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1.发明授权Variable area nozzle for gas turbine engines driven by shape memory alloy actuators 有权由形状记忆合金致动器驱动的燃气涡轮发动机的可变面积喷嘴公开(公告)号：US06318070B1
公开(公告)日：2001-11-20
申请号：US09517937
申请日：2000-03-03
申请人： Nancy M. Rey , Robin M. Miller , Thomas G. Tillman , Robert M. Rukus , John L. Kettle , James R. Dunphy , Zaffir A. Chaudhry , David D. Pearson , Kenneth C. Dreitlein , Constantino V. Loffredo , Thomas A. Wynosky
发明人： Nancy M. Rey , Robin M. Miller , Thomas G. Tillman , Robert M. Rukus , John L. Kettle , James R. Dunphy , Zaffir A. Chaudhry , David D. Pearson , Kenneth C. Dreitlein , Constantino V. Loffredo , Thomas A. Wynosky
IPC分类号： F02K302
CPC分类号： F02K1/1207 , F03G7/065 , F05D2300/505 , Y02T50/671 , Y10T74/20
摘要： A gas turbine engine includes a variable area nozzle having a plurality of flaps. The flaps are actuated by a plurality of actuating mechanisms driven by shape memory alloy (SMA) actuators to vary fan exist nozzle area. The SMA actuator has a deformed shape in its martensitic state and a parent shape in its austenitic state. The SMA actuator is heated to transform from martensitic state to austenitic state generating a force output to actuate the flaps. The variable area nozzle also includes a plurality of return mechanisms deforming the SMA actuator when the SMA actuator is in its martensitic state.
摘要翻译： 燃气涡轮发动机包括具有多个翼片的可变区域喷嘴。 翼片由形状记忆合金（SMA）致动器驱动的多个致动机构致动，以改变风扇存在的喷嘴面积。 SMA致动器在其马氏体状态下具有变形的形状，并且其奥氏体状态具有母体形状。 SMA致动器被加热以从马氏体状态转变为奥氏体状态，产生力输出以致动翼片。 可变区域喷嘴还包括当SMA致动器处于其马氏体状态时使SMA致动器变形的多个返回机构。
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公开(公告)号：US5833140A
公开(公告)日：1998-11-10
申请号：US764420
申请日：1996-12-12
CPC分类号： F02K1/11 , Y02T50/671
摘要： A variable exhaust nozzle (26) for a turbine engine nacelle (16) includes a pair of semi-cowls (58, 60) disposed about a longitudinally extending central axis (14) and a pair of corresponding shells (36, 38) each of which is spaced radially inwardly from the corresponding semi-cowl and is pivotable about a pivot axis (42, 44) between an extended position and a retracted position. The semi-cowls and shells have curved, geometrically similar inner and outer surfaces (86, 100) respectively so that gap (108) between the shells and the cowl is uniform irrespective of the angular orientation of the shells. A seal (128) which includes longitudinally extending legs (128a, 128b) and an optional circumferential leg (128c) prevents detrimental air leakage. Pivotal movement of the shells effects large changes in the discharge area A.sub.D of the nozzle without compromising the external aerodynamic characteristics of the nacelle. In one embodiment of the invention, each shell includes an extension (110) which facilitates the attainment of large area changes. The radial uniformity of gap (108) contributes to the durability and simplicity of the seal by ensuring that the seal is not repeatedly compressed and relaxed during operation of the nozzle.
摘要翻译： 用于涡轮发动机舱（16）的可变排气喷嘴（26）包括围绕纵向延伸的中心轴线（14）和一对相应的壳体（36,38）设置的一对半罩（58,60），每对 其从对应的半罩面径向向内间隔开，并且可在延伸位置和缩回位置之间绕枢转轴线（42,44）枢转。 半罩和贝壳分别具有弯曲的，几何相似的内表面和外表面（86,100），使得壳和罩之间的间隙（108）均匀，而与壳的角取向无关。 包括纵向延伸的腿部（128a，128b）和任选的圆周腿部（128c）的密封件（128）防止有害的空气泄漏。 壳体的枢转运动在喷嘴的排放面积AD上产生大的变化，而不损害机舱的外部空气动力特性。 在本发明的一个实施例中，每个壳包括有助于实现大面积变化的延伸部（110）。 间隙（108）的径向均匀性通过确保在喷嘴操作期间密封件不被重复压缩和松弛而有助于密封件的耐久性和简单性。
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3.发明申请APPARATUSES AND SYSTEMS WITH VERTICALLY AND LONGITUDINALLY OFFSET MOUNTING FLANGES 有权具有垂直和长期偏移安装法兰的装置和系统公开(公告)号：US20130153739A1
公开(公告)日：2013-06-20
申请号：US13327355
申请日：2011-12-15
CPC分类号： B64D27/26 , B64D27/00 , B64D27/16 , B64D2027/262 , B64D2027/268 , F02K3/10 , F05D2240/91 , F05D2250/312 , F05D2260/30 , F23R3/20 , F23R3/283
摘要： A flanged apparatus includes an apparatus body and a flanged mount, which includes a support pylon, a first mounting flange and a second mounting flange. The support pylon includes a first pylon segment, a second pylon segment and a routing notch. The first pylon segment is cantilevered from the apparatus body, and extends to the first mounting flange. The second pylon segment is cantilevered from the first pylon support, and extends from the first mounting flange to the second mounting flange. The routing notch extends vertically between the first pylon segment and the second pylon segment. The first mounting flange and the second mounting flange extend laterally from the support pylon, and the first mounting flange is separated from the second mounting flange by a longitudinal distance and a vertical distance.
摘要翻译： 一种带凸缘的装置包括装置主体和带凸缘的安装件，其包括支撑塔，第一安装凸缘和第二安装凸缘。 支撑塔包括第一吊架段，第二吊架段和路线槽。 第一个吊架段从装置主体悬臂，并延伸到第一安装法兰。 第二个吊架段从第一个支架支撑悬臂，并从第一安装法兰延伸到第二安装法兰。 导向槽在第一吊架段和第二吊架段之间垂直延伸。 第一安装凸缘和第二安装凸缘从支撑塔横向延伸，并且第一安装凸缘与第二安装凸缘分离，纵向距离和垂直距离。
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公开(公告)号：US20080236136A1
公开(公告)日：2008-10-02
申请号：US11693871
申请日：2007-03-30
IPC分类号： F02K9/66
CPC分类号： F01D25/04 , F01D17/105 , F01D17/141 , F02C9/18 , F02K1/822 , F02K3/075 , F05D2220/36 , F05D2260/52 , F05D2260/56 , F05D2260/96 , Y02T50/675
摘要： A linkage system includes a pivot bias assembly at each pivot which removes internal clearances and resultant vibratory wear. The pivot bias assembly includes a cavity which defines an axis transverse to the pivot axis. A spring biased piston is located therein to provide a radial load toward the rotation pivot to close radial clearances. The spring loaded piston reduces all the radial internal clearances to zero to reduce vibratory wear created by engine vibratory inputs. An assembly flat is positioned such that the component is assembled in a non-operating angular position such that the spring biased piston is under minimal or no load then the component is rotated into operating position so as to preload the spring biased piston.
摘要翻译： 联动系统包括在每个枢轴处的枢转偏压组件，其移除内部间隙并产生振动磨损。 枢轴偏置组件包括限定横向于枢转轴线的轴线的空腔。 弹簧偏置的活塞位于其中以朝向旋转枢轴提供径向负载以封闭径向间隙。 弹簧加载的活塞将所有径向内部间隙减小到零，以减少发动机振动输入产生的振动磨损。 组件平面被定位成使得部件组装在非操作角度位置，使得弹簧偏置的活塞处于最小或无负载，然后部件被转动到操作位置，以便预加载弹簧偏置的活塞。
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公开(公告)号：US5524847A
公开(公告)日：1996-06-11
申请号：US117464
申请日：1993-09-07
申请人： Robert F. Brodell , Edward J. Hovan , Steven T. Selfors , Constantino V. Loffredo , Paul W. Duesler
发明人： Robert F. Brodell , Edward J. Hovan , Steven T. Selfors , Constantino V. Loffredo , Paul W. Duesler
CPC分类号： B64D29/02 , B64C7/02 , B64D27/26 , B64D2027/264 , B64D2027/268 , Y02T50/44
摘要： A nacelle and mounting arrangement for a high bypass ratio ducted fan aircraft engine mounted external to the aircraft main structure is disclosed. The nacelle and mounting arrangement isolate the engine from the adverse effects of certain aerodynamic forces acting on the nacelle by transferring substantially all of those forces directly from the nacelle to the aircraft and transferring substantially none of those forces to the engine. Various arrangements of the nacelle components which facilitate engine removal while avoiding the placement of nacelle component interfaces in highly stressed regions of the nacelle are also disclosed.
摘要翻译： 公开了一种用于在飞机主体结构外部安装的高旁路比风扇飞机发动机的机舱和安装装置。 机舱和安装装置通过将基本上所有这些力直接从机舱转移到飞机并将这些力基本上不传递到发动机而将发动机与作用在机舱上的某些空气动力的不利影响隔离开来。 还公开了便于发动机移除同时避免在机舱的高应力区域中放置机舱部件接口的机舱部件的各种布置。
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公开(公告)号：US09719370B2
公开(公告)日：2017-08-01
申请号：US11693871
申请日：2007-03-30
CPC分类号： F01D25/04 , F01D17/105 , F01D17/141 , F02C9/18 , F02K1/822 , F02K3/075 , F05D2220/36 , F05D2260/52 , F05D2260/56 , F05D2260/96 , Y02T50/675
摘要： A linkage system includes a pivot bias assembly at each pivot which removes internal clearances and resultant vibratory wear. The pivot bias assembly includes a cavity which defines an axis transverse to the pivot axis. A spring biased piston is located therein to provide a radial load toward the rotation pivot to close radial clearances. The spring loaded piston reduces all the radial internal clearances to zero to reduce vibratory wear created by engine vibratory inputs. An assembly flat is positioned such that the component is assembled in a non-operating angular position such that the spring biased piston is under minimal or no load then the component is rotated into operating position so as to preload the spring biased piston.
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7.发明授权Variable area fan exhaust nozzle having mechanically separate sleeve and thrust reverser actuation systems 失效可变面积的风扇排气喷嘴具有机械分离的套筒和推力反向器致动系统
公开(公告)号：US5778659A
公开(公告)日：1998-07-14
申请号：US823294
申请日：1997-03-21
摘要： A gas turbine engine (10) includes a translating sleeve (38) disposed within a downstream portion of an outer nacelle (20). A variable area fan exhaust nozzle (30) is defined between the trailing edge (32) of the translating sleeve (38) and a conical core cowl (26) disposed radially inwardly of the outer nacelle (20) and spaced apart therefrom. The translating sleeve (38) translates downstream to cooperate with the decreasing diameter of the core cowl (26) to increase the area of the fan exhaust nozzle (30).
摘要翻译： 燃气涡轮发动机（10）包括设置在外部机舱（20）的下游部分内的平移套筒（38）。 可变区域风扇排气喷嘴（30）被限定在平移套管（38）的后缘（32）和设置在外部机舱（20）的径向内侧并与其间隔开的锥形芯罩（26）之间。 平移套筒（38）在下游平移以配合核心罩（26）的直径减小，以增加风扇排气喷嘴（30）的面积。
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8.发明授权Apparatuses and systems with vertically and longitudinally offset mounting flanges 有权具有垂直和纵向偏移安装法兰的装置和系统公开(公告)号：US08567745B2
公开(公告)日：2013-10-29
申请号：US13327355
申请日：2011-12-15
IPC分类号： F16M1/00
CPC分类号： B64D27/26 , B64D27/00 , B64D27/16 , B64D2027/262 , B64D2027/268 , F02K3/10 , F05D2240/91 , F05D2250/312 , F05D2260/30 , F23R3/20 , F23R3/283
摘要： A flanged apparatus includes an apparatus body and a flanged mount, which includes a support pylon, a first mounting flange and a second mounting flange. The support pylon includes a first pylon segment, a second pylon segment and a routing notch. The first pylon segment is cantilevered from the apparatus body, and extends to the first mounting flange. The second pylon segment is cantilevered from the first pylon support, and extends from the first mounting flange to the second mounting flange. The routing notch extends vertically between the first pylon segment and the second pylon segment. The first mounting flange and the second mounting flange extend laterally from the support pylon, and the first mounting flange is separated from the second mounting flange by a longitudinal distance and a vertical distance.
摘要翻译： 一种带凸缘的装置包括装置主体和带凸缘的安装件，其包括支撑塔，第一安装凸缘和第二安装凸缘。 支撑塔包括第一吊架段，第二吊架段和路线槽。 第一个吊架段从装置主体悬臂，并延伸到第一安装法兰。 第二个吊架段从第一个支架支撑悬臂，并从第一安装法兰延伸到第二安装法兰。 导向槽在第一吊架段和第二吊架段之间垂直延伸。 第一安装凸缘和第二安装凸缘从支撑塔横向延伸，并且第一安装凸缘与第二安装凸缘分离，纵向距离和垂直距离。
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