Results 1 to 10 of about 283 (166)

Delay Analysis and the Control of Electro-Hydrostatic Actuators

open access: yesApplied Sciences, 2022
The electro-hydrostatic actuator (EHA) has a high energy density and a compact structure so it is widely used in all/more electric aircraft. To gain energy-saving capability, the hydraulic lock can be applied in the EHA system, which can overcome the ...
Jiaming Zhang   +4 more
doaj   +2 more sources

Biomimetic Linkage Mechanism Robust Control for Variable Stator Vanes in Aero-Engine [PDF]

open access: yesBiomimetics
This work addresses the position tracking control design of the stator vane driven by electro-hydrostatic actuators facing uncertain aerodynamic disturbances.
Qinqin Sun   +3 more
doaj   +2 more sources

Intelligent Health Assessment of Aviation Bearing Based on Deep Transfer Graph Convolutional Networks under Large Speed Fluctuations [PDF]

open access: yesSensors, 2023
As a critical support and fixed component of aero engines, electro-hydrostatic actuators, and other equipment, the operation of aviation bearings is often subject to high speed, high-temperature rise, large load, and other continuous complex fluctuation ...
Xiaoli Zhao   +7 more
doaj   +2 more sources

Design and Performance Study for Electrothermally Deep-Sea Drive Microunits Using a Paraffin Phase Change Material [PDF]

open access: yesMicromachines, 2021
Considering the further exploration of the ocean, the requirements for deep-sea operation equipment have increased. Many problems existing in the widely used deep-sea hydraulic system have become increasingly prominent. Compared with the traditional deep-
Dayong Ning   +6 more
doaj   +2 more sources

Dynamically Weighted Spatiotemporal Fusion for Deep Learning-Based Prediction of EHA Degradation in Aviation Systems [PDF]

open access: yesSensors
Electro-hydrostatic actuators (EHAs) are increasingly deployed in modern aircraft due to their compact size, fast response, and high power-to-weight ratio.
Tianyuan Guan   +7 more
doaj   +2 more sources

Thermal Characteristic and Analysis of Electro-Hydrostatic Actuator

open access: yesIEEE Access
Electro-hydrostatic actuators (EHAs) are widely utilized due to their superior integration and high power-to-weight ratio. However, the elimination of a centralized oil source in EHAs restricts the cooling capacity of the system, leading to potential ...
Jiahui Liu   +6 more
doaj   +2 more sources

Research on Fault Diagnosis Method of Electro‐Hydrostatic Actuator [PDF]

open access: yesShock and Vibration, 2021
Electrohydrostatic actuator is a type of actuator that uses hydraulic energy as the energy transmission carrier, which has the advantages of small size and high power. Since it is commonly used in harsh conditions such as strong vibration, high pressure, and heavy loads, condition monitoring and fault diagnosis of its hydraulic system are particularly ...
Lei Zhufeng   +4 more
openaire   +2 more sources

Disturbance Observer-Based Sliding Mode Controller for Underwater Electro-Hydrostatic Actuator Affected by Seawater Pressure

open access: yesMachines, 2022
This paper presents a disturbance-observer-based sliding mode control strategy for an underwater electro-hydrostatic actuator, particularly considering that electro-hydrostatic actuators (EHAs) significantly suffer from sea pressure disturbance, which ...
Yong Nie   +6 more
doaj   +1 more source

Results of a Feasibility Study of a Prognostic System for Electro-Hydraulic Flight Control Actuators

open access: yesInternational Journal of Prognostics and Health Management, 2021
Electro-Hydraulic Servo-Actuators (EHSA) are currently the most used actuation technology for primary flight control systems of civil and military aircrafts. Although some alternatives have emerged in the last decade, such as electromechanical or electro-
Sylvain Autin   +3 more
doaj   +1 more source

Validation of Aero-Load Estimator for Convair 880 Aircraft Flight Simulator Benchmark with Electro-Hydrostatic Actuators [PDF]

open access: yesINCAS Bulletin, 2021
Simulating an aircraft model using of high fidelity models of subsystems for its primary and secondary flight control actuators requires measuring or estimating aero-load data acting on flight control surfaces.
Yamina BOUGHARI   +4 more
doaj   +1 more source

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