Invention Grant
US09272772B2 Surface element for an aircraft, aircraft and method for improving high-lift generation on a surface element
有权
用于飞机的表面元件，用于改善表面元件上的高升力产生的飞行器和方法
- Patent Title: Surface element for an aircraft, aircraft and method for improving high-lift generation on a surface element
- Patent Title (中): 用于飞机的表面元件，用于改善表面元件上的高升力产生的飞行器和方法
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Application No.: US13850414Application Date: 2013-03-26
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Publication No.: US09272772B2Publication Date: 2016-03-01
- Inventor: Daniel Reckzeh , Burkhard Goelling , Matthias Lengers
- Applicant: Airbus Operations GmbH
- Applicant Address: DE
- Assignee: Airbus Operations GmbH
- Current Assignee: Airbus Operations GmbH
- Current Assignee Address: DE
- Agency: Lerner, David, Littenberg, Krumholz & Mentlik, LLP
- Priority: EP12162149 20120329
- Main IPC: B64C21/04
- IPC: B64C21/04 ; B64C21/02 ; B64C9/24 ; B64C21/06
Abstract:
A surface element, e.g. a wing, of an aircraft includes a leading edge, a high lift device arrangement positioned along the leading edge and at least one add-on body positioned in a leading edge region, wherein the high lift device arrangement is interrupted in the region of at least one add-on body for preventing collision with the add-on body and wherein the surface element includes an arrangement of openings in a region covering the add-on body, which openings are connected to an air conveying device for conveying air through the openings. Thereby an additional flap for harmonizing the flow above a pylon or other add-on body can be eliminated.
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