Title:
LANDING GEAR FOR AIRCRAFT
Document Type and Number:
Japanese Patent JPS60116598
Kind Code:
A
Abstract:
The landing gear comprises: a rod including nested first and second tubes between which there slides a cylinder whose outer end supports a running gear; a strut surrounding the top of the rod and including a steering mechanism cooperating with a rotary tube disposed between the rod and the strut; and a fluid actuator constituted by at least one chamber between the strut and the rod and having a feed inlet only. The landing gear is particularly applicable to helicopters that are required to "kneel down" camel fashion, e.g., for storage in the hold of an aircraft carrier or a cargo plane.
Inventors:
JIYATSUKU BOO
MITSUSHIERU DERIAN
MITSUSHIERU DERIAN
Application Number:
JP23653084A
Publication Date:
June 24, 1985
Filing Date:
November 09, 1984
Export Citation:
Assignee:
METSUSHIE ISUPAANO BIYUGATSUTE
International Classes:
B64C25/00; B64C25/58; B64C25/60; (IPC1-7): B64C25/00
Attorney, Agent or Firm:
Takashi Koshiba (1 person outside)