Invention Grant
US08596584B2 High-lift system for an aircraft with a main wing and an adjustable slat
有权
具有主翼和可调节板条的飞机的高升力系统
- Patent Title: High-lift system for an aircraft with a main wing and an adjustable slat
- Patent Title (中): 具有主翼和可调节板条的飞机的高升力系统
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Application No.: US12808959Application Date: 2008-12-22
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Publication No.: US08596584B2Publication Date: 2013-12-03
- Inventor: Thilo Knacke , Frank Thiele
- Applicant: Thilo Knacke , Frank Thiele
- Applicant Address: DE Hamburg
- Assignee: Airbus Operations GmbH
- Current Assignee: Airbus Operations GmbH
- Current Assignee Address: DE Hamburg
- Agency: Ingrassia Fisher & Lorenz P.C.
- Priority: DE102007061590 20071220
- International Application: PCT/EP2008/011042 WO 20081222
- International Announcement: WO2009/080355 WO 20090702
- Main IPC: B64C9/24
- IPC: B64C9/24 ; B64C21/06

Abstract:
A high-lift system for an aircraft with a main wing and a slat that by way of an adjustment device is adjustable relative to the main wing to various adjustment states, with a gap resulting between the rear of the slat, which rear faces the main wing, and the main wing, where the size of the gap results from the adjustment state of the slat relative to the main wing, where in the interior of the slat an air guidance channel with at least one inlet and an outlet is formed, where the inlet is arranged at the rear, which faces the main wing, in order to influence the airflow in the gap.
Public/Granted literature
- US20100258679A1 High-Lift System for an Aircraft with a Main Wing and an Adjustable Slat Public/Granted day:2010-10-14
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