Title:
航空機用車輪支持機構
Document Type and Number:
Japanese Patent JP4050885
Kind Code:
B2
Abstract:
An aircraft wheel support mechanism capable of reducing the impact to the tire at the time of landing and capable of reducing the impact to the tire at the time of the wheel colliding with an obstacle lying on the runway. The mechanism comprises a suspension mechanism (3) for rotatably supporting a wheel (13) by the lower end of a support member (2) connected to the fuselage, the suspension mechanism (3) having a crank shaft assembly (5), and is characterized in that the crank shaft assembly comprises a horizontal support shaft (51) rotatably supported by the lower end of the support member, an axle (52) for rotatably supporting the wheel, and an arm (53) positioned at right angles with the horizontal support shaft and axle for connecting one end of the horizontal support shaft to one end of the axle.
Inventors:
Kichi Koji Oka
Application Number:
JP2001268869A
Publication Date:
February 20, 2008
Filing Date:
September 05, 2001
Export Citation:
Assignee:
Kichi Koji Oka
Arze Co., Ltd.
Arze Co., Ltd.
International Classes:
B64C25/58; B64C25/00; B64C25/10; B64C25/42; B64C25/60
Domestic Patent References:
| JP60071394A |
Attorney, Agent or Firm:
Aoyama Aoi
Tadataka Omori
Yasushi Ohata
Tadataka Omori
Tadataka Omori
Yasushi Ohata
Tadataka Omori