利索-全球专利检索

  1. 登录
  2. 注册

搜索结果

41 条记录 (耗时 0.016 秒)

    ROTARY ACTUATOR
    32.
    发明公开
    ROTARY ACTUATOR 审中-公开

    公开(公告)号：EP3868653A1

    公开(公告)日：2021-08-25

    申请号：EP21158938.7

    申请日：2021-02-24

    申请人： The Boeing Company

    发明人： STANDLEY, John A. ,  LISENKO, Kim R. ,  ZAZYNSKI, Timothy Paul

    IPC分类号： B64C13/36 ,  F15B15/12 ,  B64C13/50

    摘要： A rotary actuator (32), including a manifold block (34) and a rotor assembly (36) that includes a rotor shaft (46) and a plurality of arcuate pistons (60) attached to the rotor shaft, each arcuate piston curving at a set radial distance from the rotor shaft, and each piston attached to the rotor shaft via a crank arm (58). A pressure chamber assembly (64) coupled to the manifold block defines a plurality of piston pressure chambers (66) that receive and at least partially enclose each arcuate piston, including a plurality of gland seals (72) disposed adjacent the entrance of each piston pressure chamber to create a seal between the inner surface (70) of the pressure chamber and the outer surface (68) of the arcuate piston. Each gland seal includes an inner seal (88) that engages the piston surface of the arcuate piston, and plural outer seals (901) that engage the inner surface of the piston pressure chamber, forming a hydraulic seal.

    APPARATUS AND METHOD FOR HIGH ENERGY DENSITY LINEAR ACTUATION WITH INTEGRAL BRAKING
    34.
    发明公开
    APPARATUS AND METHOD FOR HIGH ENERGY DENSITY LINEAR ACTUATION WITH INTEGRAL BRAKING 审中-公开
    具有整体制动的高能量密度线性驱动的装置和方法

    公开(公告)号：EP3311036A1

    公开(公告)日：2018-04-25

    申请号：EP16787950.1

    申请日：2016-04-14

    申请人： Raytheon Company

    发明人： STAGGERS, David D.

    IPC分类号： F15B15/10 ,  B64C13/36 ,  F42B10/64

    摘要： A pneumatic artificial muscle (PAM) actuator includes first and second end caps, an elastic bladder connected to the end caps, and a covering around the elastic bladder and connected to the end caps. At least one of the first and second end caps is configured to move and narrow a distance between the end caps in response to inflation of the elastic bladder by a fluid. At least one of the end caps includes a vent configured to allow the fluid to exit the elastic bladder and collapse the covering after activation of the PAM actuator. At least the covering is configured to provide braking for the PAM actuator. The covering may be configured to collapse at least partially between the first and second end caps to provide at least some of the braking for the PAM actuator.

    Aircraft control surface drive mechanism
    35.
    发明公开
    Aircraft control surface drive mechanism 审中-公开
    飞机控制面驱动机构

    公开(公告)号：EP2530012A3

    公开(公告)日：2017-07-12

    申请号：EP12166774.5

    申请日：2012-05-04

    申请人： Nabtesco Corporation

    发明人： Ito, Koji

    IPC分类号： B64C13/24 ,  B64C13/36 ,  F15B18/00

    CPC分类号： B64C13/36 ,  B64C13/24 ,  F15B15/04 ,  F15B15/1404

    摘要： An actuator includes a plurality of cylinder units (11) each including a cylinder and a rod (21), and is pivotably attached, at a first end thereof, to a control surface (102). A reaction link (12) is pivotably attached, at a first end thereof, to a fulcrum shaft (104) rotatably supporting the control surface. The reaction link (12) is pivotably attached, at a second end thereof, to a second end of the actuator between the plurality of cylinder units (11).

    摘要翻译： 致动器包括多个汽缸单元（11），每个汽缸单元包括汽缸和杆（21），并且在其第一端处可枢转地附接到控制表面（102）。 反作用连杆（12）在其第一端处可枢转地连接到可旋转地支撑控制表面的支轴（104）。 反作用连杆（12）在其第二端可枢转地连接到多个缸单元（11）之间的致动器的第二端。

    ENGINE DRIVEN PUMP (EDP) AUTOMATIC DEPRESSURIZATION SYSTEM
    37.
    发明公开
    ENGINE DRIVEN PUMP (EDP) AUTOMATIC DEPRESSURIZATION SYSTEM 审中-公开
    自动化设备DRUCKENTLASTUNGSSYSTEM MIT MOTORBETRIEBENER PUMPE（EDP）

    公开(公告)号：EP3025956A1

    公开(公告)日：2016-06-01

    申请号：EP15196298.2

    申请日：2015-11-25

    申请人： The Boeing Company

    发明人： WILSON, Thomas Michael ,  HASENOEHRL, Thomas Raymond ,  CHIN, Edmond C. ,  LESYNA, Mark William

    IPC分类号： B64C13/36 ,  F02C7/32

    CPC分类号： G05D16/2066 ,  B64C13/36 ,  B64C13/40 ,  B64C25/22 ,  B64D41/00 ,  F02C7/32

    摘要： An automatic engine driven pump (EDP) depressurization system for an aircraft is disclosed. The aircraft includes at least two EDPs (30a) driven by a main engine for converting mechanical power provided by the main engine into hydraulic power for distribution by a hydraulic system. The EDP depressurization system includes a depressurization device (70a) corresponding to each of the at least two EDPs (30a) and a control module (80). The depressurization devices (70a) are each energized to depressurize a respective EDP (30a). The control module (80) is in signal communication with each of the depressurization devices (70a). The control module (80) includes control logic for automatically generating a depressurization signal that energizes one of the depressurization devices based on a plurality of operational conditions of the aircraft.

    摘要翻译： 公开了一种用于飞行器的自动发动机驱动泵（EDP）减压系统。 飞机包括由主发动机驱动的至少两个EDP（30a），用于将由主发动机提供的机械动力转换成液压动力以通过液压系统分配。 EDP​​减压系统包括对应于至少两个EDP（30a）和控制模块（80）中的每一个的减压装置（70a）。 减压装置（70a）各自通电以对各个EDP（30a）进行减压。 控制模块（80）与每个减压装置（70a）进行信号通信。 控制模块（80）包括控制逻辑，用于根据飞行器的多个操作条件，自动产生对一个减压装置通电的减压信号。

    LINIENFÖRMIGER, HYDRAULISCHER SCHWENKANTRIEB
    39.
    发明公开
    LINIENFÖRMIGER, HYDRAULISCHER SCHWENKANTRIEB 有权
    线形，液压回转系统

    公开(公告)号：EP1488111A1

    公开(公告)日：2004-12-22

    申请号：EP03718601.2

    申请日：2003-02-21

    申请人： EADS Deutschland GmbH ,  Airbus Deutschland GmbH

    发明人： BREUER, Ulf ,  JÄNKER, Peter ,  LORKOWSKI, Thomas

    IPC分类号： F15B15/08 ,  B64C13/36

    CPC分类号： F15B15/068 ,  B64C13/40 ,  Y10T74/18056

    摘要： The invention relates to a linear, hydraulic pivot drive, especially for the flap control system of aerodynamic structures. Said pivot drive (1) comprises a housing (2) provided with ports (3, 4) for introducing a hydraulic medium, a piston (5) which is arranged inside the housing (2) and can be axially displaced by the effect of the hydraulic medium, and an output shaft (6) which is provided with coarse threads (8a, 8b) and interacts with the piston (5) in order to convert the axial displacement of the piston (5) into a rotational movement. The invention is characterised in that the output shaft (6) is integrated into the piston (5), the coarse threads (8a, 8b) running in the same direction and engaging in the piston (5), and the cross-section of the piston has a spline profile for effectively preventing a rotational movement of the piston (5).