Fail-safe lock for an airplane rudder
US4141520A · kind A · utility
Assignee
Inventors
Key dates
| Filing date | Jun 20, 1977 |
| Grant date | Feb 27, 1979 |
| Priority date | — |
| Expiry date | Jun 20, 1997 |
Classification
- Technology area (CPC Y)Emerging Cross-Sectional Technologies
- CPC primaryY10T292/0994
- WIPO fieldTransport
- WIPO sectorMechanical engineering
Abstract
A locking mechanism for a swingably mounted flight control surface member of an airplane, such as a rudder, which is embodied in a unitized frame structure that can be applied to either new or existing airplanes, which includes a bracket mounted assembly arranged for mounting within an enclosed portion such as the tail cone, in a position wherein a reciprocable locking bolt may be manually selectively moved by an outside ground attendant to a projecting position in locking engagement with a keeper carried by an adjacent part of the flight control member, and to a released retracted position. The bolt is connected to one end of a rocker arm carried by a rotatable shaft having an end extending to the exterior of the enclosed portion, and being arranged for releasably receiving an actuating tool. A spring urges the rocker arm, upon movement through a dead-center position, into limit positions corresponding to the locking and unlocking positions of the bolt, and a switch is arranged for actuation at one of the operative positions of the bolt. A fail-safe feature includes an associated cam for moving the bolt from a locking position to an unlocking position in response to the movement o…
Source: USPTO / EPO open patent data. Objective bibliographic and citation counts.