Patent · US Expired

Aircraft control yoke

US5921507A · kind A · utility

6Cited by
10References
46Claims
0Family size

Assignee

Inventors

Key dates

Filing dateMay 16, 1994
Grant dateJul 13, 1999
Priority date
Expiry dateMay 16, 2014

Classification

  • Technology area (CPC B)Performing Operations; Transporting
  • CPC primaryB64D2201/00
  • WIPO fieldTransport
  • WIPO sectorMechanical engineering

Abstract

An airbag module is positioned relative to an aircraft control yoke or shaft, the airbag being actuated by majority voting sensors that are responsive to acceleration forces upon the aircraft. The aircraft control yoke or control yoke post is constructed to telescope, extend, or move a limited distance toward the pilot as the airbag inflates. The yoke carries telescoping, extendable, or movable handle portions that allow left and right hand pilot grip handles to move, if necessary, under the force of the expanding airbag. Hand sleeves may be provided to help maintain the pilot's hands on the grip handles during airbag expansion. The movable yoke and handle portions may be manually or automatically restored to normal operative positions after airbag deflation. The yoke may be formed so as to provide a U shaped section that accommodates a horizontal support or table for holding the airbag module, a map, or a like device. The U shaped yoke and table support members are structured such that the table remains horizontal during pivoting movement of the yoke to control aircraft roll, and during generally horizontal movement of the yoke to control aircraft pitch.

Source: USPTO / EPO open patent data. Objective bibliographic and citation counts.