首页> 外国专利> DISTRIBUTED SLIDING RAILS OF THE HELICOPTER CABIN DOOR ON A CURVED AIRFRAME

DISTRIBUTED SLIDING RAILS OF THE HELICOPTER CABIN DOOR ON A CURVED AIRFRAME

机译:曲折飞机场上直升机机舱门的分布式滑轨

摘要

In order to enable convenient ingress and egress of the passenger/cargo into helicopters, it is imperative to provide wide cabin entry. In general, sliding doors are the prime option for wider entrance due to its versatility of construction in large sizes. Sliding doors require two or three long sliding rails to open and the rails must be straight. On small helicopters it is very difficult to get the sufficient straight surface to facilitate the sliding rails. Two unique methods that are reported here enables the sliding door provision by splitting the sliding rails and distributing them. Distribution would be, some portion on the door and the remaining portion on to the airframe surface. Sliding rails length distribution between door and-the airframe is about 40%-60% on the door and 60%-40% on the airframe respectively.
机译:为了使旅客/货物方便地进出直升机,必须提供宽敞的机舱入口。通常,由于滑动门的结构尺寸大,因此是更宽阔的入口的主要选择。滑动门需要两个或三个长的滑动滑轨才能打开,并且滑轨必须是直的。在小型直升机上,很难获得足够的直表面以方便滑轨。此处报告的两种独特方法是通过分开滑轨并分配滑轨来启用滑门。分布将是部分在门上,其余部分在机身表面。门与机身之间的滑轨长度分布分别在门上约为40%-60%,在机身上约为60%-40%。

著录项

  • 公开/公告号IN201641040006A

    专利类型

  • 公开/公告日2018-05-25

    原文格式PDF

  • 申请/专利权人

    申请/专利号IN201641040006

  • 发明设计人 LINGAIAH N;

    申请日2016-11-23

  • 分类号B64C1/00;

  • 国家 IN

  • 入库时间 2022-08-21 12:52:15

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