发明名称 Convergent-divergent nozzle, particularly for jet engines
摘要 The convergent-divergent nozzle is constructed with beams, forming a box section (1), mounted longitudinally. The sides of the channel (1A and 1B) are joined by a plate (3) and the trailing edges of the two flanks are also joined by a flange (2). The window (2c) in the flange, along with the two flanks and the joining plate, form the exit passage from the box section. The flange also carries a synchronising bar (7), which is H shaped and which carries a central bar (7c), forming a lever, which is connected to the control lever (14), from the mechanism controlling the convergent (11) and divergent (12) flaps, which are fitted so that the leading edge (11a), of the convergent flap is hinged to the leading edge of the flanks and the trailing edge is hinged to the leading edge (12a) of the divergent flap.
申请公布号 FR2714422(A1) 申请公布日期 1995.06.30
申请号 FR19830000423 申请日期 1983.01.13
申请人 CAMBOULIVES ANDRE ALPHONSE MEDER 发明人 CAMBOULIVES ANDRE, ALPHONSE, MEDERIC, LEON
分类号 F02K1/12;(IPC1-7):F02K1/06;F02K1/78 主分类号 F02K1/12
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