Gas-liquid two-phase composite static pressure support structure
A technology of static pressure support and air intake structure, applied in bearings, shafts and bearings, mechanical equipment, etc., can solve the problems of poor rigidity, low viscosity of compressed air, high viscosity of hydraulic oil, etc., and achieve low friction, low heat generation, and incompressibility good sex effect
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Embodiment 1
[0051] Such as Figure 1 to Figure 4 As shown, the slider 1 and the pad 2 are used, and a small gap h0 is set between the two. When in use, the compressed air from the air source 4 flows into the air inlet 1-1 through the throttle 3, and the hydraulic oil from the oil source 6 flows into the oil inlet 2-1 through the throttle 5. Compressed air and hydraulic oil form a gas-liquid two-phase composite film at the oil cavity 2-2 and the oil sealing surface 2-3.
[0052] During this period, the thickness h1 of the air film in the composite film at the oil sealing surface 2-3 can be controlled by adjusting the air resistance of the restrictor 3 and the liquid resistance of the restrictor 5 . During general adjustment, it is necessary to ensure that the gas film thickness h1 is much smaller than the oil film thickness h2, so as to obtain high rigidity and low friction of the composite film. combine as Figure 4 It shows a schematic diagram of the velocity gradient distribution in ...
Embodiment 2
[0057] This embodiment describes the situation when the gas-liquid two-phase composite static pressure support structure is applied to the static pressure radial bearing.
[0058] Such as Figure 5 to Figure 7 As shown, after adopting the configuration of the present invention, the bearing bush 7 and the mandrel 8 may be included. A slight gap is provided between the two. Simultaneously, the bearing bush 7 is provided with some oil inlet holes 7-1, the oil cavity 7-2, the oil sealing surface 7-3, and the mandrel 8 is provided with some air inlet holes 8-1, and the journal surface 8-2.
[0059]Each oil inlet hole 7-1 is provided with a restrictor and an oil source similar to those in the first embodiment. Each air inlet 8-1 is provided with a restrictor and an air source similar to those in the first embodiment. Moreover, the adjustment of the air film thickness is substantially smaller than the micro gap, and the principle of air film thickness adjustment is the same as tha...
Embodiment 3
[0062] This embodiment describes the situation when the gas-liquid two-phase composite static pressure support structure is applied to a static pressure thrust bearing.
[0063] Such as Figure 8-10 As shown, it includes a thrust plate 9 and a bearing bush 10 . Similarly, a small gap is provided between the two, and an air inlet 9-1 and a thrust surface 9-2 are arranged on the thrust disc 9 . The bearing bush 10 is provided with an oil inlet hole 10-1, an oil chamber 10-2, an oil sealing surface 10-3, and an oil return groove 10-4.
[0064] During use, each air inlet 9-1 is provided with a restrictor similar to that in the first embodiment. Moreover, a restrictor similar to that in Embodiment 1 is provided at the oil inlet hole 10-1. The air film thickness is adjusted to be substantially smaller than the tiny gap, and the principle of air film thickness adjustment is the same as that in Embodiment 1, which will not be repeated here.
[0065] In actual implementation, when ...
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