Synonyme wurden verwendet für: Actuators
Suche ohne Synonyme: title: Aerospace Actuators 1

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    Aerospace Hydraulics and Actuation Lessons Learned

    SAE Technical Papers | 2017
    This SAE Aerospace Information Report (AIR) contains Lessons Learned from aerospace actuation, control and fluid power systems technologies ...
    Schlagwörter: Flight control actuators

    Control electronics, electromechanical actuator, aircraft and method for damping the movement of an electromechanical actuator

    Freier Zugriff
    FRANK KRONBURGER / JULIAN KINZELMANN | Europäisches Patentamt | 2023
    deactivate or deactivates DC/DC converter 1 supplying electrical power to the electric motor, and to an electromechanical actuator. The control ...

    ACTUATOR AND LENGTH CONTROL SYSTEM

    Freier Zugriff
    YASUDA SUSUMU / KITAMOTO KAZUYA | Europäisches Patentamt | 2020

    To provide an actuator which makes response to input quicker.SOLUTION: An actuator 1 includes: a first support member 16 and a second

     ...

    Aerospace Fluid Power - FAA Regulatory History - Transport Airplane Hydraulic Systems

    SAE Technical Papers | 2019
    This SAE Aerospace Information Report (AIR) contains regulatory and guidance information related to transport airplane hydraulic systems ...
    Schlagwörter: Flight control actuators

    Development Process - Aerospace Fly-By-Wire Actuation System

    SAE Technical Papers | 2020
    This document provides a description of a process for development of fly-by-wire actuation systems. Included are (1) the development of ...

    Aerospace Hydraulics and Actuation Lessons Learned

    SAE Technical Papers | 2010
    This SAE Aerospace Information Report (AIR) contains Lessons Learned from aerospace actuation, control and fluid power systems technologies ...
    Schlagwörter: Flight control actuators

    Aerospace Fluid Power - FAA Regulatory History - Transport Airplane Hydraulic Systems

    SAE Technical Papers | 2013
    This SAE Aerospace Information Report (AIR) contains regulatory and guidance information related to transport airplane hydraulic systems ...
    Schlagwörter: Flight control actuators

    ALIGNMENT SYSTEMS AND METHODS FOR MOVING FUSELAGE STRUCTURES OF AEROSPACE VEHICLE INTO ASSEMBLY ALIGNMENT

    Freier Zugriff
    JAKE A WILSON / CRAIG A CHARLTON / ANDREW M HUCKEY et al. | Europäisches Patentamt | 2019

    To provide alignment systems and methods for moving fuselage structures of an aerospace vehicle into assembly alignment.SOLUTION: The

     ...

    Coiled Tubing, Corrosion Resistant Steel, Hydraulic Applications, Aerospace

    SAE Technical Papers | 2002
    This SAE Aerospace Recommended Practice (ARP) encompasses design, analysis, fabrication, and installation of pressurized metal tubing used ...

    Development Process - Aerospace Fly-By-Wire Actuation System

    SAE Technical Papers | 1997
    This document provides a description of a process for development of fly-by-wire actuation systems. Included are (1) the development of ...

    Evaluation of a High-Torque Backlash-Free Roller Actuator

    Steinetz, Bruce M. / Rohn, Douglas A. / Anderson, William | NTRS | 1986
    holding capability of a 16:1 ratio, 430 N-m (320 ft-lb) planetary roller drive for a potential space vehicle actuator application. The drive's ...

      Evaluation of a high-torque backlash-free roller actuator

      Steinetz, Bruce M. / Rohn, Douglas A. / Anderson, William | NTRS | 1986
      capability of a 16:1 ratio, 430 N-m (320 ft-lb) planetary roller drive for a potential space vehicle actuator application. The drive's planet roller ...

    Biologically-Inspired Micro-Robots. Volume 1. Robots Based on Crickets

    R. Quinn / R. Ritzmann / S. Phillips et al. | NTIS | 2005
    , supplied by the compressor, from the plenum to the actuators on the rear legs. A six-legged non-autonomous vehicle was designed, constructed and ...
    Verlag: Case Western Reserve Univ., Cleveland, OH. Dept. of Mechanical and Aerospace Engineering
    Schlagwörter: Actuators

    Development and Validation of an Aircraft Seat Cushion Component Test, Volume 1

    S. J. Hooper / M. J. Henderson | NTIS | 2005
    originally certified to the requirements of Title 14 Code of Federal Regulations 25.562 or Technical Standard Order C127a. The methodology ...

    Eighth Space Cryogenic Workshop, 31 July-1 Aug. 1989, Pasadena, CA, USA

    Tema Archiv | 1990
    ; mechanical cryocoolers; sorption cooler technology; closed cycle cooler; stress analysis; cryogenic valve actuator; dilution refrigeration ...
    Schlagwörter: AEROSPACE , CRYOGENIC VALVE ACTUATOR

    Application of Model Following Control and Estimation Techniques to Attitude Control of Maneuvering Spacecraft. Part 1. Theory and Simulation Results

    T. Zwartbol / A. P. Terpstra / P. T. L. M. Vanwoerkom et al. | NTIS | 1982
    system comprises a strapdown rate-integrating gyro and a slit-type star sensor for optical-inertial attitude sensing, a reaction wheel actuator ...
    Verlag: National Aerospace Lab., Amsterdam (Netherlands)

    Semiannual Technical Summary Report No. 2, 1 Jul-31 Dec 59

    NTIS | 1960
    Schlagwörter: Launch vehicle (Aerospace) , Actuators , H-1 engines

    HYDRAULISCHER FLUGSTEUERAKTUATOR MIT DOPPELDICHTUNGSVORRICHTUNG UND DEFINIERTER LECKAGE

    Freier Zugriff
    KLETT JÜRGEN / KEGEL PHILIPP / PETRETTI ALBERT et al. | Europäisches Patentamt | 2018
    Zylinder sowie eine Doppeldichtungsvorrichtung mit wenigstens einer Primärdichtung (1) und wenigstens einem Kolbenring (2) als Sekundärdichtung (2 ...

    INLET ARRANGEMENT, A PROPULSION SYSTEM, AND AN AIRCRAFT

    Freier Zugriff
    FREUND DONALD / MUZYCHKA DEREK / KLUTZKE DOUGLAS | Europäisches Patentamt | 2023

    An inlet arrangement for a propulsion system includes an actuator, a linkage and an inlet assembly. The inlet assembly includes (1) a

     ...

      INLET ARRANGEMENT, A PROPULSION SYSTEM, AND AN AIRCRAFT

      Freier Zugriff
      FREUND DONALD / MUZYCHKA DEREK / KLUTZKE DOUGLAS | Europäisches Patentamt | 2023

      An inlet arrangement for a propulsion system includes an actuator (64), a linkage (62) and an inlet assembly (32, 3). The inlet assembly

       ...

    Flexible Spacecraft Three Axis Attitude Maneuver by Active Vibration Control

    Freier Zugriff
    M. Sayanjali / J. Roshanian / A. Ghafari | DOAJ | 2009
    vibration control method by PZT actuator. Control law for vibration control is based on LQG method ...
    Verlag: Aerospace Research Institute