Patent · US Active

Aircraft door arrangement

US9205909B2 · kind B2 · utility

0Cited by
7References
15Claims
0Family size

Assignee

Inventors

Key dates

Filing dateJan 27, 2014
Grant dateDec 8, 2015
Priority date
Expiry dateMar 14, 2034

Classification

  • Technology area (CPC B)Performing Operations; Transporting
  • CPC primaryB64C1/1415
  • WIPO fieldTransport
  • WIPO sectorMechanical engineering

Abstract

An aircraft door arrangement having a pivotable door for closing an aperture in the fuselage of an aircraft and selectively movable between closed and open positions by a linear actuating mechanism having a casing and a rod selectively extendable and retractable. An actuator mounting mounts the casing between two elements of the primary structure of the aircraft. The rod is pivotally coupled to the door. The actuator mounting includes a rigid mounting component including three legs extending in a common plane together with the casing and the rotation axis and each having a first and a second longitudinal end. The first and second legs symmetrically extend from the casing at an angle at opposite sides thereof. Each of the second ends of the first and second legs is rotatably coupled on the rotation axis to another one of the spaced elements of the primary structure of the aircraft.

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