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111. 发明专利

FR2741910A1 未知
公开(公告)号：FR2741910A1
公开(公告)日：1997-06-06
申请号：FR9514137
申请日：1995-11-30
申请人： HISPANO SUIZA SA
发明人： GONIDEC PATRICK , VAUCHEL GUY BERNARD
IPC分类号： F02K1/70 , F02K3/02 , F02K1/64 , F02K1/72
摘要： The thrust reversal system consists of several flaps which form part of the jet engine's outer wall when closed. The flaps open to deflect the flow of gases forwards. Each flap has outer and inner walls and a hinged rear section (121). The inner surface of it forms part of the outer wall of the flow duct when closed. The flow tends to hold in its closed position. The rear hinged section of each flap consists of a panel which is pivoted to the main flap at its forward end and actuated by a mechanical connector linked to the main flap drive. When the main flap is in its deployed position, the rear section is situated outside the main flow and to the rear of the flap, where it forms a cavity (36). The main flap's drive is in the form of a power cylinder, and the connector can be in the form of a pivoted arm or a spring.

112. 发明专利

DE69111526D1 未知
公开(公告)号：DE69111526D1
公开(公告)日：1995-08-31
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.

113. 发明专利

GB2161862A Double flow turbine engine equipped with a thrust reverser 未知
公开(公告)号：GB2161862A
公开(公告)日：1986-01-22
申请号：GB8418395
申请日：1984-07-19
申请人： GIRAUD PIERRE
发明人： GIRAUD PIERRE
IPC分类号： F02K1/38 , F02K1/60 , F02K1/64 , F02K1/74 , F02K3/02 , F02K1/54
摘要： In order to reduce the effectiveness of a mixing device 6 for the hot and cold flows C,F of the engine when the doors 8,9 of a thrust reverser are deployed, movable flaps 12 are provided to selectively block at least some of the cold flow channels 7.

114. 发明专利

IT1068895B 未知
公开(公告)号：IT1068895B
公开(公告)日：1985-03-21
申请号：IT2819676
申请日：1976-10-11
申请人： ROLLS ROYCE
IPC分类号： B64D33/00 , F02K1/64 , F02C
摘要： Gas turbine engine power plants sometimes are provided with thrust reversing equipment, the outlet of which is close to the power plant air intake. Such arrangements create re-ingestion problems. There is described herein an apparatus which either maintains the upstream portion of reversed flow in a given position with respect to the plane of the air intake or alternatively destroys the reversed flow entirely.

115. 发明专利

DE2844739A1 未知
公开(公告)号：DE2844739A1
公开(公告)日：1979-05-10
申请号：DE2844739
申请日：1978-10-13
申请人： ROLLS ROYCE
发明人： SMITH THOMAS ERIC , PALMER CHARLES ROBER
IPC分类号： F02K1/64 , B64D33/00 , F02K1/60 , F02K1/74 , B64C15/06

116. 发明专利

GB1506588A GAS TURBINE ENGINE POWER PLANTS FOR AIRCRAFT 未知
公开(公告)号：GB1506588A
公开(公告)日：1978-04-05
申请号：GB4175175
申请日：1975-10-11
申请人： ROLLS ROYCE
IPC分类号： B64D33/00 , F02K1/64 , B64C15/04 , B64C21/00 , F02K1/20 , B64C21/04
摘要： 1506588 Aircraft thrust reversers ROLLS ROYCE Ltd 5 Oct 1976 [11 Oct 1975] 41751/75 Heading F2R [Also in Division B7] In a gas-turbine-engine thrust reverser fan air is directed over the outer surface of the engine cowl 30 by the Coanda effect, and the location at which this forwardly moving air impinges against the relatively rearwardly moving ambient air is controlled to avoid reingestion. As the aircraft speed decreases the stagnation area 34 of high pressure moves forwardly until a sensor 36 detects its presence. The sensor includes valves (not shown) which are spring-biased closed, and the detected high pressure is sufficient to overcome the springs and open the valves to permit compressed air from the compressor 38 to escape radially from the cowl via a conduit and pressure adjuster 42. In an alternative embodiment, Fig. 3, the sensor comprises two pitot tubes 44, 46 which receive ambient air flow and reversed air flow, respectively, and are connected to a fluidic device 50. A double-headed piston 52 is operated by the fluidic device to control a butterfly valve 56 located in a conduit 54 which feeds compressed air to a Coanda-effect producing nozzle 22a. The fluidic devices of two similar engines may be connected (Fig. 4, not shown) to obviate asymmetric thrust reversal in the event of one of the engine thrust reversers malfunctioning.

117. 发明专利

FR2163688B1 未知
公开(公告)号：FR2163688B1
公开(公告)日：1977-12-23
申请号：FR7244797
申请日：1972-12-15
申请人： ROLLS ROYCE
IPC分类号： B64D27/16 , F02K1/64 , F02K3/00 , F04D29/00

118. 发明专利

DE2645349A1 未知
公开(公告)号：DE2645349A1
公开(公告)日：1977-04-21
申请号：DE2645349
申请日：1976-10-07
申请人： ROLLS ROYCE 1971 LTD
发明人： SMITH THOMAS ERIC
IPC分类号： B64D33/00 , F02K1/64 , B64C15/06
摘要： Gas turbine engine power plants sometimes are provided with thrust reversing equipment, the outlet of which is close to the power plant air intake. Such arrangements create re-ingestion problems. There is described herein an apparatus which either maintains the upstream portion of reversed flow in a given position with respect to the plane of the air intake or alternatively destroys the reversed flow entirely.

119. 发明专利

IT971846B 未知
公开(公告)号：IT971846B
公开(公告)日：1974-05-10
申请号：IT3288872
申请日：1972-12-14
申请人： ROLLS ROYCE 1971 LTD
IPC分类号： B64D27/16 , F02K1/64 , F02C

120. 发明专利

IT963706B 未知
公开(公告)号：IT963706B
公开(公告)日：1974-01-21
申请号：IT2785172
申请日：1972-08-03
申请人： ROLLS ROYCE 1971 LTD
IPC分类号： F02K1/64 , B64D33/00 , C09D5/23 , C09D7/12 , F02K1/68 , F02C

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