Title:
セミレバー式着陸装置および関連方法
Document Type and Number:
Japanese Patent JP5596218
Kind Code:
B2
Abstract:
A method of positioning landing gear of an airplane is provided that includes providing the landing gear including a shock strut, a truck beam operatively pivotally connected to the shock strut, first and second interconnected links operatively connected to the truck beam and a third link extending between the shock strut and the first and second links with the third link pivotally connected to the second link at a third pivot. When the landing gear is commanded to a lowered position, the third pivot is positioned in a first position to support a taxi mode, a take-off mode and a landing mode if the landing gear is operational and in a second position to support an alternate landing mode if the landing gear is not fully operational. When the landing gear is commanded to a raised position, the third pivot is in the second position to support a stow mode.
Inventors:
Moeller and Mitchell El.
Long and Michael Ey.
Oder and Richard B.
Long and Michael Ey.
Oder and Richard B.
Application Number:
JP2013501270A
Publication Date:
September 24, 2014
Filing Date:
February 23, 2011
Export Citation:
Assignee:
The Boeing company The Boeing Company
International Classes:
B64C25/34; B64C25/18
Attorney, Agent or Firm:
Yoshitaka Sonoda
Yoshinori Kobayashi
Yoshinori Kobayashi