Experimental Study on Thrust Foil Gas Bearing Using Metal Mesh

2017 ◽  
Vol 2017.23 (0) ◽  
pp. 1910
Author(s):  
Tomonori MATSUSHITA ◽  
Yuta SUNAMI ◽  
Hiromu HASHIMOTO ◽  
Masayuki OCHIAI
1968 ◽  
Vol 90 (4) ◽  
pp. 687-696 ◽  
Author(s):  
R. Y. Wong ◽  
W. L. Stewart ◽  
H. E. Rohlik

This paper describes findings obtained to date in the area of journal gas bearings from an experimental study of a Brayton cycle turbocompressor designed for the requirements of a two-shaft 10-kw space power system. The journal bearing design utilizes three pads pivoted on conforming balls and sockets. Two of the pivots are rigidly mounted to the frame, and the third pivot is mounted to the frame through a low-spring-rate diaphragm. This paper describes the salient package and bearing design features and then presents the principal results obtained from testing the package in both a spin calibration rig and operation at design temperature conditions with an inert gas. The results discussed include (a) the successful use of a pneumatic loading device to vary pad load during operation, (b) the operating characteristics of the bearings as obtained over a range of pad loads and ambient conditions, (c) structural and dynamic behavior of the bearing-support system during design temperature operation and (d) a discussion of the wear characteristics of the conforming ball-and-socket pivot as obtained from the tests made to date.


Author(s):  
Adolfo Delgado

Compliant hybrid gas bearings combine key enabling features from both fixed geometry externally pressurized gas bearings and compliant foil bearings. The compliant hybrid bearing relies on both hydrostatic and hydrodynamic film pressures to generate load capacity and stiffness to the rotor system, while providing damping through integrally mounted metal mesh bearing support dampers. This paper presents experimentally identified force coefficients for a 110 mm compliantly damped gas bearing using a controlled-motion test rig. Test parameters include hydrostatic inlet pressure, excitation frequency, and rotor speed. The experiments were structured to evaluate the feasibility of implementing these bearings in large size turbomachinery. Dynamic test results indicate weak dependency of equivalent direct stiffness coefficients to most test parameters except for frequency and speed, where higher speeds and excitation frequency decreased equivalent bearing stiffness values. The bearing system equivalent direct damping was negatively impacted by increased inlet pressure and excitation frequency, while the cross-coupled force coefficients showed values an order of magnitude lower than the direct coefficients. The experiments also include orbital excitations to simulate unbalance response representative of a target machine while synchronously traversing a critical speed. The results indicate that the gas bearing can accommodate vibration levels larger than the set bore clearance while maintaining satisfactory damping levels.


2015 ◽  
Vol 29 (5) ◽  
pp. 2089-2095 ◽  
Author(s):  
Yu Hou ◽  
Bin Ma ◽  
Shanju Yang ◽  
Xingya Chen ◽  
Yueqing Zheng ◽  
...  

2012 ◽  
Vol 220-223 ◽  
pp. 611-614
Author(s):  
Ru Gang Chen ◽  
Ya Jun Nie ◽  
Quan Zhou ◽  
Chao Gong ◽  
Tao Chen

A new type of hydrostatic journal gas bearing with axial slot of tangential gas entry for miniature air turboexpander is firstly developed in this paper. This bearing configuration is presented and constructed to fit manufacture simplicity. The experimental investigations are carried out to reveal the relationship between bearing parameters and instability threshold speed. It is feasible to increase the stability of hydrostatic journal gas bearing by adopting this kind of configuration with axial slot of tangential gas entry. Some valuable tested results are obtained to reveal the optimum slot height and radial clearance for this miniature air turboexpander.


2006 ◽  
Vol 5 (2) ◽  
pp. 115
Author(s):  
E. Liatsikos ◽  
T. Voudoukis ◽  
D. Karnabatidis ◽  
N. Christeas ◽  
G. Kagadis ◽  
...  

2004 ◽  
Vol 2004.3 (0) ◽  
pp. 351-352
Author(s):  
Hideo YOSHIDA ◽  
Hideomi ISHIBE ◽  
Hiroki MATSUI ◽  
Takeshi EGAWA ◽  
Satoshi YOSHITOMI ◽  
...  

Author(s):  
Adolfo Delgado

Compliant hybrid gas bearings (HGBs) combine key enabling features from both fixed geometry externally pressurized gas bearings and compliant foil bearings. The compliant hybrid bearing relies on both hydrostatic and hydrodynamic film pressures to generate load capacity and stiffness to the rotor system, while providing damping through integrally mounted metal mesh bearing support dampers. This paper presents experimentally identified force coefficients for a 110 mm compliantly damped gas bearing using a controlled-motion test rig. Test parameters include hydrostatic inlet pressure, excitation frequency, and rotor speed. The experiments were structured to evaluate the feasibility of implementing these bearings in large size turbomachinery. Dynamic test results indicate weak dependency of equivalent direct stiffness coefficients to most test parameters except for frequency and speed, where higher speeds and excitation frequency decreased equivalent bearing stiffness values. The bearing system equivalent direct damping was negatively impacted by increased inlet pressure and excitation frequency, while the cross-coupled force coefficients showed values an order of magnitude lower than the direct coefficients. The experiments also include orbital excitations to simulate unbalance response representative of a target machine while synchronously traversing a critical speed. The results indicate the gas bearing can accommodate vibration levels larger than the set bore clearance while maintaining satisfactory damping levels.


2019 ◽  
Vol 33 (12) ◽  
pp. 12587-12600 ◽  
Author(s):  
Xidong Du ◽  
Min Gu ◽  
Zhenkun Hou ◽  
Zhenjian Liu ◽  
Tengfei Wu

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