Invention Grant
US09352827B2 Hydraulic shimmy damper for aircraft landing gear 有权
用于飞机起落架的液压振动阻尼器

  • Patent Title: Hydraulic shimmy damper for aircraft landing gear
  • Patent Title (中): 用于飞机起落架的液压振动阻尼器
  • Application No.: US13813048
    Application Date: 2011-07-28
  • Publication No.: US09352827B2
    Publication Date: 2016-05-31
  • Inventor: Marin Besliu
  • Applicant: Marin Besliu
  • Applicant Address: CA Ontario
  • Assignee: Messier-Dowty Inc.
  • Current Assignee: Messier-Dowty Inc.
  • Current Assignee Address: CA Ontario
  • Agency: Sughrue Mion, PLLC
  • Priority: CA2711199 20100729
  • International Application: PCT/CA2011/050464 WO 20110728
  • International Announcement: WO2012/012904 WO 20120202
  • Main IPC: B64C25/50
  • IPC: B64C25/50 F16F9/32 F16F9/06 F16F13/00
Hydraulic shimmy damper for aircraft landing gear
Abstract:
A hydraulic shimmy damper that resolves drawbacks in several known shimmy dampers, such as damping characteristics that are dependent on oil temperature variations. The disclosed shimmy damper includes a hydraulic compensator (40) having an internal fluid volume that is significantly more important than a fluid volume expelled from the body of the shimmy damper when its piston moves fore and aft. The shimmy damper also includes a hydraulic manifold (30) arranged between the body and the hydraulic compensator and defining a transfer channel between chambers in the piston that is connected to the hydraulic compensator. The manifold receives interchangeable hydraulic cartridge-type valves (CV1,RV1; CV2,RV2) for metering the fluid flowing from the chambers to the transfer channel, and allows the fluid to freely enter the chambers from the transfer channel. The present shimmy damper is therefore much less sensitive to oil temperature variation under intense shimmy.
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