Title:
航空機用の脚展開装置及び航空機の脚展開方法
Document Type and Number:
Japanese Patent JP6871000
Kind Code:
B2
Abstract:
PROBLEM TO BE SOLVED: To provide a landing gear deploying device for an aircraft, which can perform deploying and shock-absorbing of a landing gear of the aircraft with a simpler configuration.SOLUTION: A landing gear deploying device 1 for an aircraft has an expansion and contraction mechanism 3 and a motor 4. The expansion and contraction mechanism is connected to a landing gear 2A of the aircraft to deploy and store the landing gear and absorb a shock on the landing gear. The motor expands and contracts the expansion and contraction mechanism. In a method of deploying a landing gear of an aircraft, deployment and storage of the landing gear and shock-absorbing of the landing gear are performed using the landing gear deploying device for the aircraft. A control circuit 5 can exert control for mitigating a roll in wing low landing under the situation of a cross wind.SELECTED DRAWING: Figure 1
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| WO/2023/156511 | VARIABLE-LENGTH LANDING GEAR AND AIRCRAFT EQUIPPED WITH SUCH A LANDING GEAR |
| WO/2018/095238 | UNMANNED AERIAL VEHICLE AND UNDERCARRIAGE DEVICE THEREOF |
| WO/1998/024688 | AIRCRAFT LANDING GEAR ARRANGEMENT |
Inventors:
Hitomi Atsushi
Application Number:
JP2017015390A
Publication Date:
May 12, 2021
Filing Date:
January 31, 2017
Export Citation:
Assignee:
Subaru corporation
International Classes:
B64C25/12; B64C25/24; B64C25/26
Domestic Patent References:
| JP2012510405A |
Foreign References:
| US5875994 | ||||
| US20130105624 |
Attorney, Agent or Firm:
Takehiko Yamada
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