发明申请
- 专利标题: Latch Pin Assembly
-
申请号: US15881248申请日: 2018-01-26
-
公开(公告)号: US20180148159A1公开(公告)日: 2018-05-31
- 发明人: Mark S. Good , Charles E. Jokisch
- 申请人: The Boeing Company
- 申请人地址: US IL Chicago
- 专利权人: The Boeing Company
- 当前专利权人: The Boeing Company
- 当前专利权人地址: US IL Chicago
- 主分类号: B64C3/56
- IPC分类号: B64C3/56 ; F15B15/26 ; B64C23/06 ; F15B11/00
摘要:
A folding wing tip system of an aircraft includes a latch pin actuator having a primary mechanical lock and a secondary hydraulic lock. The mechanical lock may include a lock cam movable between a lock position, in which the lock cam engages the latch pin, and an unlock position, in which the lock cam is disengaged from the latch pin, and a first lock actuator mechanically coupled to the lock cam and configured to provide a bias force pushing the lock cam toward the lock position. The hydraulic lock may be disposed in an unlatching hydraulic line and has an initial state, in which fluid flow through the unlatching hydraulic line is blocked thereby to hold the latch pin in the latched position, and an open state, in which fluid flow through the unlatching hydraulic line is permitted thereby to permit retraction of the latch pin to the unlatched position.
公开/授权文献
- US10173766B2 Latch pin assembly 公开/授权日:2019-01-08
信息查询