Title:
LANDING GEAR FOR FLIGHT VEHICLE
Document Type and Number:
Japanese Patent JP2023148642
Kind Code:
A
Abstract:
To provide a reusable landing gear for a flight vehicle.SOLUTION: A landing gear 2 for a flight vehicle 1 is used during landing. The landing gear 2 for the flight vehicle 1 comprises: a first cylinder structure 3A with an upper end rollably coupled to the flight vehicle 1; and a second cylinder structure with a lower end contactable with the ground, configured to be relatively movable in an axial direction along a reference axis CL with respect to the first cylinder structure 3A, and configured to be relatively rotatable about the reference axis CL with respect to the first cylinder structure 3A. The first cylinder structure 3A and the second cylinder structure 3B switch the landing gear 2 between a stowed state and a released state by means of the relative movement and the relative rotation.SELECTED DRAWING: Figure 1
Inventors:
ECHIZENYA TSUYOSHI
Application Number:
JP2022056780A
Publication Date:
October 13, 2023
Filing Date:
March 30, 2022
Export Citation:
Assignee:
HONDA MOTOR CO LTD
International Classes:
B64C25/10; B64C25/20; B64C25/62
Attorney, Agent or Firm:
田▲崎▼ 聡
Shingo Suzuki
Taichi Sakai
Shinichi Watanabe
Shingo Suzuki
Taichi Sakai
Shinichi Watanabe
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