent to the side surface metal fitting 12 and extending in the thrusting direction, anda hook 16 guided by the rail 14 at a holding position C that can be moved in the thrustingdirection so as to hold an attitude of the rocket at the holding position C. The rail 14 hasa guide groove 15 for guiding the hook 16 in the thrusting direction. The hook 16 has apair of oscillating parts 18 circulating in opposite directions to each other around arotating shaft 17 extending in the thrusting direction from the holding position C to areleasing position O. The pair of oscillating parts 18 are held at the holding position C bya prescribed distance from the launching of the rocket and subsequently they are turnedin opposite directions to each other.SELECTED DRAWING: Figure 2
申请人：株式会社ＩＨＩエアロスペース
地址：東京都江東区豊洲三丁目１番１号
国籍：JP
代理人：堀田 実,野村 俊博
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