Invention Grant
US08157050B2 Device for reducing noise generated by an aircraft jet engine with curve ducts
有权
用于减少具有曲线导管的飞机喷气发动机产生的噪音的装置
- Patent Title: Device for reducing noise generated by an aircraft jet engine with curve ducts
- Patent Title (中): 用于减少具有曲线导管的飞机喷气发动机产生的噪音的装置
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Application No.: US12935423Application Date: 2009-03-31
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Publication No.: US08157050B2Publication Date: 2012-04-17
- Inventor: Jerome Huber , Jean-Paul Bonnet , Joel Delville , Peter Jordan , Francois Strekowski
- Applicant: Jerome Huber , Jean-Paul Bonnet , Joel Delville , Peter Jordan , Francois Strekowski
- Applicant Address: FR Toulouse FR Paris FR Poitier
- Assignee: Airbus Operations (S.A.S.),Centre National de la Recherche Scientifique (CNRS),Universitéde Poitiers
- Current Assignee: Airbus Operations (S.A.S.),Centre National de la Recherche Scientifique (CNRS),Universitéde Poitiers
- Current Assignee Address: FR Toulouse FR Paris FR Poitier
- Agency: Oblon, Spivak, McClelland, Maier & Neustadt, L.L.P.
- Priority: FR0852120 20080331
- International Application: PCT/FR2009/000374 WO 20090331
- International Announcement: WO2009/133271 WO 20091105
- Main IPC: F01K1/14
- IPC: F01K1/14

Abstract:
A jet engine, including a wall surrounding a first gas flow ejected from a downstream end of the wall along a longitudinal axis, a second flow of gas running outside the wall in a direction of ejection of the first gas flow, at least one duct arranged on the periphery of the downstream end of the wall which is desired to eject a gas flow for interacting with one and/or the other gas flow, the at least one duct including a terminal section provided at the free end thereof with an outlet opening through which the fluid is ejected. The terminal section successively includes a first section of straight duct aligned along a median axis and a second duct section forming a bend relative to the straight section, the second portion having a free end provided with the outlet opening and sufficiently close to the median axis of the first section to give the terminal section a reduced restriction in a direction of formation of the bend.
Public/Granted literature
- US20110042162A1 DEVICE FOR REDUCING NOISE GENERATED BY AN AIRCRAFT JET ENGINE WITH CURVE DUCTS Public/Granted day:2011-02-24
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