发明名称 Slide door device for aircraft
摘要 A slide door device for an aircraft includes an upper guide roller at a tip end of an upper arm provided at an upper part of a slide door and a lower guide roller at a tip end of a lower arm provided at a lower part of the slide door that are rollably engaged with an upper guide rail and a lower guide rail that are fixed along an upper edge and a lower edge of a door opening frame formed in a fuselage of an aircraft, respectively. An intermediate guide roller, provided at a tip end of an intermediate arm provided in a door opening, is rollably engaged with an intermediate guide rail that is fixed to an inner surface of the slide door, while smoothly guiding the slide door with the upper guide rail, the lower guide rail, and the intermediate guide rail.
申请公布号 US8070102(B2) 申请公布日期 2011.12.06
申请号 US20090533822 申请日期 2009.07.31
申请人 KOBAYASHI MASAKI;YAMANOUCHI HIROSHI;HONDA MOTOR CO., LTD. 发明人 KOBAYASHI MASAKI;YAMANOUCHI HIROSHI
分类号 B64C1/14 主分类号 B64C1/14
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