Zobrazeno 1 - 9
of 9
pro vyhledávání: '"Lizhen Miao"'
Publikováno v:
IEEE Access, Vol 6, Pp 23896-23906 (2018)
In order to damp torsional vibrations in a helicopter, which would cause resonance in rotating components like engine, transmission, and rotor, an adaptive notch filter is proposed. Instead of fixed notch filter, the adaptive one, with FFT analyzer a
Externí odkaz:
https://doaj.org/article/4359c7abd13e4a9f8a5780790946c755
Publikováno v:
Journal of Tissue Viability. 31:259-267
Pressure injury imposes a significant burden for patients and healthcare systems and the majority of pressure injuries are preventable. The early identification of pressure injury is critical for its prevention. As an objective measure, biomarkers ha
Autor:
Yuanyuan, Zhang, Hongxia, Lu, Lizhen, Miao, Yanru, Chen, Xiaoli, Chen, Yutan, Wang, Sijun, Li, Xiangping, Fan, Fanghong, Yan, Wenjie, Shang, Lin, Han, Yuxia, Ma
Publikováno v:
Health & Social Care in the Community. 30
The ageing of the population has resulted in an increase in the demand for long-term care services for older people, but with limited resources, its challenges have also been highlighted. Although factors affecting the willingness of older people to
Publikováno v:
Proceedings of the Institution of Mechanical Engineers, Part I: Journal of Systems and Control Engineering. 231:554-566
A real-time optimization control method is proposed to enhance engine thrust response and enlarge its maximum thrust during emergent flight. This real-time optimization control is model based, and ...
Publikováno v:
International Journal of Turbo & Jet-Engines.
A real-time optimization control method is proposed to extend turbo-fan engine service life. This real-time optimization control is based on an on-board engine mode, which is devised by a MRR-LSSVR (multi-input multi-output recursive reduced least sq
Law of Torsional Vibration and Discussion on Vibration Suppression Based on Helicopter/Engine System
Publikováno v:
International Journal of Turbo & Jet-Engines. 33
With both the advantages like attacking close targets and the disadvantages especially like dynamic coupling, helicopter deserves more investigations these days. This paper did dynamic study both in a simplified and a multi-degree of freedom, compreh
Publikováno v:
International Journal of Turbo & Jet-Engines. 33
An integrated model including inlet, engine and nozzle with their internal and external characteristics was built to simulate the propulsion installed performance. With the integrated model, a new performance seeking control scheme under supersonic s
Publikováno v:
International Journal of Turbo & Jet-Engines. 32
A closed-loop control law employing compressor guided vanes is firstly investigated to solve unacceptable fuel flow dynamic change in single fuel control for turbo-shaft engine here, especially for rotorcraft in variable rotor speed process. Based on
Publikováno v:
International Journal of Turbo & Jet-Engines; Dec2017, Vol. 34 Issue 4, p321-332, 12p