Invention Grant
- Patent Title: Flow body, in particular for aircraft
- Patent Title (中): 流体,特别是飞机
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Application No.: US13441944Application Date: 2012-04-09
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Publication No.: US08702042B2Publication Date: 2014-04-22
- Inventor: Martin Gerber , Geza Schrauf
- Applicant: Martin Gerber , Geza Schrauf
- 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: DE102009049049 20091012
- Main IPC: B64C21/02
- IPC: B64C21/02

Abstract:
A flow body is disclosed, particularly for aircraft. The flow body includes an outer side impinged on in a predetermined manner by a fluid in a direction of impinging flow, the flow body having on its outer side at least one flow control device including micro-perforations arranged in at least one segment of the outer side, at least one connecting passage communicated with the micro-perforations via at least one suction chamber so fluid flowing through the micro-perforations flows via the suction chamber into the connecting passage, at least one suction device having a first inlet communicated with the connecting passage, a second inlet communicated with at least one ram fluid feed line, wherein the ram fluid feed line is in a region of the flow body opposite to the direction of impinging flow of the flow body, and an outlet device for discharging the fluid.
Public/Granted literature
- US20130025727A1 FLOW BODY, IN PARTICULAR FOR AIRCRAFT Public/Granted day:2013-01-31
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