公开(公告)号：US20110171030A1

公开(公告)日：2011-07-14

申请号：US12954765

申请日：2010-11-26

申请人： Andrew SWIFT ,  Antony MORGAN

发明人： Andrew SWIFT ,  Antony MORGAN

IPC分类号： F01D7/00

CPC分类号： F01D7/00 ,  B64C11/308 ,  B64D2027/005 ,  F01D1/26 ,  F01D21/18 ,  F02C7/36 ,  F02C9/58 ,  F02K3/072 ,  F05D2220/324 ,  F05D2250/44 ,  Y02T50/66 ,  Y02T50/673

摘要： A back-up featherer for an engine arrangement having a main hydraulic actuator which angularly displaces propellers of a propeller assembly of the engine arrangement, and fluid supply lines for transferring hydraulic fluid between a hydraulic pressure power source located on a static structure of the engine arrangement and the main hydraulic actuator. The back-up featherer has a back-up actuator assembly for angular displacement of the propellers, the back-up actuator assembly rotating with the propeller assembly, a signal detector operatively connected to the back-up actuator assembly and rotates with the propeller assembly, and a back-up rotating coupling. A static side of the back-up rotating coupling is mounted to the static structure of the engine arrangement and communicates with a regulator located on a static structure of the engine arrangement. A rotating side of the back-up hydraulic rotating coupling rotates with the propeller assembly and communicates with the signal detector.

摘要翻译： 一种用于发动机装置的备用专利，其具有主要液压致动器，该主液压致动器成角度地置换发动机装置的螺旋桨组件的螺旋桨，以及用于在位于发动机装置的静态结构上的液压动力源之间传送液压流体的流体供应管线 和主液压执行机构。 后备专家具有用于螺旋桨角位移的后备执行机构组件，支承致动器组件与螺旋桨组件一起旋转，信号检测器可操作地连接到备用致动器组件并与螺旋桨组件一起旋转， 和备用旋转联轴器。 备用旋转联轴器的静态侧安装到发动机装置的静态结构，并与位于发动机装置的静态结构上的调节器连通。 后备液压旋转联轴器的旋转侧与螺旋桨组件一起旋转，并与信号检测器通信。

公开(公告)号：US20110164978A1

公开(公告)日：2011-07-07

申请号：US12956457

申请日：2010-11-30

申请人： Andrew SWIFT ,  Antony MORGAN

发明人： Andrew SWIFT ,  Antony MORGAN

IPC分类号： F01D7/00

CPC分类号： F02K3/062 ,  B64C11/308 ,  B64C11/385 ,  B64C11/40 ,  B64D2027/005 ,  F02K3/072 ,  F05D2220/324 ,  F05D2260/76 ,  F05D2260/79 ,  F05D2270/094 ,  Y02T50/66 ,  Y02T50/671

摘要： A back-up featherer is provided for an engine arrangement having a main hydraulic actuator which angularly displaces propellers of a propeller assembly of the engine arrangement. The back-up featherer has a back-up hydraulic actuator for angular displacement of the propellers, the back-up hydraulic actuator rotating with the propeller assembly. The back-up featherer further has one or more back-up fluid supply lines for transferring hydraulic fluid between a hydraulic pressure power source located on a static structure of the engine arrangement and the back-up hydraulic actuator. The back-up featherer further has a back-up hydraulic rotating coupling, the back-up fluid supply lines fluidly communicating with the back-up hydraulic actuator via the back-up rotating coupling. A static side of the back-up hydraulic rotating coupling is mounted to the static structure of the engine arrangement, and a rotating side of the back-up hydraulic rotating coupling rotates with the propeller assembly.

摘要翻译： 提供了一种用于具有主液压致动器的发动机装置的备用专利，所述主液压致动器成角度地置换发动机装置的螺旋桨组件的螺旋桨。 后备专家具有用于螺旋桨角位移的备用液压致动器，后备液压致动器与螺旋桨组件一起旋转。 后备专家还具有一个或多个备用流体供应管线，用于在位于发动机装置的静态结构的液压动力源和后备液压致动器之间传送液压流体。 备用设备还具有备用液压旋转联轴器，备用流体供应线路通过备用旋转联轴器与后备液压致动器流体连通。 备用液压旋转联轴器的静态侧安装在发动机装置的静止结构上，后备液压旋转联轴器的旋转侧与螺旋桨组件一起旋转。

公开(公告)号：US06971855B2

公开(公告)日：2005-12-06

申请号：US10724629

申请日：2003-12-02

申请人： Martyn Richards ,  Kenneth F Udall ,  Andrew Swift

发明人： Martyn Richards ,  Kenneth F Udall ,  Andrew Swift

IPC分类号： F01D5/30 ,  F04D29/34 ,  F01D5/32

CPC分类号： F04D29/34 ,  F01D5/3015

摘要： A blade arrangement for a gas turbine engine includes a plurality of blades mounted for rotation on a disc so as to extend radially therefrom and a retention member, the retention member including an attachment portion which is attached to the disc and an abutment portion for resisting forward axial movement of at least one of the blades relative to the disc. The blade arrangement further comprises restraint means spaced from the attachment portion of the retention member, for substantially preventing radially outward movement of the abutment portion of the retention member when a forward axial force is applied by the blade to the abutment portion.

摘要翻译： 用于燃气涡轮发动机的叶片装置包括多个叶片，其安装成用于在盘上旋转以从其径向延伸并且具有保持构件，所述保持构件包括附接到盘的附接部分和用于抵抗向前的邻接部分 至少一个叶片相对于盘的轴向运动。 叶片装置还包括与保持构件的附接部分间隔开的约束装置，用于当刀片向邻接部分施加向前的轴向力时，基本上防止保持构件的邻接部分的径向向外移动。

公开(公告)号：US08851849B2

公开(公告)日：2014-10-07

申请号：US12954782

申请日：2010-11-26

申请人： Andrew Swift ,  Antony Morgan

发明人： Andrew Swift ,  Antony Morgan

IPC分类号： B64C11/28 ,  B64C11/32

CPC分类号： B64C11/32 ,  Y02T50/66

摘要： A pitch change apparatus is provided for a propeller assembly having a row of propeller blades which rotate around an axis of the assembly. The apparatus has a unison ring which is coaxial with the propeller assembly. The unison ring is movable to drive respective mechanisms for varying the pitch of the blades. The apparatus further has a plurality of pitch lock assemblies circumferentially distributed around the unison ring. Each pitch lock assembly has a free state which allows movement of the unison ring and a locked state which prevents or limits movement of the unison ring and thus prevents or limits variation of the pitch of the blades. The pitch lock assembly moves from the free to the locked state when the assembly receives a signal to lock the blades.

摘要翻译： 为螺旋桨组件提供了一种换桨装置，该螺旋桨组件具有围绕组件的轴线旋转的一排螺旋桨叶片。 该装置具有与螺旋桨组件同轴的一致环。 协调环可移动以驱动用于改变叶片间距的相应机构。 该装置还具有围绕协调环周向分布的多个俯仰锁定组件。 每个俯仰锁定组件具有自由状态，其允许协调环的移动和锁定状态，其阻止或限制协调环的移动，从而防止或限制叶片的俯仰变化。 当组件接收到锁定刀片的信号时，俯仰锁定组件从空闲状态移动到锁定状态。

公开(公告)号：US08573927B2

公开(公告)日：2013-11-05

申请号：US12954765

申请日：2010-11-26

申请人： Andrew Swift ,  Antony Morgan

发明人： Andrew Swift ,  Antony Morgan

IPC分类号： F01D7/00

CPC分类号： F01D7/00 ,  B64C11/308 ,  B64D2027/005 ,  F01D1/26 ,  F01D21/18 ,  F02C7/36 ,  F02C9/58 ,  F02K3/072 ,  F05D2220/324 ,  F05D2250/44 ,  Y02T50/66 ,  Y02T50/673

摘要： A back-up featherer for an engine arrangement having a main hydraulic actuator which angularly displaces propellers of a propeller assembly of the engine arrangement, and fluid supply lines for transferring hydraulic fluid between a hydraulic pressure power source located on a static structure of the engine arrangement and the main hydraulic actuator. The back-up featherer has a back-up actuator assembly for angular displacement of the propellers, the back-up actuator assembly rotating with the propeller assembly, a signal detector operatively connected to the back-up actuator assembly and rotates with the propeller assembly, and a back-up rotating coupling. A static side of the back-up rotating coupling is mounted to the static structure of the engine arrangement and communicates with a regulator located on a static structure of the engine arrangement. A rotating side of the back-up hydraulic rotating coupling rotates with the propeller assembly and communicates with the signal detector.

摘要翻译： 一种用于发动机装置的备用专利，其具有主要液压致动器，该主液压致动器成角度地置换发动机装置的螺旋桨组件的螺旋桨，以及用于在位于发动机装置的静态结构上的液压动力源之间传送液压流体的流体供应管线 和主液压执行机构。 后备专家具有用于螺旋桨角位移的后备执行机构组件，支承致动器组件与螺旋桨组件一起旋转，信号检测器可操作地连接到备用致动器组件并与螺旋桨组件一起旋转， 和备用旋转联轴器。 备用旋转联轴器的静态侧安装到发动机装置的静态结构，并与位于发动机装置的静态结构上的调节器连通。 后备液压旋转联轴器的旋转侧与螺旋桨组件一起旋转，并与信号检测器通信。

公开(公告)号：US20110142648A1

公开(公告)日：2011-06-16

申请号：US12945286

申请日：2010-11-12

申请人： Andrew SWIFT ,  Antony MORGAN

发明人： Andrew SWIFT ,  Antony MORGAN

IPC分类号： F01D7/00

CPC分类号： F02C6/206 ,  B64D2027/005 ,  F02C3/10 ,  F02K3/025 ,  F05D2260/40311 ,  F05D2260/74 ,  F05D2260/79 ,  Y02T50/66

摘要： An engine arrangement has a gear assembly that drives a first propeller assembly. The gear assembly is driven by a power drive shaft that joins to the gear assembly at a first side. The engine arrangement has a static conduit that extends along a longitudinal internal cavity of the power drive shaft. The conduit penetrates the gear assembly such that a portion of the conduit projects from an opposing second side of the gear assembly. The engine arrangement has one or more first fluid supply lines routed along the static conduit between a hydraulic pressure power source and the first hydraulic actuator. A first hydraulic rotating coupling is mounted to the projecting portion of the static conduit. The first fluid supply lines fluidly communicate with the first hydraulic actuator via the first rotating coupling.

摘要翻译： 发动机装置具有驱动第一螺旋桨组件的齿轮组件。 齿轮组件由在第一侧连接到齿轮组件的动力传动轴驱动。 发动机装置具有沿动力驱动轴的纵向内部空腔延伸的静态导管。 导管穿过齿轮组件，使得导管的一部分从齿轮组件的相对的第二侧突出。 发动机装置具有一个或多个在液压动力源和第一液压致动器之间沿着静态导管路线的第一流体供应管线。 第一液压旋转联轴器安装到静态导管的突出部分。 第一流体供应管线经由第一旋转联接器与第一液压致动器流体连通。

公开(公告)号：US20110274544A1

公开(公告)日：2011-11-10

申请号：US13086880

申请日：2011-04-14

申请人： Andrew SWIFT ,  Antony MORGAN

发明人： Andrew SWIFT ,  Antony MORGAN

IPC分类号： F01D7/00

CPC分类号： B64C11/385 ,  B64D2027/026 ,  Y02T50/66

摘要： A pitch control mechanism for controlling the pitch of propeller assembly propellers has a hydraulic actuator, main hydraulic fluid supply lines, first back-up hydraulic fluid supply lines, and second back-up hydraulic fluid supply lines. The hydraulic actuator has first and second hydraulic cylinders that each angularly displace the propellers between fine and coarse positions. The main hydraulic fluid supply lines supply fluid to the first and second hydraulic cylinders for operating the hydraulic cylinders. The first back-up hydraulic fluid supply lines supply fluid to the hydraulic cylinder for displacing the propellers to a coarser position. The second back-up hydraulic fluid supply lines supply fluid to the second hydraulic cylinder for displacing the propellers to a coarser position. When the main hydraulic fluid supply lines supply inadequate fluid, the first and/or second back-up hydraulic fluid supply lines can supply fluid for displacing the propellers to a coarser position.

摘要翻译： 用于控制螺旋桨组件螺旋桨的桨距的俯仰控制机构具有液压致动器，主液压流体供应管线，第一备用液压流体供应管线和第二后备液压流体供应管线。 液压致动器具有第一和第二液压缸，每个液压缸在精细和粗略位置之间均有角度地移动螺旋桨。 主液压流体供应管线向第一和第二液压缸供应流体以操作液压缸。 第一备用液压流体供应管路将液体供应到液压缸，以将螺旋桨移动到较粗的位置。 第二备用液压流体供应管线将流体供应到第二液压缸，用于将螺旋桨移动到较粗的位置。 当主液压流体供应管线供应不足的流体时，第一和/或第二备用液压流体供应管线可以供应用于将螺旋桨移动到较粗的位置的流体。

公开(公告)号：US08845291B2

公开(公告)日：2014-09-30

申请号：US12945286

申请日：2010-11-12

申请人： Andrew Swift ,  Antony Morgan

发明人： Andrew Swift ,  Antony Morgan

IPC分类号： B64C11/30 ,  F02C3/10 ,  F02C6/20 ,  F02K3/02

CPC分类号： F02C6/206 ,  B64D2027/005 ,  F02C3/10 ,  F02K3/025 ,  F05D2260/40311 ,  F05D2260/74 ,  F05D2260/79 ,  Y02T50/66

摘要： An engine arrangement has a gear assembly that drives a first propeller assembly. The gear assembly is driven by a power drive shaft that joins to the gear assembly at a first side. The engine arrangement has a static conduit that extends along a longitudinal internal cavity of the power drive shaft. The conduit penetrates the gear assembly such that a portion of the conduit projects from an opposing second side of the gear assembly. The engine arrangement has one or more first fluid supply lines routed along the static conduit between a hydraulic pressure power source and the first hydraulic actuator. A first hydraulic rotating coupling is mounted to the projecting portion of the static conduit. The first fluid supply lines fluidly communicate with the first hydraulic actuator via the first rotating coupling.

摘要翻译： 发动机装置具有驱动第一螺旋桨组件的齿轮组件。 齿轮组件由在第一侧连接到齿轮组件的动力传动轴驱动。 发动机装置具有沿动力驱动轴的纵向内部空腔延伸的静态导管。 导管穿过齿轮组件，使得导管的一部分从齿轮组件的相对的第二侧突出。 发动机装置具有一个或多个在液压动力源和第一液压致动器之间沿着静态导管布置的第一流体供应管线。 第一液压旋转联轴器安装到静态导管的突出部分。 第一流体供应管线经由第一旋转联接器与第一液压致动器流体连通。

公开(公告)号：US08757977B2

公开(公告)日：2014-06-24

申请号：US13086795

申请日：2011-04-14

申请人： Andrew Swift ,  Antony Morgan ,  Paul Simms

发明人： Andrew Swift ,  Antony Morgan ,  Paul Simms

IPC分类号： B64C11/42

CPC分类号： B64C11/385 ,  B64D2027/026 ,  Y02T50/66

摘要： A back-up featherer is provided for an engine arrangement having a main hydraulic actuator which operates a pitch change mechanism to angularly displace propellers of a propeller assembly of the engine arrangement, the pitch change mechanism and main hydraulic actuator rotating with the propeller assembly. The back-up featherer has one or more back-up hydraulic actuators located on a static structure of the engine arrangement. The back-up featherer further has one or more load application members which are located on the static structure of the engine arrangement and which are movable by the back-up hydraulic actuators. When moved by the back-up hydraulic actuators, the load application members bear against an engagement portion of the pitch change mechanism across a rotating interface formed therebetween to apply a load to the pitch change mechanism which results in angular displacement of the propellers.

摘要翻译： 为具有主液压致动器的发动机装置提供备用专利，该主液压致动器操作变桨机构以使发动机装置的螺旋桨组件的推进器成角度地移动，桨距变化机构和主液压致动器与螺旋桨组件一起旋转。 后备专家具有位于发动机装置的静态结构上的一个或多个备用液压致动器。 备用设备还具有一个或多个负载施加构件，其位于发动机装置的静态结构上并且可由后备液压致动器移动。 当由备用液压致动器移动时，负载施加构件通过形成在它们之间的旋转界面承受变桨机构的接合部分，以对螺距改变机构施加负载，这导致螺旋桨的角位移。

公开(公告)号：US08757975B2

公开(公告)日：2014-06-24

申请号：US13086880

申请日：2011-04-14

申请人： Andrew Swift ,  Antony Morgan

发明人： Andrew Swift ,  Antony Morgan

IPC分类号： B64C11/38

CPC分类号： B64C11/385 ,  B64D2027/026 ,  Y02T50/66

摘要： A pitch control mechanism for controlling the pitch of propeller assembly propellers has a hydraulic actuator, main hydraulic fluid supply lines, first back-up hydraulic fluid supply lines, and second back-up hydraulic fluid supply lines. The hydraulic actuator has first and second hydraulic cylinders that each angularly displace the propellers between fine and coarse positions. The main hydraulic fluid supply lines supply fluid to the first and second hydraulic cylinders for operating the hydraulic cylinders. The first back-up hydraulic fluid supply lines supply fluid to the hydraulic cylinder for displacing the propellers to a coarser position. The second back-up hydraulic fluid supply lines supply fluid to the second hydraulic cylinder for displacing the propellers to a coarser position. When the main hydraulic fluid supply lines supply inadequate fluid, the first and/or second back-up hydraulic fluid supply lines can supply fluid for displacing the propellers to a coarser position.

摘要翻译： 用于控制螺旋桨组件螺旋桨的桨距的俯仰控制机构具有液压致动器，主液压流体供应管线，第一备用液压流体供应管线和第二后备液压流体供应管线。 液压致动器具有第一和第二液压缸，每个液压缸在精细和粗略位置之间均有角度地移动螺旋桨。 主液压流体供应管线向第一和第二液压缸供应流体以操作液压缸。 第一备用液压流体供应管路将液体供应到液压缸，以将螺旋桨移动到较粗的位置。 第二备用液压流体供应管线将流体供应到第二液压缸，用于将螺旋桨移动到较粗的位置。 当主液压流体供应管线供应不足的流体时，第一和/或第二备用液压流体供应管线可以供应用于将螺旋桨移动到较粗的位置的流体。