scholarly journals Measurements of Fast Transitions at a Reversible Pump Turbine Model in Closed Loop Test Rig

2021 ◽  
Vol 1909 (1) ◽  
pp. 012087
Author(s):  
J Junginger ◽  
O Kirschner ◽  
S Riedelbauch
Author(s):  
Deyou Li ◽  
Hongjie Wang ◽  
Jinxia Chen ◽  
Torbjørn K. Nielsen ◽  
Daqing Qin ◽  
...  

The hump characteristic is one of the major instabilities in pump-turbines. When pump-turbines operate in the hump region, strong noise and serious fluctuations could be observed, which are harmful to the safe and stable operations and even destroy the whole unit as well as water conveyance system. In this paper, a low specific speed (nq = 36.1 min−1) pump-turbine model was experimentally investigated. Firstly, the hump characteristic was obtained under 19 mm guide vane opening. More interestingly, when the hump characteristic was measured in two directions (increasing and decreasing the discharge), the hysteresis characteristic was found during the hump region. The analysis of performance characteristics reveals that the hump instability is resultant of Euler momentum and hydraulic losses, and different Euler momentum and hydraulic losses in the two development processes lead to hysteresis phenomenon. Then, 12 pressure sensors were mounted in the different parts of the pump-turbine model to obtain the time and frequency characteristics. The analysis of fast Fourier transform confirms that the hump characteristic is related to the low-frequency (0.04–0.15 times rotational frequency) vortices. The occurrence and cease of vortices depend on the operating condition and measurement direction, which contribute to the hysteresis characteristic. Finally, the type of the low-frequency vortices was analyzed through the cross power spectrum.


2015 ◽  
Vol 77 ◽  
pp. 32-42 ◽  
Author(s):  
Li Deyou ◽  
Wang Hongjie ◽  
Xiang Gaoming ◽  
Gong Ruzhi ◽  
Wei Xianzhu ◽  
...  

Energies ◽  
2016 ◽  
Vol 9 (8) ◽  
pp. 620 ◽  
Author(s):  
Deyou Li ◽  
Hongjie Wang ◽  
Jinxia Chen ◽  
Torbjørn Nielsen ◽  
Daqing Qin ◽  
...  

2013 ◽  
Vol 52 (5) ◽  
pp. 052023 ◽  
Author(s):  
D Y Li ◽  
H J Wang ◽  
J L Zhao ◽  
R Z Gong ◽  
X Z Wei ◽  
...  

2016 ◽  
Vol 29 (4) ◽  
pp. 803-812 ◽  
Author(s):  
Deyou Li ◽  
Ruzhi Gong ◽  
Hongjie Wang ◽  
Gaoming Xiang ◽  
Xianzhu Wei ◽  
...  

Aviation ◽  
2010 ◽  
Vol 14 (1) ◽  
pp. 3-11 ◽  
Author(s):  
Tadeusz Markowski ◽  
Stanislaw Noga ◽  
Stanislaw Rudy

The development of computer techniques and computational systems based on the finite element method allows one to conduct a free vibration analysis of large systems like an aviation gearbox test rig. The object of this paper is to present a free vibration analysis of a gear fatigue test rig working in a closed loop configuration. A numerical model of the test rig based on the finite element method is presented in this paper. The base model contains all the essential structures of the real system. After the numerical results of the natural frequencies of the rig were obtained, they were then verified by the experimental results on a real object. Numerical analysis was performed using the ANSYS code. Santrauka Baigtiniu elementu metodu paremtas kompiuterines technikos ir kompiuteriniu sistemu kūrimas leidžia atlikti laisvuju svyravimu analize tokios dideles sistemos, kaip aviacines pavaru dežes, testavimo irenginys. Šio darbo tikslas buvo atlikti pavaru dežes nuovargio bandymu irenginio, veikiančio uždaro kontūro konfigūracijoje, laisvuju svyravimu analize. Taip pat pateikiamas testavimo irenginio skaitinis modelis, kurio veikimas yra pagristas baigtiniu elementu metodu. Pagrindinis modelis turi visas tikrosios sistemos svarbiausias struktūras. Gavus irenginio savuju dažniu kiekybinius rezultatus, buvo patikrinti realaus objekto eksperimentiniai rezultatai. Naudojantis ANSYS sistema buvo atlikta skaitine analize.


1987 ◽  
Vol 109 (3) ◽  
pp. 276-285 ◽  
Author(s):  
S. LeQuoc ◽  
R. M. H. Cheng ◽  
A. Limaye

This paper describes a new concept of electrohydraulic servovalve where the novelty lies mainly in the fact that the return pressure and return orifice of the servovalve are tuneable and can be adjusted to satisfy the system control requirements. The actuator velocity characteristics of a hydraulic servomechanism operating under steady state condition is analysed through the use of dimensionless quantities. It is established that the proposed configuration exhibits a nonlinear actuator velocity versus servovalve opening relationship and at small servovalve opening, the system offers a higher actuator velocity. The closed loop system transient responses are also investigated by means of digital computer simulation. The results are experimentally verified on a test rig specifically designed for this purpose. It is observed that with the return pressure and return orifice properly tuned, one can achieve a high gain yet high damping servosystem. A design procedure is described which provides the designer with a step by step method for determining the tuning parameters in order to obtain a desired system performance.


2015 ◽  
Vol 18 (4) ◽  
pp. 49-55
Author(s):  
Patrick Mark Singh ◽  
Chengcheng Chen ◽  
Zhenmu Chen ◽  
Young-Do Choi

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