SUBSURFACE SAFETY VALVE ACTUATOR
    2.
    发明公开

    公开(公告)号:US20240018846A1

    公开(公告)日:2024-01-18

    申请号:US18036643

    申请日:2021-11-11

    申请人: Moog Inc.

    IPC分类号: E21B34/06

    CPC分类号: E21B34/066 E21B2200/05

    摘要: A subsurface safety valve actuation system in well tubing comprising a safety valve, piston assembly, motor, pump, spring, reservoir, first valve, and second valve configured to provide pressure in a chamber of the piston assembly that drives the safety valve to an open position, retain pressure in the chamber that retains the safety valve in the open position, release pressure in the chamber via a first hydraulic release path and/or a second hydraulic release path between the chamber and the reservoir that extends through the first valve and second valve, respectively, and the first and second hydraulic release paths being independent from each other, whereby pressure in the chamber that retains the safety valve in the open position may be released via the first or second hydraulic release path when there is a fault in the other of the first or second release path.

    Teleoperation system, method, apparatus, and computer-readable medium

    公开(公告)号:US11559898B2

    公开(公告)日:2023-01-24

    申请号:US16652862

    申请日:2018-10-05

    申请人: Moog Inc.

    摘要: Embodiments of the present disclosure provide a system, method, apparatus and computer-readable medium for teleoperation. An exemplary system includes a robot machine having a machine body, at least one sensor, at least one robot processor, and at least one user processor operable to maintain a user simulation model of the robot machine and the environment surrounding the robot machine, the at least one user processor being remote from the robot machine. The system further includes at least one user interface comprising a haptic user interface operable to receive user commands and to transmit the user commands to the user simulation model, a display operable to display a virtual representation of the user simulation model.

    PRELOADED TORQUE SHAFT AND THE FLIGHT CONTROL DRIVELINE MADE THEREWITH

    公开(公告)号:US20220242555A1

    公开(公告)日:2022-08-04

    申请号:US17612622

    申请日:2020-05-22

    申请人: Moog Inc.

    IPC分类号: B64C13/32 F16C3/02 B29D99/00

    摘要: Presented are a method and apparatus for an aircraft flight surface actuation system including a motor having an output shaft. A gearbox is coupled with the output shaft, whereby a first driving force output via the motor is converted to a second driving force. A torque shaft assembly is driveably coupled with the gearbox. The torque shaft assembly includes a first tube, a second tube located at least partially through the first tube and located coaxial therewith, wherein the first tube comprises an axial preload operable to mitigate lateral deflection, and wherein the first tube comprises a torsional preload operable to mitigate torsional deflection. In addition, the aircraft flight surface actuation system includes an eccentric cam mechanism driveably coupled with the torque shaft assembly, and a flight surface coupled with the eccentric cam mechanism.

    Secure and traceable manufactured parts

    公开(公告)号:US11107168B2

    公开(公告)日:2021-08-31

    申请号:US15600576

    申请日:2017-05-19

    申请人: Moog Inc.

    摘要: A method for the verification and authentication of additive manufactured product, comprising the steps of receiving, from a customer, at least one customer requirement for a product, deriving at least one manufacturing requirement and generating a product geometry file for the product, recording, by a first computing device, to a distributed transaction register, a first transaction reflecting certification of the product geometry file, obtaining a first output reflecting the first transaction, printing the product with a 3D printer, recording, by a second computing device, to the distributed transaction register, a second transaction reflecting the printing of the product and the first output, obtaining a second output reflecting the second transaction, embedding within the product a unique code reflecting the second output, whereby the product geometry file and the printing of said product may be verified with the unique code such that the product may be authenticated.

    Metal ribbon stator and motor comprising same

    公开(公告)号:US11081913B2

    公开(公告)日:2021-08-03

    申请号:US16392208

    申请日:2019-04-23

    申请人: Moog Inc.

    发明人: David Calley

    摘要: A stator made from a ribbon of metal having multiple layers of slit metal, and motors made therefrom are described. A ribbon having multiple layers of metal is formed into a stator such as by flattening or pleating the ribbon to form each pole of a stator having a plurality of stator teeth, or poles. The stator formed from the metal ribbon may be configured into any suitable type of motor, such as an axial transverse flu motor. A magnetic flu return may also be made out of metal ribbon.

    Three-dimensional monolithic diaphragm tank

    公开(公告)号:US11067037B2

    公开(公告)日:2021-07-20

    申请号:US16513410

    申请日:2019-07-16

    申请人: Moog Inc.

    摘要: A three-dimensional monolithic diaphragm tank including a first portion having a first inner surface, a second portion having a second inner surface, and a deformable diaphragm extending from a peripheral junction with the first inner surface and the second inner surface. The first inner surface and the diaphragm defining a first chamber. The second inner surface and the diaphragm defining a second chamber. The first portion having an outlet port in fluid communication with the first chamber, and the second portion having an inlet port in fluid communication with the second chamber. The peripheral junction of the diaphragm and the first inner surface including an integral inner fillet having an inner radius.

    Hub mounted vibration suppression system

    公开(公告)号:US10308355B2

    公开(公告)日:2019-06-04

    申请号:US15212978

    申请日:2016-07-18

    申请人: Moog Inc.

    发明人: Arturo M. Arce

    IPC分类号: B64C11/02 B64C27/00

    摘要: An improved vibration control actuation system for a rotary-wing aircraft having a plurality of rotor blades mounted to a rotor hub and driven about a central axis of rotation at an operational speed and in a rotational direction relative to a non-rotating body of the aircraft comprising a vibration control frame adapted to be mounted to the hub and to rotate relative to the hub about the central axis in a rotational direction opposite to the rotational direction of the hub, a frame motor configured to rotate the frame about the central axis, the frame supporting first and second motors configured to rotate first and second masses about first and second axes not concentric with the central axis, and a controller for receiving input signals and outputting command signals to the first and second motors.

    Multiple actuator and linkage system

    公开(公告)号:US10281033B2

    公开(公告)日:2019-05-07

    申请号:US14376000

    申请日:2012-02-09

    申请人: John Kopp

    发明人: John Kopp

    摘要: An actuator system comprising a shared link (121) arranged to pivot about a first axis (131) relative to a reference structure, a controlled element (125) arranged to pivot about a second axis (126) relative to the reference structure, a first member (146, 152) arranged to pivot about a third axis (134) relative to the shard link and a fourth axis (136) relative to the controlled member, a first actuator arranged to control a first variable distance (LI) between the third axis and fourth axis, a second member (147, 153) arranged to pivot about a fifth axis (133) relative to the shared link and a sixth axis (135) relative to the controlled element, a second actuator (141) arranged to control a second variable distance between the fifth axis and the sixth axis, the system configured such that a change in the first variable distance causes rotation of the controlled element about the second axis when the second variable distance is constant and vice versa.