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81. 发明专利

DE69111526T2 未知
公开(公告)号：DE69111526T2
公开(公告)日：1996-01-18
申请号：DE69111526
申请日：1991-05-30
申请人： ROLLS ROYCE PLC
发明人： WARD ANDREW GEORGE
IPC分类号： B64C15/02 , B64D33/04 , F02K1/56 , F02K1/64 , F02K1/76
摘要： A gas turbine engine (10) is provided with a thrust reverser (16). In order to avoid inadvertent operation of the thrust reverser (16) when the gas turbine engine (10) is not running, a safety switch (19) is provided on the engine (10) at a position remote from the thrust reverser (16). The thrust reverser control system is arranged so that when the engine (10) is not running the thrust reverser (16) will only operate when the safety switch (19) is being manually operated.

82. 发明专利

DE69300685D1 未知
公开(公告)号：DE69300685D1
公开(公告)日：1995-11-30
申请号：DE69300685
申请日：1993-02-18
申请人： HUREL DUBOIS AVIONS
发明人： STANDISH ROBERT
IPC分类号： F02K1/56 , F02K1/70

83. 发明专利

AT129779T 未知
公开(公告)号：AT129779T
公开(公告)日：1995-11-15
申请号：AT92402458
申请日：1992-09-09
申请人： HISPANO SUIZA SA
发明人： CARIMALI FELIX , LEGRAS MICHEL JEAN LUCIEN
IPC分类号： F02K1/56 , F02K1/60 , F02K1/70

84. 发明专利

FR2687733A1 未知
公开(公告)号：FR2687733A1
公开(公告)日：1993-08-27
申请号：FR9202230
申请日：1992-02-26
申请人： HUREL DUBOIS AVIONS
发明人： STANDISH ROBERT
IPC分类号： F02K1/56 , F02K1/70

85. 发明专利

GB2226084A VARIABLE AREA JET ENGINE EXHAUST NOZZLE 未知
公开(公告)号：GB2226084A
公开(公告)日：1990-06-20
申请号：GB8918335
申请日：1989-08-11
申请人： GEN ELECTRIC
发明人： NASH DUDLEY OWEN , CROFT STEVEN JOHN , BOBO MELVIN
IPC分类号： B64C15/02 , B64D33/04 , F02K1/00 , F02K1/12 , F02K1/56 , F02K1/82

86. 发明专利

GB2188886B THRUST DEFLECTORS FOR TURBOMACHINE PROPULSION NOZZLES 未知
公开(公告)号：GB2188886B
公开(公告)日：1990-01-31
申请号：GB8706686
申请日：1987-03-20
申请人： ROLLS ROYCE PLC
发明人： TAPE ROBERT FRANCIS
IPC分类号： B64C25/42 , B64D33/04 , F02K1/00 , F02K1/56 , F02K1/60

87. 发明专利

NL184377B 未知
公开(公告)号：NL184377B
公开(公告)日：1989-02-01
申请号：NL7905588
申请日：1979-07-18
申请人： SNECMA
IPC分类号： F02K1/76 , F02K1/56
摘要： Device for hydraulic control of thrust reversal units activated by jacks in a jet engine. The jacks are connected to a rotary hydraulic engine fed by a hydraulic circuit which involves a mechanism for slowing down the speed of the reversal units when they approach the stop units. The hydraulic circuit allows for directly subjecting the engine's capacity to the opposing load on the engine. Application of this invention is possible to a dual flow turbojet in which the reversal units rotate in the cold flow.

88. 发明专利

DE3463821D1 DEVICE FOR INCREASING AND DEFLECTING THRUST OF JET-PROPULSION ENGINE OF V/STOL AIRCRAFT 未知
公开(公告)号：DE3463821D1
公开(公告)日：1987-06-25
申请号：DE3463821
申请日：1984-01-25
申请人： FUJI HEAVY IND LTD
发明人： HORINOUCHI SHIGERU , TANAKA ATSUSHI
IPC分类号： B64C15/02 , F02K1/00 , F02K1/36 , F02K1/78 , F02K1/56
摘要： In a vertical/short takeoff and landing (V/STOL) aircraft in which the exhaust gas from a jet-propulsion engine is discharged through an exhaust gas passage, secondary air induction passages (14, 14) are formed on the outer sides of the nozzle (12) for communicatively connecting the outside atmosphere to the upstream end of the exhaust gas passage (13), thereby to induct outside air as secondary air, into the exhaust gas passage (13) to be mixed with the exhaust gas. … Inlet flap gates (15, 15) are respectively provided at the inlet ends of the secondary air induction passages (14, 14). … A deflector device (22) is provided at the outlet part of the exhaust gas passage (13).

89. 发明专利

DE2823206C2 未知
公开(公告)号：DE2823206C2
公开(公告)日：1987-03-05
申请号：DE2823206
申请日：1978-05-25
申请人： THE BOEING CO., SEATTLE, WASH., US
发明人： RODOLPH, PETER KLAUS CHRISTOPH, SEATTLE, WASH., US
IPC分类号： B64D33/00 , B64D33/04 , F02K1/60 , F02K1/56
摘要： A cascade/clamshell thrust reverser combination for jet engines wherein the clamshell door in the full-forward thrust mode position, covers a cascade arrangement of vane members provided in the annular engine casing. For obtaining the thrust reverser mode, a track and pivot mechanism is employed. Initially, the door moves backwards on the track while simultaneously slightly rotating so that the total movement of the door follows a predetermined arc. During this initial movement the first portion of the vanes are gradually exposed. Upon continuation towards the full reverser mode, the door will move into a rotating movement thereby fully exposing all vanes and closing the forward thrust nozzle opening. The successive combined track/pivot movement to a pivot rotating movement allows for the maneuvering of a maximum large structural sized clamshell door within the multiple contoured confines of the exit casing, thereby providing the most optimum thrust reverser effect. The invention further resides in tailoring or varying the discharge angles of the vane members of the cascade from front to rear to maintain the effective discharge area for the engine essentially constant during inflight partial deployment of the clamshell door.

90. 发明专利

FR2481748B1 未知
公开(公告)号：FR2481748B1
公开(公告)日：1986-11-21
申请号：FR8108579
申请日：1981-04-29
申请人： ROLLS ROYCE
发明人： HITCHCOCK MALCOLM CHARLES
IPC分类号： F02K1/56 , F02K1/60 , F02K1/12 , B64D33/04

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