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27 条记录 (耗时 0.045 秒)

    Non-glaring aesthetically pleasing lighting fixtures
    11.
    发明授权
    Non-glaring aesthetically pleasing lighting fixtures 失效
    不着色的美观照明灯具

    公开(公告)号：US06238065B1

    公开(公告)日：2001-05-29

    申请号：US09207743

    申请日：1998-12-08

    申请人： Peter J. Jones

    发明人： Peter J. Jones

    IPC分类号： F21V502

    CPC分类号： F21S11/00 ,  F21S8/02 ,  F21V5/02 ,  F21V5/04 ,  F21V5/08 ,  F21V7/0025 ,  F21V11/00 ,  F21V11/06 ,  F21V13/10 ,  G02B19/0028 ,  G02B19/0042 ,  G02B19/0047

    摘要： A lighting structure and method of forming a lighting structure including a light transmitting lens positioned in front of a light source, whereby the light transmitting lens has a substantially non-opaque front surface and a light receiving rear surface, and an array of substantially tubular elements positioned proximate to the substantially non-opaque front surface of the lens. The lighting structure may further include a reflective surface that projects light from the light source to the rear surface of the light transmitting lens and through the light transmitting lens. When the lighting structure is turned off, the array of substantially tubular elements is capable of making lighting structure appear to be a part of the surrounding surface in which the lighting structure is embedded. When the lighting structure is turned on, the array of substantially tubular elements masks the sight of the light source and shields a viewer's eyes from the glare of the reflector.

    摘要翻译： 一种形成包括位于光源前方的透光透镜的照明结构的照明结构和方法，由此所述透光透镜具有基本上不透明的前表面和光接收后表面，以及基本上管状的元件阵列 定位在透镜的基本上不透明的前表面附近。 照明结构还可以包括将来自光源的光投射到透光透镜的后表面并通过透光透镜的反射表面。 当照明结构被关闭时，基本上管状元件的阵列能够使得照明结构看起来是照明结构被嵌入其中的周围表面的一部分。 当照明结构被打开时，基本管状元件的阵列掩盖光源的视线并且遮蔽观察者的眼睛避免反射器的眩光。

    Active fluid mounting
    12.
    发明授权
    Active fluid mounting 失效
    主动流体安装

    公开(公告)号：US5957440A

    公开(公告)日：1999-09-28

    申请号：US835433

    申请日：1997-04-08

    申请人： Peter J. Jones ,  Douglas E. Ivers ,  Kevin C. Cooney ,  Gerald P. Whiteford

    发明人： Peter J. Jones ,  Douglas E. Ivers ,  Kevin C. Cooney ,  Gerald P. Whiteford

    IPC分类号： F16F7/10 ,  F16F13/06 ,  F16F13/22 ,  F16F13/26 ,  F16F5/00

    CPC分类号： F16F13/22 ,  F16F13/06 ,  F16F13/26 ,  F16F7/1005 ,  F16F2228/00

    摘要： An active fluid mounting for isolating vibration between a vibrating member (21) and a structure (23). In one aspect, the active fluid mounting (20) includes an inner member (22), an outer member (24), a first flexible element (26), and an cartridge-like active fluid element (28) which is unitary and readily detachable, attached between the inner and outer members, (22) and (24). The cartridge-like active fluid element (28) preferably includes a first housing member (30) for attachment to inner member (22), a second housing member (32) for attachment to outer member (24), a second flexible element (34) for flexibly interconnecting first housing member (30) to second housing member (32), at least one fluid chamber (36) having a volume stiffness, a fluid (40) contained within, a moveable piston (42) interacting with fluid (40) in the fluid chamber (36) to cause pressure variations and produce dynamic forces which act between the inner and outer member, (22) and (24), and a preferable coil-and-magnet assembly (44) for driving piston (42) housed internally within active fluid element (28). In another aspect, a piston (42a) which is inductively driven is described. In yet another, an interchangeable motor unit including a magnet (68), coil (70), and pole pieces (66) is received within the inner member (22).

    摘要翻译： 一种用于隔离振动构件（21）和结构（23）之间的振动的主动流体安装件。 在一个方面，主动流体安装件（20）包括内部构件（22），外部构件（24），第一柔性元件（26）和总成并且容易地形成的筒状活性流体元件（28） 可拆卸地安装在内部和外部构件（22）和（24）之间。 盒状有源流体元件（28）优选地包括用于附接到内部构件（22）的第一壳体构件（30），用于附接到外部构件（24）的第二壳体构件（32），第二柔性元件（34） ，用于将第一壳体构件（30）柔性地互连到第二壳体构件（32），具有体积刚度的至少一个流体室（36），容纳在与流体（40）相互作用的可移动活塞（42）内的流体 ）导致流体室（36）中的压力变化并产生作用在内部和外部构件（22）和（24）之间的动力，以及用于驱动活塞（42）的优选的线圈和磁体组件（44） ）容纳在主动流体元件（28）内部。 另一方面，描述了感应驱动的活塞（42a）。 在另一方面，包括磁体（68），线圈（70）和极片（66）的可互换电动机单元被容纳在内部构件（22）内。

    Method and apparatus for reducing transient motion between an aircraft power member and structure during takeoff, landing and maneuvers
    13.
    发明授权
    Method and apparatus for reducing transient motion between an aircraft power member and structure during takeoff, landing and maneuvers 失效
    用于在起飞，着陆和演习期间减少飞机动力构件和结构之间的瞬时运动的方法和装置

    公开(公告)号：US5788372A

    公开(公告)日：1998-08-04

    申请号：US644147

    申请日：1996-05-10

    申请人： Peter J. Jones ,  Dennis P. McGuire

    发明人： Peter J. Jones ,  Dennis P. McGuire

    IPC分类号： B64D27/26 ,  F16F9/508 ,  F16F9/512 ,  F16F13/06 ,  F16M1/00 ,  F16F7/10 ,  F16K15/00

    CPC分类号： B64D27/26 ,  F16F13/06 ,  F16F9/5126 ,  Y10T137/7847 ,  Y10T137/7869

    摘要： A method and apparatus is described for limiting transient motions between an aircraft power member and aircraft structure. The apparatus incorporates a coupler (20) for use with inertial-type mounts and includes a body portion (21) having a coupler piston (32) telescopically received therein. Upon exceeding a transient relative motion which causes a fluid flow velocity to be exceeded, seat (38) formed on coupler piston (32) interacts with lip (39) on body portion (21) to cause a fluid flow restriction. This method and apparatus restricts and limits transient motions, i.e., acts as a snuffer, to limit further relative motion between an aircraft power member (54) and an aircraft structural member (52). The coupler piston (32) preferably includes a flexible seal (38) formed thereon and orifice (40) therethrough for providing additional throttle-type damping upon snubbing. This method and apparatus is particularly useful in inertial-type fluid mounts for mounting aircraft engines, fluid pylon isolators for helicopter pylon isolation, and Fluid Torque Restraint (FTR) systems for aircraft for limiting transient motions under certain conditions, such as during takeoff, landing, and maneuvers, yet providing isolation under normal operating conditions.

    摘要翻译： 描述了用于限制飞机功率构件和飞行器结构之间的瞬时运动的方法和装置。 该装置包括用于惯性型座架的联接器（20），并且包括具有可伸缩地容纳在其中的联接器活塞（32）的主体部分（21）。 当超过导致流体流速超过的瞬时相对运动时，形成在联接器活塞（32）上的座（38）与主体部分（21）上的唇部（39）相互作用以引起流体流动限制。 该方法和装置限制和限制瞬态运动，即用作缓冲器，以限制飞机动力构件（54）和飞机结构构件（52）之间的进一步的相对运动。 联接器活塞（32）优选地包括形成在其上的柔性密封件（38）和穿过其中的孔口（40），用于在缓冲时提供额外的节流型阻尼。 这种方法和装置在用于安装飞机发动机，用于直升机塔架隔离的流体塔架隔离器和用于飞机的流体扭矩限制（FTR）系统）的惯性式流体支架中特别有用，以限制在特定条件下的瞬变运动，例如在起飞，着陆期间 和机动，但在正常运行条件下提供隔离。

    Flexible composite coupling
    14.
    发明授权
    Flexible composite coupling 失效
    柔性复合耦合

    公开(公告)号：US5551918A

    公开(公告)日：1996-09-03

    申请号：US843671

    申请日：1992-02-28

    申请人： Peter J. Jones ,  Peter L. Valentine ,  Duncan J. Lawrie

    发明人： Peter J. Jones ,  Peter L. Valentine ,  Duncan J. Lawrie

    IPC分类号： F16D3/72 ,  F16D3/50

    CPC分类号： F16D3/725

    摘要： A flexible composite coupling (20) wherein a wound filament or roving is wound between two attachment members (22) and (24) and is fully or partially impregnated with a resin matrix such as urethane to form a flexible element (32). The attachment members (22) and (24) include radially extending flanges (26) and (28) which have a radiused periphery (30) formed on them, over which the flexible element (32) is wound. The flexible element (32) diverges inwardly from the flanges' (26) and (28) radiused periphery (30) to form opposed diaphragm portions (34) and (35) of the flexible element (32) which smoothly meet at a minimum diameter (36). Hoop winds (38) of a material with high strain capacity wrapped about this minimum diameter (36) pretension the filaments or roving within the flexible element (32).

    摘要翻译： 一种柔性复合联接器（20），其中缠绕的细丝或粗纱缠绕在两个附接构件（22）和（24）之间，并且完全或部分地浸渍有诸如聚氨酯的树脂基质以形成柔性元件（32）。 附接构件（22）和（24）包括径向延伸的凸缘（26）和（28），其上形成有形成在其上的圆角的周边（30），柔性元件（32）被缠绕在凸缘上。 柔性元件（32）从凸缘（26）和（28）向外扩散到圆周（30），以形成柔性元件（32）的相对的隔膜部分（34）和（35） （36）。 围绕该最小直径（36）缠绕的具有高应变能力的材料的缠绕风（38）预先将柔性元件（32）内的长丝或粗纱预紧。

    Rotary wing aircraft rotary lead lag damper
    17.
    发明授权
    Rotary wing aircraft rotary lead lag damper 有权
    旋翼飞机旋转牵引阻尼器

    公开(公告)号：US08356977B2

    公开(公告)日：2013-01-22

    申请号：US11754673

    申请日：2007-05-29

    申请人： Peter J. Jones ,  Zachary Fuhrer

    发明人： Peter J. Jones ,  Zachary Fuhrer

    IPC分类号： B64C27/51 ,  F16F9/14

    CPC分类号： B64C27/51 ,  F16F9/145

    摘要： The rotary damper for controlling helicopter motions includes an outer canister with an inner paddle wheel receiving cavity which receives an inner paddle wheel with upper and lower elastomeric tubular intermediate members between the inner paddle wheel and the outer canister. The canister and inner paddle wheel form neighboring variable volume chambers in liquid communication through liquid damping conduits. A clockwise rotation of the inner paddle wheel about the center of rotation axis relative to the outer canister pumps damper liquid from a second variable volume chamber through a first liquid conduit towards a first variable volume chamber, and a counterclockwise rotation of the paddle wheel relative to the outer canister pumps the damper liquid from the first variable volume chamber through the first liquid conduit towards the second variable volume chamber with the elastomeric tubular intermediate members providing for the relative rotation and containing the damper liquid in the damper.

    摘要翻译： 用于控制直升机运动的旋转阻尼器包括具有内桨轮容纳腔的外筒，其接纳内桨轮，其具有在内桨轮和外筒之间的上弹性体管管中间构件和下弹性体管状中间构件。 罐和内桨轮通过液体阻尼管道形成液体连通的相邻可变容积室。 内侧叶轮围绕旋转轴线的中心相对于外部罐泵顺时针旋转，将来自第二可变容积室的液体通过第一液体导管朝向第一可变容积室进行阻尼，并且相对于桨叶的逆时针旋转 外罐将来自第一可变体积室的阻尼液从第一液体导管朝向第二可变容积室泵送，弹性体管状中间构件提供相对旋转并将阻尼液体容纳在阻尼器中。

    Fluid damper including flexible damping plate
    19.
    发明授权
    Fluid damper including flexible damping plate 失效
    流体阻尼器包括柔性阻尼板

    公开(公告)号：US6045328A

    公开(公告)日：2000-04-04

    申请号：US159293

    申请日：1998-09-23

    申请人： Peter J. Jones

    发明人： Peter J. Jones

    IPC分类号： B64C27/35 ,  B63H5/10 ,  F16F13/08 ,  F16F13/10 ,  F16F15/023 ,  F16F15/08

    CPC分类号： F16F13/105 ,  B64C27/51

    摘要： A fluid and elastomer damper includes a first and second members and an elastomer section flexibly mounting the second member to the first member and allowing lateral movement therebetween. The elastomer section includes an inner wall forming a portion of a cavity defined within the damper and a damping fluid disposed within the cavity. A flexible damping plate separates the cavity into first and second chambers. At least one passageway is formed between the damping plate and the inner wall, the passageway exhibiting a gap dimension between the wall and the damping plate. When lateral movement occurs between the first and second members, the gap dimension is maintained substantially constant by flexing of the damping plate along the lateral direction.

    摘要翻译： 流体和弹性体阻尼器包括第一和第二构件以及将第二构件柔性地安装到第一构件并允许它们之间横向移动的弹性体部分。 弹性体部分包括形成限定在阻尼器内的空腔的一部分的内壁和设置在空腔内的阻尼流体。 柔性阻尼板将空腔分成第一和第二腔室。 在阻尼板和内壁之间形成至少一个通道，通道在壁和阻尼板之间呈现间隙尺寸。 当在第一和第二构件之间发生横向移动时，通过阻尼板沿着横向方向弯曲，间隙尺寸保持基本上恒定。

    Volume compensated fluid mount
    20.
    发明授权
    Volume compensated fluid mount 失效
    体积补偿液体安装

    公开(公告)号：US4811919A

    公开(公告)日：1989-03-14

    申请号：US83435

    申请日：1987-08-06

    申请人： Peter J. Jones

    发明人： Peter J. Jones

    IPC分类号： F16F13/00 ,  B64D27/18 ,  B64D27/26 ,  F01D25/28 ,  F02C7/20 ,  F16F13/04 ,  F16F13/08 ,  F16F13/26

    CPC分类号： F02C7/20 ,  B64D27/18 ,  B64D27/26 ,  F01D25/28 ,  F16F13/08 ,  B64D2027/264 ,  Y02T50/671

    摘要： A fluid mount particularly suited for mounting an engine in an aircraft. The mount includes a frame which is fastened to the engine and a support movably mounted in the frame and adapted to receive a wing pylon stub shaft. Opposed liquid-filled chambers are provided on opposite sides of the stub shaft support and are fluidly interconnected by an elongate tube. An auxiliary chamber is provided on the frame adjacent to the upper liquid chamber and is divided internally into a gas-filled portion and a liquid-filled portion which is in communication with the upper liquid chamber via an orifice. The auxiliary chamber accommodates changes in liquid volume without adversely affecting either the static or dynamic performance of the mount.