发明授权
US07870740B2 Turbojet engine comprising an afterburner duct cooled by a variable-throughput ventilation stream
有权
涡轮喷气发动机包括由可变通量通气流冷却的后燃器管道
- 专利标题: Turbojet engine comprising an afterburner duct cooled by a variable-throughput ventilation stream
- 专利标题(中): 涡轮喷气发动机包括由可变通量通气流冷却的后燃器管道
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申请号: US11741400申请日: 2007-04-27
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公开(公告)号: US07870740B2公开(公告)日: 2011-01-18
- 发明人: Jacques Marcel Arthur Bunel , Thierry Andre Emmanuel Cortes , Alain Pierre Page , Fabienne Vagner
- 申请人: Jacques Marcel Arthur Bunel , Thierry Andre Emmanuel Cortes , Alain Pierre Page , Fabienne Vagner
- 申请人地址: FR Paris
- 专利权人: SNECMA
- 当前专利权人: SNECMA
- 当前专利权人地址: FR Paris
- 代理机构: Oblon, Spivak, McClelland, Maier & Neustadt, L.L.P.
- 优先权: FR0651522 20060428
- 主分类号: F02K3/10
- IPC分类号: F02K3/10
摘要:
An afterbody for a turbojet engine is disclosed. The afterbody includes an afterburner casing, a thermal protection liner, and a diaphragm-forming assembly interposed between the liner and the casing. The diaphragm-forming assembly defines a flow area which is traversed by a ventilation stream. The diaphragm-forming assembly includes two annular plates overlapping one another, each being perforated with a plurality of apertures and being mounted on the liner and the casing respectively. The apertures jointly define the flow area of the assembly. Furthermore, the assembly is designed such that the expansion of the liner causes an angular displacement of the plate with respect to the plate, leading to an increase in the size of the flow area.
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