发明名称 Bidimensional convergent nozzle with translatable cold flaps
摘要 The primary nozzle (4) has two hot shutters (5, 6) situated after the engine's primary duct and surrounded by its housing. The housing is extended by a secondary nozzle (20) actuated by a second control system (27a) and fitted with cold shutters (21, 22) operated by a third control system (29b) independently of the angular position of the hot shutters. The cold shutters are preferably two in number and eyelid shaped, hinged to and supported by transverse pivots (23a, 23b) fixed to lateral sliders (24a) operated by the second control system (27a).
申请公布号 EP0972930(A1) 申请公布日期 2000.01.19
申请号 EP19990401711 申请日期 1999.07.08
申请人 SOCIETE NATIONALE D'ETUDE ET DECONSTRUCTION DE MOTEURS D'AVIATION, "S.N.E.C.M.A." 发明人 BOUILLER, PHILIPPE PIERRE VINCENT;BOURQUIN, PIERRE YVES;COT, FABRICE MICHEL OLIVIER;KETTLER, DANIEL;RUIS, JEAN-PIERRE
分类号 F02K1/11;F02K1/82;(IPC1-7):F02K1/12 主分类号 F02K1/11
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