Invention Grant
US08006941B2 System for reducing aerodynamic noise at a supplementary wing of an aircraft
有权
用于降低飞机辅助翼面空气动力学噪音的系统
- Patent Title: System for reducing aerodynamic noise at a supplementary wing of an aircraft
- Patent Title (中): 用于降低飞机辅助翼面空气动力学噪音的系统
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Application No.: US12829831Application Date: 2010-07-02
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Publication No.: US08006941B2Publication Date: 2011-08-30
- Inventor: Thomas Lorkowski , Boris Grohmann
- Applicant: Thomas Lorkowski , Boris Grohmann
- Applicant Address: DE Hamburg
- Assignee: Airbus Deutschland GmbH
- Current Assignee: Airbus Deutschland GmbH
- Current Assignee Address: DE Hamburg
- Agency: Crowell & Moring LLP
- Priority: DE102004056537 20041123
- Main IPC: B64C3/50
- IPC: B64C3/50

Abstract:
A system for reducing aerodynamic noise of a supplementary wing of an aircraft is provided. The supplementary wing is hinged to a main wing and is extendable when a gap region between the main wing and the supplementary wing is opened. The system includes a separating surface which can be moved into the gap region when the supplementary wing is extended and which extends at least partially along a separation flow line between a vortex flow region and a gap flow for the air flowing in the gap region. The separating surface is an n-stable surface which through an actuator device can be moved between at least one of the stable states and at least one additional state.
Public/Granted literature
- US20100282900A1 System for Reducing Aerodynamic Noise at a Supplementary Wing of an Aircraft Public/Granted day:2010-11-11
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