Invention Grant
US08646726B2 Method and apparatus for determining the apparent operational integrity of a no-back device 有权
用于确定无背装置的视在操作完整性的方法和装置

  • Patent Title: Method and apparatus for determining the apparent operational integrity of a no-back device
  • Patent Title (中): 用于确定无背装置的视在操作完整性的方法和装置
  • Application No.: US12997694
    Application Date: 2008-06-13
  • Publication No.: US08646726B2
    Publication Date: 2014-02-11
  • Inventor: David J Manzanares
  • Applicant: David J Manzanares
  • Applicant Address: US NY East Aurora
  • Assignee: Moog Inc.
  • Current Assignee: Moog Inc.
  • Current Assignee Address: US NY East Aurora
  • Agency: Phillips Lytle LLP
  • International Application: PCT/US2008/007434 WO 20080613
  • International Announcement: WO2009/151423 WO 20091217
  • Main IPC: B64C5/10
  • IPC: B64C5/10
Method and apparatus for determining the apparent operational integrity of a no-back device
Abstract:
This invention provides an improvement in a no-back device having a ball screw connected to a variable load of reversible polarity (±L) and having a portion penetrating a housing. The device includes a braking mechanism acting between the housing and the ball screw for producing a force that resists movement of the ball screw in the direction of an “aiding” load, but does not substantially resist movement of the ball screw in the direction of an “opposing” load. The improvement broadly includes: a first spring acting between the housing and the braking mechanism for exerting a first preload force (F1) on the braking mechanism for simulating the application of an external load on the ball screw in one of the directions; whereby the apparent operational integrity of the no-back device may be checked when no external load is applied to the ball screw. In use, the apparatus performs the steps of: providing a first spring; causing the first spring to exert a first preload force (F1) on the braking mechanism; determining the actual torque (Ta) required to move the ball screw while the aircraft is on the ground; comparing the actual torque with a theoretical torque (Tt) required to move the ball screw; and inferring that the no-back device is not operating correctly if the actual torque is less than the theoretical torque; thereby to test the apparent operational integrity of the no-back device when the aircraft is on the ground.
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