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Air hydraulic shock absorber

Air hydraulic shock absorber
IPC classes for russian patent Air hydraulic shock absorber (RU 2261381):
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FIELD: air hydraulic shock absorbers of chassis of transport facilities.

SUBSTANCE: the air hydraulic shock absorber consists of a cylinder, rod, plunger, movable and fixed axle boxes, hydraulic seals, gas and hydraulic chambers and a profiled needle. The shock absorber is equipped with an optimizing hydraulic double-stage regulator consisting of an internal bush with holes that is attached to the wall separating two spaces in the hydraulic chamber and linked with the plunger of the air hydraulic shock absorber fitted onto which is an external bush with holes with possibility of movement relative to the internal bush. Both bushes are interconnected by a multistart thread with a helix angle exceeding the friction angle, they are also connected by a flexible component. The profiled needle connected to the rod of the air hydraulic shock absorber enters the hole in the external bush of the optimizing hydraulic hydraulic double-stage regulator.

EFFECT: simplified design, provided stability of the dynamic characteristics at direct and reverse motions.

3 dwg, 1 tbl

 

The invention relates to a pneumatic struts chassis vehicles, in particular boarding devices airplanes and helicopters.

Known pneumatic shock absorbers are the cylinder, the plunger, the plunger with the piston, the gas and the hydraulic chamber, the movable and stationary axle boxes with hydraulic seals, openings for flow of fluid, the profiled needle (PI), the valve-reverse, anti-g ground valve (ha) forward stroke, aneroid devices, relief valves (see, for example, A.S. No. 473642 from 19.07.73, patent RU 2043946 from 12.08.92, patent SU 1190112 from 21.11.83, patent RU 2020320 from 29.12.90). The disadvantages of these absorbers are the design complexity and the inability to provide a wide range of viscosities (or temperature) of the fluid in the shock absorber at the same time the stability of such dynamic characteristics as the maximum axial load on the shock absorber and the total direct and reverse. This is due to the fact that the strong temperature decreases the viscosity of the liquid increases many times, at low temperatures (-50 -60...° (C) significantly increases the power of the hydraulic resistance inside the absorber and significantly change the dynamic characteristics of the shock absorber, which causes, firstly, the occurrence of unacceptably large dinamicas the x loads on the structure and secondly, leads to a large change of the total time backward and forward movement of the shock absorber. The change (decrease) the viscosity of the liquid can also occur due to foaming of the liquid during several successive cycles of compression-wound shock absorber, which leads to a change in the characteristics of the shock absorber.

As a prototype of the selected elastic damper (see patent RU 2156899 priority from 01.07.99), having a housing, a gas and a liquid chamber, a plunger shaped spindle, a floating piston diaphragm with holes, non-return valve. The disadvantages of this damper are the complexity of the design and the fact that it does not provide a wide range of viscosities of liquid in the absorber at the same time the stability of the dynamic characteristics in forward and reverse course.

To address these shortcomings, we offer pneumatic shock absorber (shock absorber) is equipped optimizing hydraulic double-acting regulator (GRD), installed in the hydraulic chamber.

Figure 1 is a schematic diagram of the proposed absorber, figure 2 is a longitudinal section of optimizing the hydraulic control double-acting, and figure 3 - cut sleeves GRD in its three operating positions. The absorber consists of a cylinder 1, a piston 2, piston 3, the concentration in the OI pan 4, fixed axle box 5, gas 6 and 7 hydraulic chambers of hydraulic seals 8, profiled needle 9 and optimizing hydraulic double-acting regulator (GND) 18 consisting of the inner sleeve 10 with holes 11, fixedly mounted on the wall 16 of the plunger 3, the separating cavity "b" and "B" in the hydraulic chamber. The sleeve 10 in running landing to rotate around and move along its axis wearing outer sleeve 12 with openings 14. Sleeve 10 and 12 are connected in multiple threads 13 with angle turns more friction angle, the orifices 11 of the sleeve 10 relative to the side of the hole 14 of the sleeve 12 is shifted counterclockwise by angle α1and regarding the other part of the holes 14 clockwise angle α2. The ends of the sleeves 10 and 12 are connected in multiple by a spring 15. Holes 11 of the sleeve 10 and the holes 14 of the sleeve 12 have different cross sections and location around the circumference and along the axis of the sleeves. Square holes are designed so that when the mutual rotation and axial movement of the sleeves 10 and 12 matching holes 11 and 14 for fluid in forward and reverse motion of the shock absorber corresponds to two different laws, changes in the area of through-holes for fluid from the magnitude and direction of the angle of rotation and axial movement of the sleeve 12. The needle 9 is fixed on the shaft 2 and is GNC the ri holes 17 of the sleeve 12 with a gap.

The operation of the shock absorber is as follows.

The first mode is a direct stroke of the shock absorber. During compression (contraction) of the shock absorber when the reciprocal movement along the axis of the shock absorber of the needle 9 and the sleeve 12 changing the area of the through-holes for fluid between the needle 9 and the wall of the bore 17 depending on the progress of the shock absorber. Certain pre dependence of the square of these through-holes allows regulation of hydraulic forces depending on the progress of the shock absorber. When the compression of the shock absorber due to the resistance flowing through the openings 11 and 14 of the liquid there is a pressure difference P1(in the cavity "B") and R2(in the cavity "B") hydraulic chamber. At pressure P1more pressure P2creates a force along the axis of the sleeve 12. The result of this force on the threaded connection 13 of the sleeves 10 and 12 produces a torque that rotates the sleeve 12, for example, clockwise. The specified torque is balanced by the torque from the spring 15. Holes 14 are partially align with the holes 11 and the fluid from the cavity "B" flows into the cavity "B". This changes the size of through-holes for flow of fluid when changing differential pressures in cavities "a" and "B". Certain pre-dependency matching square hole from the corner turning parts, all specifications is a and the axial movement of the sleeve 12 allows the regulation of the hydraulic force depending on the pressure drop in the hydraulic chamber.

The second mode is the reverse stroke of the shock absorber. This mode is resgate (increase in length) of the shock absorber. At pressure P1less pressure P2there is a force directed along the axis of the sleeves 10 and 12 down. This leads to rotation of the sleeve 12 in the opposite (unlike the forward stroke of the shock absorber) direction, such as counterclockwise. The holes 14 of the sleeve 12 "open up" holes 11 of the sleeve 10 and the fluid flows from the cavity "B" cavity "In". While acting on the sleeve 12 power changes in accordance with the pressure difference P1and R2and provides the necessary area of the through-holes for fluid on the back of the course to ensure optimal values of total time of direct and reverse t∑ in a wide range of viscosities of liquid in the absorber.

You can change the square holes for flow of fluid from the stroke of the shock absorber with a needle and changes in the area of the extra holes from the pressure drop in the hydraulic chamber using HRD provides the necessary optimal change of the total area of throttling holes on both the direct and reverse motion of the shock absorber. This allows you greatly reduce the effect of viscosity of the fluid in the shock absorber on the dynamic characteristics of the damper.

The result p is obedennyh numerical studies of the landing aircraft impact, having telescopic rack chassis with different absorbers obtained comparative results of the calculation (see table) for the landing gear with shock absorbers that have: (a) permanent openings for fluid (Const); b) a profiled needle (PI); C) ground valve (ha) and d) optimizing the hydraulic double-acting regulator (GRD). The results correspond to temperatures of +60°C, +20°and -60°and With different values of the viscosity of the fluid in the hydraulic chamber and the charging pressure in the gas chamber. As can be seen from the table, the proposed design provides the greatest stability of such important characteristics of the shock absorber, as the maximum bearing load Rumaxand the total direct and reverse t∑. The change in the value Rumaxwhen the temperature changes from +60°C to -60°is only 0.88% unlike other options the design of the absorber (9.54, 23.27 and 29.12%).

A pneumatic shock absorber comprising a cylinder, a piston, plunger, movable and immovable Buchs, hydraulic seals, gas and hydraulic chambers, the profiled needle, characterized in that it includes optimizing hydraulic double-acting regulator, consisting of inner sleeve with holes, which natvig what about mounted on the wall, separating the two cavities in the hydraulic chamber and connected with the plunger of a pneumatic-hydraulic shock absorber connected to the cylinder pneumatic-hydraulic shock absorber, which is dressed with the ability to move relative to the inner sleeve outer sleeve with holes, and both sleeves are interconnected multiple threads with the angle of gradient coils more friction angle and they are connected also by the elastic element and the profiled needle, connected with the rod pneumatic-hydraulic shock absorber, enters the hole in the outer sleeve optimizing the hydraulic control double-acting.

 

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