Invention Grant
- Patent Title: Aerofoil comprising a high lift flap
- Patent Title (中): 包括高提升翼片的机翼
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Application No.: US13255276Application Date: 2010-03-29
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Publication No.: US08967550B2Publication Date: 2015-03-03
- Inventor: Bernhard Schlipf , Xavier Hue
- Applicant: Bernhard Schlipf , Xavier Hue
- 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.
- Priority: DE102009015330 20090327
- International Application: PCT/EP2010/001984 WO 20100329
- International Announcement: WO2010/108699 WO 20100930
- Main IPC: B64C9/22
- IPC: B64C9/22 ; B64C9/02 ; B64C9/16

Abstract:
A wing is provided, including a high-lift flap arranged on the wing such that it is movable by means of at least two adjustment mechanisms arranged side-by-side in the spanwise direction of the wing and adjustable by means of a drive device. Each adjustment mechanism includes a first adjustment lever, articulated on a main wing surface via a first pivotal articulation, with the formation of a first rotation axis; a second adjustment lever, articulated on the high-lift flap via a second pivotal articulation, with the formation of a second rotation axis; and a central articulation, linking together the first and the second adjustment levers, with the formation of a third rotation axis. An intermediate articulated part is arranged on at least one of the adjustment mechanisms for coupling the first adjustment lever and the main wing surface, or for coupling the second adjustment lever and the high-lift flap.
Public/Granted literature
- US20120061524A1 AEROFOIL COMPRISING A HIGH LIFT FLAP Public/Granted day:2012-03-15
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