ROTATING SHAFT ELECTRICAL CONNECTION
    181.
    发明申请
    ROTATING SHAFT ELECTRICAL CONNECTION 审中-公开
    旋转轴电气连接

    公开(公告)号:WO1987007086A1

    公开(公告)日:1987-11-19

    申请号:PCT/US1987001105

    申请日:1987-05-11

    CPC classification number: H01R4/30 H01R39/643

    Abstract: To provide for electrical connection of electrical components (14), (16) through a rotating shaft (12) in a manner facilitating assembly and disassembly of the connection for replacement of the components (14), (16), a connector assembly (20) is provided. The connector assembly (20) includes an inset (24) disposed within an insulator (22) both of which are fixed within the rotating shaft (12) in proximity to an opening (18) therein, electrical terminals or contacts (26), (28) associated with each of the electrical components (14), (16) in spaced relation thereto, and a conductive bushing (30) extending through the opening (18) in the rotating shaft (12) in electrically isolated relation thereto. Additionally, the connector assembly (20) includes an externally threaded fastener (32) for releaseably securing the electrical terminals or contacts (26), (28) and the conductive bushing (30) to the insert (24) in the insulator (22) to electrically interconnect the electrical components (14), (16) in a manner accessible externally of the rotating shaft (12).

    HYDROSTATIC TRANSMISSION WITH MECHANICAL LIMIT STOP
    182.
    发明申请
    HYDROSTATIC TRANSMISSION WITH MECHANICAL LIMIT STOP 审中-公开
    具有机械限位停止功能的液压传动

    公开(公告)号:WO1987003944A1

    公开(公告)日:1987-07-02

    申请号:PCT/US1986002659

    申请日:1986-12-10

    CPC classification number: F16H61/439 F16H61/4192 F16H61/46 F16H61/47

    Abstract: The hydrostatic transmission (6) has a mechanical limit stop (92) located entirely within hydraulic manifold (90). The limit stop (92) includes a shaft (104) which rotates in direct relation to a motor output shaft (44) of the hydrostatic transmission (6) and causes movement of a sleeve (112) having stops (114, 116) engageable with the wobbler (38) of a variable displacement pump (10) of the hydrostatic transmission to assure return of the wobbler to a neutral or zero position when the driven member (80) has reached a desired limit position and the electro-hydraulic servo valve (50) fails to operate to return the wobbler (38) to neutral position.

    Abstract translation: 静液压变速器(6)具有完全位于液压歧管(90)内的机械限位挡块(92)。 限位挡块(92)包括一个与静液压传动装置(6)的电动机输出轴(44)直接相关的轴(104),并使得具有止动件(114,116)的套筒(112)可以与 静液传动装置的可变排量泵(10)的摇摆器(38),以在驱动构件(80)达到期望极限位置时确保摆动器返回中立或零位置,并且电动液压伺服阀( 50)无法操作以将摆轮(38)返回到中立位置。

    POWER CONVERTER FOR AN ELECTRICALLY-COMPENSATED CONSTANT SPEED DRIVE
    183.
    发明申请
    POWER CONVERTER FOR AN ELECTRICALLY-COMPENSATED CONSTANT SPEED DRIVE 审中-公开
    电动转换器用于电力补偿恒速驱动

    公开(公告)号:WO1987003928A1

    公开(公告)日:1987-07-02

    申请号:PCT/US1986002656

    申请日:1986-12-10

    CPC classification number: F02C7/32 H02M5/272 H02P29/0016

    Abstract: Electrically-compensated constant speed drive, CSD, (10) which includes a speed summer (18) having first and second input shafts (20, 36) and one output shaft (22). The first input shaft (20) is coupled to a variable speed prime mover (16) and the output shaft (22) develops a constant speed motive power. A speed-compensating permanent magnet machine (PMM2) couples to the second input shaft (36) of the speed summer (18). A control permanent magnet machine (PMM1) couples to the first input shaft (20) of the speed summer (18). A power converter (30) interconnects the power windings (70, 72) of these two permanent magnet machines (PMM1, PMM2). The power converter (30) comprises first and second bi-directional AC/DC converters (54, 56), a bi-directional DC/DC converter (58), and a circuit (44) for controlling the converters (54, 56, 58) so as to maintain the output shaft (22) of the speed summer (18) at a constant, desired speed.

    Abstract translation: 电动补偿恒速驱动器CSD(10)包括具有第一和第二输入轴(20,36)和一个输出轴(22)的减速器(18)。 第一输入轴(20)联接到可变速原动机(16),输出轴(22)产生恒定速度的动力。 速度补偿永磁机(PMM2)耦合到速度夏季(18)的第二输入轴(36)。 控制永磁机(PMM1)耦合到速度夏季(18)的第一输入轴(20)。 功率转换器(30)将这两个永久磁铁机(PMM1,PMM2)的功率绕组(70,72)互连。 功率转换器(30)包括第一和第二双向AC / DC转换器(54,56),双向DC / DC转换器(58)和用于控制转换器(54,56)的电路(44) 以便将速度夏季(18)的输出轴(22)保持在恒定的期望速度。

    SELF-POWERED ROTARY ACTUATOR UTILIZING ROTATION GENERATED CENTRIFUGAL HEAD
    184.
    发明申请
    SELF-POWERED ROTARY ACTUATOR UTILIZING ROTATION GENERATED CENTRIFUGAL HEAD 审中-公开
    自动旋转执行器利用旋转生成离心头

    公开(公告)号:WO1987003927A1

    公开(公告)日:1987-07-02

    申请号:PCT/US1986002767

    申请日:1986-12-19

    CPC classification number: F15B15/12

    Abstract: Conventional rotary-vane hydraulic actuators require external pressure sources. The hydraulic actuator (35) disclosed utilizes the centrifugal head developed in its pressure chambers (52, 54) when the entire actuator (35) rotates as a source of pressure. As actuator (35) rotates fluid exits outlet port (56) and passes through a servovalve (64) into chamber (54) to move vane (49) relative to the actuator (35). To move vane (49) in the other direction, fluid exits outlet port (58) and passes through the valve into chamber (52). This self-powered actuator has utility in systems requiring relative angular positioning between a pair of rotating elements such as a pair of voltage regulator rotors in a dual permanent magnet generator.

    Abstract translation: 传统的旋转叶片液压致动器需要外部压力源。 所公开的液压致动器(35)在整个致动器(35)作为压力源旋转时利用在其压力室(52,54)中形成的离心头。 当致动器(35)使流体离开出口(56)旋转并通过伺服阀(64)进入腔室(54)以相对于致动器(35)移动叶片(49)。 为了沿另一方向移动叶片(49),流体离开出口(58)并通过阀进入腔室(52)。 这种自动动力执行器在需要在一对旋转元件(例如双重永磁发电机中的一对电压调节器转子)之间的相对角度定位的系统中具有实用性。

    ELECTRIC GENERATOR COOLING ARRANGEMENT
    185.
    发明申请
    ELECTRIC GENERATOR COOLING ARRANGEMENT 审中-公开
    电力发电机冷却装置

    公开(公告)号:WO1987003431A1

    公开(公告)日:1987-06-04

    申请号:PCT/US1986001610

    申请日:1986-08-04

    CPC classification number: H02K11/042 H02K9/19

    Abstract: For cooling a known electric generator a floating oil transfer tube was utilized, which was unsuitable for cooling a rectifier assembly within the generator. This problem is solved by a cooling arrangement (10) for the electric generator (12) capable of supplying oil to a cyclindrical rotor cavity (18) to maintain a predetermined flow rate therethrough while providing spray oil cooling to the rotating rectifier assembly (26), the stationary non-rotating oil transfer tube (20) extends from one end (14a) of a generator housing (14) within a rotating shaft (16) in generally coaxial relation with the one end (20a) of the tube (20) being in communication with an oil inlet (22) through the housing (14) and the other end (20b) of the tube (20) mounted within a rotating fitting (24) in the rotating shaft (16), the oil transfer tube (20) has a radially extending orifice for spraying oil passing through the tube into the path of travel of the rectifier assembly (26) upstream of the rotating fitting (24) and the rotating fitting (24) has an opening (36) for carrying the remainder of the oil passing through the oil transfer tube (20) into the cylindrical rotor cavity (18) within the rotating shaft (16) downstream of the rectifier assembly (26).

    Abstract translation: 为了冷却已知的发电机,使用浮动油输送管,其不适于冷却发电机内的整流器组件。 该问题通过一种用于发电机(12)的冷却装置(10)来解决,该冷却装置能够向循环转子腔(18)供应油,以保持预定流量通过其中,同时向旋转整流器组件(26)提供喷射油冷却, 固定的非旋转输油管20从发生器壳体14的一端(14a)延伸到旋转轴(16)内,与管(20)的一端(20a)大致同轴, 与安装在旋转轴(16)中的旋转配件(24)内的通过壳体(14)和管(20)的另一端(20b)连通的进油口(22),输油管 20)具有径向延伸的孔,用于将通过管的油喷射到旋转配件(24)上游的整流器组件(26)的行进路径中,并且旋转配件(24)具有用于承载 剩余的油通过输油管(20)进入圆柱形 在整流器组件(26)下游的旋转轴(16)内的转子腔(18)。

    THERMAL DISCONNECT COUPLING
    186.
    发明申请
    THERMAL DISCONNECT COUPLING 审中-公开
    热断开连接

    公开(公告)号:WO1987003057A1

    公开(公告)日:1987-05-21

    申请号:PCT/US1986002369

    申请日:1986-11-03

    CPC classification number: F16D9/02 F16D11/14

    Abstract: Dispersion of eutectic material (56) in a thermal disconnect coupling following thermal actuation is avoided by disposing the body (56) of eutectic material in a first axially opening cavity (40) in a driven shaft (24) having teeth (32) normally meshed with teeth (22) on a driving shaft (16). The first cavity (40) is closed by a wall (50) forming part of an output shaft (26) and the interface of the cavity (40) and the wall (50) is provided with seals (92, 94). The first cavity (40) is separated from a second cavity (42) in the driven shaft (24) by a perforated web (44, 46) and together with an element (60) supported by the output shaft (26) defines second chamber into which the body (56) may flow upon thermal actuation. The interface of the element (60) and the second cavity (42) is provided with seals (92, 94) to prevent the escape of eutectic material from the second chamber.

    PERMANENT MAGNET ROTOR ASSEMBLY WITH FIBROUS WRAP
    187.
    发明申请
    PERMANENT MAGNET ROTOR ASSEMBLY WITH FIBROUS WRAP 审中-公开
    永磁电机转子总成与FIBROUS WRAP

    公开(公告)号:WO1987002524A1

    公开(公告)日:1987-04-23

    申请号:PCT/US1986001744

    申请日:1986-08-25

    CPC classification number: H02K1/278 H02K15/03

    Abstract: Loose or frayed fibers at the axial end of a fibrous wrap (42) about the periphery of rotor hub (10) mounting permanent magnets (22) are avoided by placing steps (40) between first and second diametral sections (36, 38) in side plates (32, 34) that sandwich the magnets (22), the wrap preventing radial displacement of the magnets, and the side plates preventing axial displacement.

    INVERTER CONTROL
    189.
    发明申请
    INVERTER CONTROL 审中-公开
    逆变器控制

    公开(公告)号:WO1986004192A1

    公开(公告)日:1986-07-17

    申请号:PCT/US1985002549

    申请日:1985-12-19

    CPC classification number: H02M7/53873

    Abstract: Prior inverter controls have been developed which are capable of controlling switches in an inverter to produce one of a plurality of polyphase output waveforms. Such controls utilize one or more memories to store a plurality of modulation patterns for controlling the switches. However, such types of inverter controls cannot provide individual phase regulation with the required degree of noise immunity. In order to overcome this problem, an inverter control (27) according to the present invention includes a plurality of memories (60, 62, 64) one for each phase, each of which is subdivided into a plurality of memory blocks which store a number of bytes, each of which is eight bits in length. Each bit is a zero or one, with a zero representing a first output condition for the respective phase, such as a notch, and a one representing a second output condition, such as a pulse. Memory address decoding logic (72, 100, 102) includes means for accessing a particular memory block in each memory in accordance with a control signal representing the desired waveform to be generated at each phase output. Also included are means (78) for sequentially addressing the bytes within a memory block so that the bytes stored within the block are sequentially provided at an output of the memory. A multiplexer/latch (76, 115, 117) latches a particular bit of each byte so that a control waveform is developed at the output of the latch. The control waveform is utilized to derive operating signals for switches in the respective inverter phase so that the desired waveform is generated. The inverter control of the present invention accomplishes individual phase regulation of the inverter output and is relatively immune to noise which can cause distortion in the output power.

    DEPLOYMENT MECHANISM FOR A RAM AIR TURBINE
    190.
    发明申请
    DEPLOYMENT MECHANISM FOR A RAM AIR TURBINE 审中-公开
    RAM空气涡轮机的部署机制

    公开(公告)号:WO1986003725A1

    公开(公告)日:1986-07-03

    申请号:PCT/US1985002551

    申请日:1985-12-19

    CPC classification number: B64D41/007

    Abstract: Deployment mechanism for a ram air turbine has conventionally consisted of a strut pivotally mounted within a storage bay of an aircraft and which pivots to a downwardly-extending position to bring the ram air turbine into deployed position. Such a structure has required a storage bay in the aircraft having a large stowing volume because of the primarily rotational movement of the ram air turbine and has not maximized the speed of deployment of the ram air turbine. The improved deployment mechanism for the ram air turbine (10) has front and rear linkages (40, 42) pivotally connected at one of their ends within the storage bay (24) of the aircraft and their other ends pivotally connected to the ram air turbine and includes a spring-loaded deployment actuator (44) operable to move the ram air turbine from stowed position. The front and rear linkages (40, 42) are constructed and mounted at pivot joints to provide primarily a linear motion of the ram air turbine (10) in moving between stowed and deployed positions to provide for fast deployment and also minimize the volume of the storage bay and the area of the access doors thereto.

Patent Agency Ranking