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1. 发明公开

EP2113649A3 A gas turbine engine exhaust nozzle having a composite article comprising a shape memory material member 无效转让
标题翻译：一种燃气涡轮发动机排气喷嘴，其具有包含形状记忆材料构件的复合制品
公开(公告)号：EP2113649A3
公开(公告)日：2017-10-18
申请号：EP09250772.2
申请日：2009-03-19
申请人： Rolls-Royce plc
发明人： Webster, John Richard
IPC分类号： F02K1/10 , F02K1/12 , F02K1/48
CPC分类号： F02K1/10 , F02K1/12 , F02K1/48 , F05D2300/505 , F05D2300/603 , Y02T50/672 , Y10T428/249924
摘要： A composite article (18, 20) comprises a composite member (30), a flexible member (36) and at least one shape memory material member (38). The composite member (30) has longitudinally extending fibres (34) in a matrix material (32). The at least one shape memory material member (38) extends substantially parallel to the composite member (30) and the flexible member (36) is positioned between the composite member (30) and the at least one shape memory material member (38) to bond the at least one shape memory material member (38) to the composite member (30). The composite article is particularly suitable for use as a tab (18, 20) for an exhaust nozzle (12, 14) of a turbofan gas turbine engine (10)
摘要翻译：复合制品（18,20）包括复合构件（30），柔性构件（36）和至少一个形状记忆材料构件（38）。复合构件（30）具有在基体材料（32）中的纵向延伸的纤维（34）。所述至少一个形状记忆材料构件（38）基本上平行于所述复合构件（30）延伸，并且所述柔性构件（36）定位在所述复合构件（30）与所述至少一个形状记忆材料构件（38）将至少一个形状记忆材料构件（38）结合到复合构件（30）。复合制品特别适合用作涡轮风扇燃气涡轮发动机（10）的排气喷嘴（12,14）的接头（18,20）

2. 发明公开

EP2462330A2 HIGH STIFFNESS SHAPE MEMORY ALLOY ACTUATED AEROSTRUCTURE 有权
标题翻译：强度高，形状记忆合金担任航空结构件
公开(公告)号：EP2462330A2
公开(公告)日：2012-06-13
申请号：EP10763898.3
申请日：2010-07-16
申请人： The Boeing Company , Widdle Jr., Richard D.
发明人： WIDDLE JR., Richard D. , GRIMSHAW, Matthew T. , CROSSON-ELTURAN, Kava S. , MABE, James Henry , CALKINS, Frederick T. , GRAVATT, Lynn Marie , SHOME, Moushumi
IPC分类号： F02K1/00 , B05B12/00
CPC分类号： F02K1/10 , B64C2027/7288 , F02K1/386 , F03G7/065 , F05D2250/184 , F05D2300/505 , Y02T50/34 , Y02T50/672
摘要： A shape memory alloy (SMA) actuated aerostructure operable to dynamically change shape according to flight conditions is disclosed. Deformable structures are actuated by SMA actuators that are coupled to face sheets of the deformable structures. Actuating the SMA actuators produces complex shape changes of the deformable structures by activating shape changes of the SMA actuators. The SMA actuators are actuated via an active or passive temperature change based on operating conditions. The SMA actuated aerostructure can be used for morphable nozzles such as a variable area fan nozzle and/or a variable geometry chevron of a jet engine to reduce engine noise during takeoff without degrading fuel burn during cruise.

3. 发明公开

EP2074307A1 TRANSLATING CORE COWL HAVING AERODYNAMIC FLAP SECTIONS 有权转让
标题翻译：具有气动折叠部分翻译INSIDE HOOD
公开(公告)号：EP2074307A1
公开(公告)日：2009-07-01
申请号：EP06851135.1
申请日：2006-10-12
申请人： United Technologies Corporation
发明人： LEVASSEUR, Glenn
IPC分类号： F02K1/10
CPC分类号： F02K3/06 , F02K1/08 , F02K1/10 , F02K1/15
摘要： An example core nacelle for a gas turbine engine includes a core cowl positioned adjacent an inner duct boundary of a fan bypass passage having an associated discharge airflow cross-sectional area. The core cowl includes at least one translating section and at least one flap section. The translating section of the core cowl is selectively moveable to vary the discharge airflow cross-sectional area.

4. 发明公开

EP2472089A3 Flade discharge in 2-d exhaust nozzle 有权
标题翻译： Flade-Entladung在2-D-Auspuffdüse
公开(公告)号：EP2472089A3
公开(公告)日：2017-03-29
申请号：EP11194560.6
申请日：2011-12-20
申请人： General Electric Company
发明人： Lariviere, Erin Lee , Ettorre, Stephen Michael
IPC分类号： F02K1/82 , F02K3/072 , F02K3/075 , F02K3/077 , F02K3/10 , F02K7/16 , F02C9/20 , F02K1/08 , F02K1/10 , F02K3/062 , F02K3/065 , F02K3/08 , F02K1/06 , F02K1/30 , F02K1/09
CPC分类号： F02K1/82 , F02C9/20 , F02K1/06 , F02K1/08 , F02K1/09 , F02K1/10 , F02K1/30 , F02K3/062 , F02K3/065 , F02K3/072 , F02K3/075 , F02K3/077 , F02K3/08 , F02K3/10 , F02K7/16
摘要： An aircraft gas turbine engine (10) has a row of FLADE fan blades (5) disposed radially outwardly of and drivingly connected to a fan (31) in the engine's fan section (14). The FLADE fan blades (5) extend across a FLADE duct (3) circumscribing the fan section (14). A two dimensional air discharge passage (81) is in fluid flow communication with the FLADE duct (3) and with FLADE air upstream and downstream discharge slots (400, 402) in a divergent flap (360) of a two dimensional exhaust nozzle (300). A valve fully closes the upstream slot (400) when the downstream slot (402) is fully opened and fully opens the upstream slot (400) when the downstream slot (402) is fully closed. The upstream and downstream slots (400, 402) may be located upstream and downstream respectfully of a nozzle discharge area (408) in the nozzle (300). A sliding deck (412) slides aft or down to open upstream slot (400) and close downstream slot (402) and slides forward or up to close upstream slot (400) and open downstream slot (402).
摘要翻译：飞机燃气涡轮发动机（10）具有排列在发动机的风扇部分（14）中的风扇（31）的径向向外并与其驱动连接的FLADE风扇叶片（5）。 FLADE风扇叶片（5）延伸穿过限定风扇部分（14）的FLADE导管（3）。二维空气排出通道（81）与二维排气喷嘴（300）的发散翼（360）与FLADE管道（3）流体流动连通，并且FLADE空气上游和下游排放槽（400,402））。当下游槽（402）完全打开时，阀完全关闭上游槽（400），并且当下游槽（402）完全关闭时，阀完全打开上游槽（400）。上游和下游槽（400,402）可以相对于喷嘴（300）中的喷嘴排出区域（408）位于上游和下游。滑动板（412）向后或向下滑动以打开上游槽（400）并关闭下游槽（402）并向前或向上滑动以闭合上游槽（400）并打开下游槽（402）。

5. 发明公开

EP2536941A2 ARTICULATING SLIDER TRACK 审中-公开
标题翻译：关节滑块轨道
公开(公告)号：EP2536941A2
公开(公告)日：2012-12-26
申请号：EP11751969.4
申请日：2011-02-11
申请人： General Electric Company
发明人： STUART, Alan, Roy , FEHRMANN, John, Robert , COX, Melanie, Zoe
IPC分类号： F02K1/08 , F02K1/09 , F02K1/66 , F02K1/80 , F02K1/10
CPC分类号： F01D25/28 , F02K1/08 , F02K1/09 , F02K1/10 , F02K1/763 , F02K1/80
摘要： A variable fan nozzle assembly includes a cow] member mounted on a slider track. The slider track may be articulated relative to a support member to slightly modify the position of the cowl member to vary the fan nozzle exit area. At least one 4-bar linkage may be utilized to allow articulation of the slider track responsive to an actuator. A method for varying a fan nozzle exit area includes mounting a first slider track in articulatable relationship with a support member; mounting a first cowl member in slidable relationship with a first slider track such that a fan nozzle is at least partially defined by a surface of the first cowl member; varying the operational, position of the first cowl member by articulating the first slider track without sliding the first cowl member with respect to the first slider track to vary the fan nozzle exit area.
摘要翻译：可变风扇喷嘴组件包括安装在滑块轨道上的母牛构件。滑块轨道可以相对于支撑构件铰接以稍微改变罩部件的位置以改变风扇喷嘴出口区域。至少一个4连杆机构可用于响应于致动器而允许滑块轨道的铰接。用于改变风扇喷嘴出口区域的方法包括：将第一滑块轨道安装成与支撑构件成可铰接关系; 以可滑动的关系安装第一整流罩构件，所述第一整流罩构件与第一滑动轨道相关，使得风扇喷嘴至少部分地由所述第一整流罩构件的表面限定; 通过铰接第一滑块轨道来改变第一外壳构件的操作位置，而不使第一外壳构件相对于第一滑块轨道滑动以改变风扇喷嘴出口区域。

6. 发明授权

EP2074321B1 FAN VARIABLE AREA NOZZLE WITH ADAPTIVE STRUCTURE AND METHOD OF VARYING A FAN EXIT AREA OF A GAS TURBINE ENGINE 有权转让
标题翻译： WITH CHANGE FOR IN出口横截面的燃气涡轮吹塑喷嘴的自适应结构和方法旁通喷嘴VARIABLE出口部
公开(公告)号：EP2074321B1
公开(公告)日：2012-12-05
申请号：EP06851899.2
申请日：2006-10-12
申请人： United Technologies Corporation
发明人： CHAUDHRY, Zaffir
IPC分类号： F02K3/02 , F02K3/075
CPC分类号： F02K3/025 , F02K1/10 , F05D2220/36 , F05D2250/62 , F05D2260/40311 , F05D2260/56

7. 发明公开

EP2472089A2 Flade discharge in 2-d exhaust nozzle 有权
标题翻译：在2-D排气喷管肉饼放电
公开(公告)号：EP2472089A2
公开(公告)日：2012-07-04
申请号：EP11194560.6
申请日：2011-12-20
申请人： General Electric Company
发明人： Lariviere, Erin Lee , Ettorre, Stephen Michael
IPC分类号： F02K1/82 , F02K3/072 , F02K3/075 , F02K3/077 , F02K3/10 , F02K7/16 , F02C9/20 , F02K1/08 , F02K1/10
CPC分类号： F02K1/82 , F02C9/20 , F02K1/06 , F02K1/08 , F02K1/09 , F02K1/10 , F02K1/30 , F02K3/062 , F02K3/065 , F02K3/072 , F02K3/075 , F02K3/077 , F02K3/08 , F02K3/10 , F02K7/16
摘要： An aircraft gas turbine engine (10) has a row of FLADE fan blades (5) disposed radially outwardly of and drivingly connected to a fan (31) in the engine's fan section (14). The FLADE fan blades (5) extend across a FLADE duct (3) circumscribing the fan section (14). A two dimensional air discharge passage (81) is in fluid flow communication with the FLADE duct (3) and with FLADE air upstream and downstream discharge slots (400, 402) in a divergent flap (360) of a two dimensional exhaust nozzle (300). A valve fully closes the upstream slot (400) when the downstream slot (402) is fully opened and fully opens the upstream slot (400) when the downstream slot (402) is fully closed. The upstream and downstream slots (400, 402) may be located upstream and downstream respectfully of a nozzle discharge area (408) in the nozzle (300). A sliding deck (412) slides aft or down to open upstream slot (400) and close downstream slot (402) and slides forward or up to close upstream slot (400) and open downstream slot (402).

8. 发明公开

EP1944496A3 Variable area nozzle with woven sleeve extension 有权转让
标题翻译：排气喷嘴具有可变横截面的组织通过膨胀套筒的装置
公开(公告)号：EP1944496A3
公开(公告)日：2011-10-19
申请号：EP08250041.4
申请日：2008-01-07
申请人： United Technologies Corporation
发明人： Cini, Colin L. , Baran, Kenneth C.
IPC分类号： F02K1/09 , F02K1/10
CPC分类号： F02K1/09 , F02K1/10 , F02K1/82 , F02K3/06 , F05D2300/6012 , Y02T50/672
摘要： The invention relates to gas turbine engines and a method for controlling gas turbine engines. The gas turbine engine having a variable area fan nozzle (40) including a nozzle section that is attachable to the gas turbine engine for influencing flow through the fan bypass passage (30) of the gas turbine engine. The nozzle section (40) is movable between a first length (60) and a second length (60') that is larger than the first length (60) to influence the flow. For example, the nozzle section includes members (56) that are woven together to form collapsible openings (66) that are open when the nozzle section (40) is moved to the first length (60) and that are closed when the nozzle section is moved to the second length (60').

9. 发明公开

EP2063095A2 Tuyère de soufflante à section réglable 有权转让
标题翻译： Fandüsemit verstellbarem Durchmesser
公开(公告)号：EP2063095A2
公开(公告)日：2009-05-27
申请号：EP08169654.4
申请日：2008-11-21
申请人： SNECMA
发明人： Dijoud, Delphine, Edith , Fauvelet, Benoît, Marc, Michel , Vincent, Thomas, Alain, Christian
IPC分类号： F02K1/12 , F02K1/46 , F02K3/06 , F02K1/10
CPC分类号： F02K3/06 , B64D33/04 , F02K1/10 , F02K1/46 , F05D2300/50212 , F05D2300/505 , Y02T50/67 , Y02T50/672
摘要： Variation de la section du flux d'air en sortie de soufflante en fonction des conditions de vol.
Selon l'invention la tuyère comprend une couronne de panneaux (16) déformables agencés à proximité de son bord de fuite, chaque panneau ayant une structure du type bilame (25, 26) à deux matériaux présentant des coefficients de dilatation différents et des moyens de chauffage (30) commandés étant thermiquement couplés à l'ensemble des panneaux.
摘要翻译：喷嘴具有梯形可变形板（16），齿形布置在喷嘴的边缘附近。由绝热材料制成的内部叶片（25）和外部金属叶片（26）提供不同的膨胀系数，并且相互组装成一个由温度变化引起的由系数差引起的结构的变形。包括电阻器（30）的受控加热单元，例如电粘合电阻丝和电流源，被热耦合到面板的组件。

10. 发明授权

EP0111436B1 Tuyère à section variable pour un turboréacteur et avion comportant un tel équipement 失效
标题翻译：用于涡轮反应器的可变区域喷射器，以及包含这种设备的飞机
公开(公告)号：EP0111436B1
公开(公告)日：1986-09-10
申请号：EP83402364.0
申请日：1983-12-07
申请人： SOCIETE NATIONALE D'ETUDE ET DE CONSTRUCTION DE MOTEURS D'AVIATION, "S.N.E.C.M.A."
发明人： Bayle-Laboure, Gérard Joseph Pascal , Bouiller, Jean Georges , Buisson, Marc François Bernard , Soligny, Marcel Robert
IPC分类号： F02K1/06
CPC分类号： F02K1/10 , F02K1/006 , Y02T50/671

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