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Hydraulic actuation system for cargo doors with cam-type latches

机译:带有凸轮型闩锁的货舱门液压致动系统

摘要

A door actuation system for an outwardly opening aircraft door for use in an aircraft having a door opening, a cam post, and a plurality of latch pins. The door actuation system includes a locking mechanism operably coupled to the door, wherein the locking mechanism is positionable in a locked position preventing the door from being opened and an unlocked position. The system further includes a pull-in mechanism that is hydraulically actuated and includes a cam slot member capable of operably engaging the cam post of the aircraft. The pull-in mechanism is positionable in an uncammed position and a cammed position. A latching mechanism is also provided that is hydraulically actuated and includes a plurality of cam latches each capable of operably receiving one of the plurality of latch pins. The latching mechanism is positionable in a latched position and an unlatched position. The pull-in mechanism and the latching mechanism are capable of preventing opening of the door when the pull-in mechanism is in the cammed position and the latching mechanism is in the latched position, even if the locking mechanism is in the unlocked position.
机译:用于向外打开飞机门的门致动系统,其用于飞机中,具有门开口,凸轮柱和多个闩锁销。门致动系统包括可操作地联接至门的锁定机构,其中该锁定机构可定位在锁定位置以防止门被打开和处于解锁位置。该系统还包括被液压致动的拉入机构,并且包括能够与飞机的凸轮柱可操作地接合的凸轮槽构件。拉入机构可定位在非凸轮位置和凸轮位置。还提供了一种由液压致动的闩锁机构,其包括多个凸轮闩锁,每个凸轮闩锁能够可操作地接收多个闩锁销中的一个。闩锁机构可定位在闩锁位置和非闩锁位置。即使在锁定机构处于解锁位置的情况下,拉入机构和闩锁机构也能够在拉入机构处于凸轮位置并且闩锁机构处于闩锁位置时防止门打开。

著录项

  • 公开/公告号US6457675B1

    专利类型

  • 公开/公告日2002-10-01

    原文格式PDF

  • 申请/专利权人 THE BOEING COMPANY;

    申请/专利号US20010891582

  • 发明设计人 STEPHEN A. LOCANTORE;LEO W. PLUDE;

    申请日2001-06-25

  • 分类号B64C11/40;

  • 国家 US

  • 入库时间 2022-08-22 00:47:46

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