发明申请
- 专利标题: AIRCRAFT PROPULSION UNIT
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申请号: US16074578申请日: 2017-02-03
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公开(公告)号: US20190040816A1公开(公告)日: 2019-02-07
- 发明人: Carmen Gina ANCUTA , Kevin Morgane LEMARCHAND , Olivier KERBLER , Melody SERISET
- 申请人: SAFRAN AIRCRAFT ENGINES , SAFRAN NACELLES
- 申请人地址: FR Paris FR Gonfreville L'orcher
- 专利权人: SAFRAN AIRCRAFT ENGINES,SAFRAN NACELLES
- 当前专利权人: SAFRAN AIRCRAFT ENGINES,SAFRAN NACELLES
- 当前专利权人地址: FR Paris FR Gonfreville L'orcher
- 优先权: FR1650897 20160204
- 国际申请: PCT/FR2017/050251 WO 20170203
- 主分类号: F02K1/76
- IPC分类号: F02K1/76 ; B64D33/04 ; F01D25/16 ; F02K1/72
摘要:
An aircraft propulsion assembly including a bypass turbojet having a stationary inter-compressor casing positioned upstream from a space between passages, a nacelle including at its downstream end an inner wall that defines the outside of the space between passages and the inside of the bypass stream flow passage, and an outer wall arranged around the inner wall and that defines the outside of the bypass stream flow passage, at least a portion of the inner wall being suitable for moving between a maintenance position and a working position, and a thrust-reverser including a downstream element of the outer wall that is movable in translation between a retracted position and a thrust-reversal position in which it allows bypass stream deflector elements to be deployed in a radial direction, the deployment of the stream deflector elements being controlled by guide rods.
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