Results 51 to 60 of about 63,012 (308)

Analysis and experimental validation of a pressure control method using magneto-rheology fluid flows

open access: yesThe Journal of Engineering, 2018
In this study, a spool actuating mechanism using controlled pressure difference is proposed for a large hydraulic servo valve. The actuating mechanism is accomplished by tuning magneto-rheological (MR) fluid flow.
Fan Wang, Ning Guo, Linxiang Wang
doaj   +1 more source

Frequency Domain Design Method of the Aeroengine Fuel Servo Constant Pressure Difference Control System with High Performance

open access: yesAerospace, 2022
The constant pressure difference regulating mechanism is widely used in aeroengine fuel servo metering systems, and it almost decides the metering precision.
Wenshuai Zhao   +4 more
doaj   +1 more source

Parachute glider Patent [PDF]

open access: yes, 1965
Multiple parachute system for landing control of Apollo type ...
Kehlet, A. B.
core   +1 more source

Performance comparison between PID and fuzzy logic controller in position control system of dc servomotor [PDF]

open access: yes, 2006
The objective of this paper is to compare the time specification performance between conventional controller and artificial intelligence controller in position control system of a DC motor. This will include design and development of a GUI software using
Md. Ghazaly, Mariam, Rahmat, Mohd Fua'ad
core   +1 more source

Shape‐Morphing Nanoengineered Hydrogel Ribbons as Hemostats

open access: yesAdvanced Functional Materials, EarlyView.
This study introduces a self‐assembling, shape‐morphing nanoengineered hydrogel ribbon system that rapidly forms porous aggregates in situ for efficient hemostasis in trauma and surgical applications. Abstract Rapid and effective hemorrhage control remains a major challenge in trauma and surgical care, particularly for complex or noncompressible wounds.
Ryan Davis Jr   +9 more
wiley   +1 more source

Research on Fatigue Stability of Rocket Launcher High Thrust Electro-mechanical Servo Actuator

open access: yesJixie chuandong, 2022
The high thrust electro-mechanical servo actuator in rocket launcher is a linear transmission mechanism with high precision planetary roller screw as its core component.
Jianxin Zhang, Wenzhu Deng, Wei Lei
doaj  

A New 3D Colon on a Chip to Decipher the Influence of Mechanical Forces on the Physiological Cellular Ecosystem

open access: yesAdvanced Healthcare Materials, EarlyView.
To dissect how mechanical forces influence intestinal physiology, we developed a stretchable 3D colon‐on‐chip that integrates tunable topography, stiffness and peristalsis‐like motion within a physiologically relevant microenvironment. We showed that stretching is a dominant factor governing epithelial behavior, markedly enhancing proliferation and ...
Moencopi Bernheim‐Dennery   +10 more
wiley   +1 more source

Research and Simulation Analysis of Fuzzy Intelligent Control System Algorithm for a Servo Precision Press

open access: yesApplied Sciences
With the rapid development of the manufacturing industry toward intelligence and flexibility, traditional mechanical presses are unable to meet the increased stamping requirements due to the difficulties in achieving variable speed control and changing ...
Yanzhong He, Xiang Luo, Xingsong Wang
doaj   +1 more source

Design of High-Dynamic PMSM Servo Drive Using Nonlinear Predictive Controller with Harmonic Disturbance Observer

open access: yesEnergies, 2022
The high-dynamic permanent magnet (PM) motor servo system with high-bandwidth is the core equipment for industrial production, and the control bandwidth is also an important indexes to evaluate the performance of the servo system. The non-cascaded direct
Zhanqing Zhou   +4 more
doaj   +1 more source

Deployment/retraction mechanism for solar maximum mission high gain antenna system [PDF]

open access: yes, 1979
A mechanism called a deployment/retraction assembly (DRA) which provides not only a stable, but a deployable platform for the high gain antenna system (HGAS) aboard the Solar Maximum Mission (SMM) spacecraft is described.
Bennett, N., Preiswerk, P.
core   +1 more source

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