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

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    Amplified piezoelectric actuators: from aerospace to underwater applications

    Bouchilloux, P. / Claeyssen, F. / Le Letty, R. | Tema Archiv | 2004
    Aerospace and underwater applications typically require actuators capable of large displacements, precise positioning, and fast response ...
    Schlagwörter: piezoelektrischer Aktor , intelligenter Aktor

    A Quasi-1-D Model for Arbitrary 3-D Synthetic Jet Actuators

    Yamaleev, Nail / Carpenter, Mark | AIAA | 2005

      A Quasi-1-D Model for Arbitrary 3-D Synthetic Jet Actuators

      Yamaleev, N. K. / Carpenter, M. H. / American Institute of Aeronautics and Astronautics | British Library Conference Proceedings | 2005
      Schlagwörter: Aerospace sciences

    Index of Aerospace Mechanisms Symposia Proceedings 1-19

    A. Rinaldo / J. Wilson | NTIS | 1986
    This index, organized in five sections (by symposium, by title, by author, by subject, and by project), brings together information on the ...
    Schlagwörter: Actuators , Aerospace systems

    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

    ARTIFICIAL SATELLITE AND AEROSPACE SIMULATOR

    Freier Zugriff
    YAGI FUMIYA / INOUE TEIICHIRO / HIRAYAMA YOSHIKAZU | Europäisches Patentamt | 2018
    cost.SOLUTION: An aerospace simulator has the function (corresponding to a satellite state setting part 10) of setting a satellite state under a ...

    ACTUATOR AND ACTIVE TRUSS

    Freier Zugriff
    YASUDA SUSUMU / KITAMOTO KAZUYA / KAMIYA TOMOHIRO et al. | Europäisches Patentamt | 2017

    PROBLEM TO BE SOLVED: To provide an actuator having such an effect that the responsiveness of dimension control becomes early.SOLUTION

     ...

    Photodeformation and Light-Temperature-Piezoelectric Coupling of Optical Actuators: Part 1 - Parameter Calibrations

    Liu, B. / Tzou, H. S. / ASME; Aerospace Division | British Library Conference Proceedings | 1996
    Schlagwörter: aerospace

    Development of a Robust, Multi-Level, Flow-Control Actuator Part 1: Experimental Studies (AIAA 2018-1055)

    Binkley, Brian / Vakili, Adam | British Library Conference Proceedings | 2018

    Architectures and Geometric Integration of Hydraulically‐supplied Actuators

    Maré, Jean‐Charles | Wiley | 2016
    integration. For actuators with a mechanical control signal input, geometrical integration must allow the position servo‐loop to be established. ...
    Schlagwörter: actuator integration , hydraulically‐supplied 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

    DECELERATOR FOR LANDING BODIES IN AEROSPACE FIELD

    Freier Zugriff
    AURIGEMMA RENATO / DELL'AVERSANA PASQUALE / GRAMICCIA LUCIANO et al. | Europäisches Patentamt | 2019

    Decelerator (1) for landing bodies, comprising a folding braking shield (3) and an articulated frame (2), to which said folding braking

     ...

      DECELERATOR FOR LANDING BODIES IN AEROSPACE FIELD

      Freier Zugriff
      AURIGEMMA RENATO / DELL'AVERSANA PASQUALE / GRAMICCIA LUCIANO et al. | Europäisches Patentamt | 2018

      Decelerator (1) for landing bodies, comprising a folding braking shield (3) and an articulated frame (2), to which said folding braking

       ...

    Index of aerospace mechanisms symposia proceedings 1-19

    Rinaldo, A. / Wilson, J. | NTRS | 1986
    This index, organized in five sections (by symposium, by title, by author, by subject, and by project), brings together information on the ...

    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 ...

    POWER CONTROLLER FOR LINEAR ACTUATOR IN DOCKING DEVICE

    Freier Zugriff
    USUKU KOSHIRO / ISAYAMA MICHIO / MOCHIGI AKIRA et al. | Europäisches Patentamt | 2024

    A power controller of a linear actuator 10 in a docking device 1 including a six-axis parallel link mechanism 5, wherein a motor driver

     ...

    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

    A tilt-rotor actuator

    White, G. | Tema Archiv | 2010
    possible failure at the system and component levels is emphasized throughout. Finally, in Appendix 1, actuator schematics for the tilt-rotor XV-15 ...
    Schlagwörter: Aktor

    OPENING SERVOMECHANISM FOR AEROSPACE PLATFORMS AND MECHANICAL COMPONENTS

    Freier Zugriff
    AURIGEMMA RENATO / DELL'AVERSANA PASQUALE / GRAMICCIA LUCIANO et al. | Europäisches Patentamt | 2016

    A braking and thermal protection device (1) for landing bodies, comprising a folding braking shield (3) and an articulated frame (2), to

     ...

    Electromechanical Actuator Cooling Fan Blades Design and Optimization

    Gyasi, Edmund / Kizito, John P. / Chow, Louis et al. | SAE Technical Papers | 2016
    For aircraft electromechanical actuator (EMA) cooling applications using forced air produced by axial fans, the main objective in fan ...

    POWER CONTROL DEVICE FOR LINEAR ACTUATOR IN DOCKING DEVICE

    Freier Zugriff
    USUKU KOSHIRO / ISAYAMA MICHIO / MOCHIGI AKIRA et al. | Europäisches Patentamt | 2022

    This power control device is for a linear actuator 10 in a docking device 1 having a six-axis parallel link mechanism 5. A motor driver

     ...

    Infrared Laser-Activated Shape Memory Actuators

    Zhang, Dawei / Liu, Yanju / Leng, Jinsong | ASCE | 2008
    one of novel actuators in smart materials, shape memory polymers (SMP) have been investigated widely. The infrared laser was chose to drive ...
    Schlagwörter: Aerospace engineering

    POWER CONTROL DEVICE OF LINEAR ACTUATOR OF DOCKING DEVICE

    Freier Zugriff
    USUKU KOSHIRO / ISAYAMA MICHIO / MOCHIKI AKIRA et al. | Europäisches Patentamt | 2022
    control device of a linear actuator 10 of a docking device 1 having a six-axis parallel link mechanism 5, a motor driver 11 for controlling a ...

    Risk of Impaired Performance Due to Reduced Muscle Mass, Strength &, Endurance (Short Title: Muscle) and Risk of Reduced Physical Performance Capabilities Due to Reduced Aerobic Capacity (Short Title: Aerobic)

    Eric Rivas / Nicole Strock / E. Lichar Dillon et al. | NTRS | 2023
    . Lastly, in-flight evaluation of hardware exercise response may differ in 0-g or partial-g compared to 1-g. Therefore, it cannot be assumed that ...
    Schlagwörter: Aerospace Medicine

    Gurney-Flap Drag Penalty Reduction with a DBD Plasma Actuator

    Zhang, Zeng / Feng, Lihao / Wang, Jinjun et al. | ASCE | 2017
    (DBD) plasma actuator, which was mounted in front of the Gurney flap to generate a countercurrent wall jet. The research was based on numerical ...

      Gurney-Flap Drag Penalty Reduction with a DBD Plasma Actuator

      Zhang, Zeng | Online Contents | 2017
      actuator, which was mounted in front of the Gurney flap to generate a countercurrent wall jet. The research was based on numerical simulation ...
      Schlagwörter: Actuators

    Achieving a High-Speed and Momentum Synthetic Jet Actuator

    Amitay, Michael | Online Contents | 2016
    momentum synthetic jet, with a peak velocity exceeding 200  m/s. A total of two scales of actuator apparatuses having either 40- or 80-mm-diameter ...
    Schlagwörter: Actuators

    Achieving a High-Speed and Momentum Synthetic Jet Actuator

    Van Buren, Tyler / Whalen, Edward / Amitay, Michael | ASCE | 2015
    200 m / s . A total of two scales of actuator ...

    Doubly Coupled Antagonistic Shape Memory Alloy Actuator for Morphing Wing

    Suzuki, Shingo / Senba, Atsuhiko / Ikeda, Tadashige et al. | Springer Verlag | 2022

    Shape memory alloy (SMA) wires have received considerable attention for use in actuators in morphing wings. This

     ...
    Schlagwörter: Actuator , Aerospace Technology and Astronautics

    Turbine Tip Clearance Flow Control Using Plasma Actuators (AIAA2006-0021)

    Van Ness II, D. K. / Corkepott, T. C. / Morris, S. C. et al. | British Library Conference Proceedings | 2006
    Schlagwörter: Aerospace sciences

    L1 Adaptive Control of a Projectile Fin by Piezoelectric Actuator

    Lee, Keum W. / Singh, Sahjendra N. | ASCE | 2012
    1 adaptive control system is designed for the control of a projectile fin. The rotational ...

    Distributed FTCC of Multi-UAVs Under Actuator Fault and Input Saturation

    Yu, Ziquan / Zhang, Youmin / Jiang, Bin et al. | Springer Verlag | 2023
    . 1, multi-UAVs can provide high efficiency in many fields, such as forest fire monitoring, detection and fighting, and ...
    Schlagwörter: Aerospace Technology and Astronautics

    Closed-Loop Based Control Allocation for Spacecraft Attitude Stabilization with Actuator Faults

    Hu, Qinglei / Li, Bo / Xiao, Bing et al. | Springer Verlag | 2021

    During the aerospace missions for the on-orbiting spacecraft, actuator faults are frequently encountered such

     ...
    Schlagwörter: Aerospace Technology and Astronautics

    Advanced Materials Flight Control Actuators

    Ching, Fred | SAE Technical Papers | 1990
    specification (F/A-18), Figure 1. In addition, the composite actuator is “jam resistant”, satisfying a survivability requirement for the Navy/Naval ...

    1986-1999 combined index IEEE aerospace and electronic systems magazine vols. 1-14 [Subject Index]

    IEEE | 2000
    primary entry includes the co-authors' names, the title of the paper or other item, and its location, specified by the publication abbreviation ...

    1986-1999 combined index IEEE aerospace and electronic systems magazine vols. 1-14 [Author Index]

    IEEE | 2000
    primary entry includes the co-authors' names, the title of the paper or other item, and its location, specified by the publication abbreviation ...

    Design and Experiment on Aircraft Electromechanical Actuator Fan at Different Altitudes and Rotational Speeds

    Gyasi, E. / Kizito, J.P. / Chow, L.C. et al. | SAE Technical Papers | 2019
    For electromechanical actuators (EMAs) and electronic devices cooling on aircraft, there is a need to study cooling fan performance at ...
    Schlagwörter: Sensors and actuators

    Numerical design and analysis of a multi-DBD actuator configuration for the experimental testing of ACHEON nozzle model

    Abdollahzadeh, M. / Rodrigues, F. / Pascoa, J.C. et al. | Elsevier | 2014
    Abstract Two dimensional numerical simulations of plasma actuator flow ...
    Schlagwörter: Plasma actuators

    Smart electronics ans MEMS for aerospace structures

    Varadan, V.K. / Varadan, V.V. | Tema Archiv | 1995
    sensors are designed to measure both pressure and shear of the fluid flow on aerospace structures. The wave form measurements may be monitored at ...
    Schlagwörter: Stellglied

    An experimental and numerical study of piezoceramic actuator hysteresis in helicopter active vibration control

    Mallick, Rajnish / Ganguli, Ranjan / Bhat, M. Seetharama | SAGE Publications | 2014
    An aeroelastic analysis is used to investigate the rate dependent hysteresis in piezoceramic actuators and its effect on helicopter ...

    Investigation of actuator placement approaches for active vibration control in the aircraft engine

    Xiaonan Zhao, / Rinderknecht, Stephan | IEEE | 2015
    of actuators play an important role in the effectiveness of vibration reduction. Two approaches of actuator placement along the vibration ...

    Silicon Microsensors for Aerospace Condition Monitoring

    Henderson, H. Thurman / Barkhoudarian, Sarkis | SAE Technical Papers | 1993
    aerospace condition and “health monitoring” by (1) moving “smart” electronics out to the sensor chip itself and (2) combining a vast quantity and ...
    Schlagwörter: Sensors and actuators

    Separated-Flow Control Simulation with a Periodic Excitation by SDBD Plasma Actuator at Re=O(205)

    Bernal-Orozco, R. A. / Arias-Montano, Alfredo / Huerta-Chávez, O. | ASCE | 2020
    dielectric-barrier discharge (SDBD) plasma actuator applied to an airfoil section at ...

    Fault tolerant control against actuator faults based on enhanced PID controller for a quadrotor

    Ermeydan, Ahmet / Kiyak, Emre | Emerald Group Publishing | 2017
    steady state error, and it does not go unstable. Motor 1 and Motor 3 respond to given motor fault quickly. When it comes to one actuator fault ...

    Turbine Blade Tip Leakage Flow Control by Partial Squealer Tip and Plasma Actuators (AIAA2006-0020)

    Douville, T. / Stephens, J. / Corke, T. et al. | British Library Conference Proceedings | 2006
    Schlagwörter: Aerospace sciences

    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

     ...