Invention Grant
US08763450B2 Locking fastening device, adjustable fastening device, component system, main wing of a wind tunnel model aircraft, and wind tunnel model aircraft having such a main wing 失效
锁紧紧固装置,可调紧固装置,部件系统,风洞模型飞机的主翼,以及具有这种主翼的风洞模型飞机

  • Patent Title: Locking fastening device, adjustable fastening device, component system, main wing of a wind tunnel model aircraft, and wind tunnel model aircraft having such a main wing
  • Patent Title (中): 锁紧紧固装置,可调紧固装置,部件系统,风洞模型飞机的主翼,以及具有这种主翼的风洞模型飞机
  • Application No.: US13309905
    Application Date: 2011-12-02
  • Publication No.: US08763450B2
    Publication Date: 2014-07-01
  • Inventor: Michael Binder
  • Applicant: Michael Binder
  • Applicant Address: DE Hamburg
  • Assignee: Airbus Operations GmbH
  • Current Assignee: Airbus Operations GmbH
  • Current Assignee Address: DE Hamburg
  • Agency: Jenkins, Wilson, Taylor & Hunt, P.A.
  • Main IPC: G01M9/00
  • IPC: G01M9/00 B64C1/06
Locking fastening device, adjustable fastening device, component system, main wing of a wind tunnel model aircraft, and wind tunnel model aircraft having such a main wing
Abstract:
A locking fastening device for fastening a first component to a second component, an adjustable fastening device for adjustably fastening a first component to a second component, and a component system including at least one first component that is fastened to a second component are described. Also described are a main wing of a wind tunnel model aircraft having an adjusting and fastening system which includes at least one locking fastening device and at least two adjustable fastening devices for adjusting and fastening an aerodynamic additional body that is adjustable relative to the main wing by means of a plurality of retaining devices, as well as a wind tunnel model aircraft having such a main wing.
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