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Aircraft undercarriage shock-absorber leg

Aircraft undercarriage shock-absorber leg
IPC classes for russian patent Aircraft undercarriage shock-absorber leg (RU 2247679):
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Aircraft undercarriage shock-absorber leg Aircraft undercarriage shock-absorber leg / 2247679
Proposed shock-absorber leg includes cylinder, rod, piston, support and working member in form of system of rods made from monocrystals compressed to solid state between piston and support; generatrix of its surface corresponds to curve of diagram of operation of hydro-pneumatic shock absorber.

FIELD: aircraft manufacture; manufacture of landing gears.

SUBSTANCE: proposed shock-absorber leg includes cylinder, rod, piston, support and working member in form of system of rods made from monocrystals compressed to solid state between piston and support; generatrix of its surface corresponds to curve of diagram of operation of hydro-pneumatic shock absorber.

EFFECT: simplified construction.

3 dwg

 

The invention relates to the field of aircraft construction, in particular for a landing devices used to absorb and dissipate the energy of the aircraft upon landing.

Known constructions of landing devices represent a set of elements transmitting and absorbing the impact energy of the tires on the surface of the runway[1], [2].

The disadvantage of these designs is the high complexity. Above mentioned disadvantages can be eliminated by replacing the working fluid of the shock absorber landing gear. Of such devices is the closest to the technical essence and the results achieved by this invention is a hydro-pneumatic chamber of the shock absorber landing gear of the aircraft [1]. The design contains a cylinder, a piston rod, the piston and the working body.

The disadvantage of this design is the high complexity.

The invention is aimed at simplifying the design.

To achieve this, the working body is made in the form of systems of monocrystalline rods, benevolence between the piston and the bearing, forming a surface which corresponds to the curve diagrams of a hydropneumatic shock absorber.

The invention is illustrated by drawings, where figure 1 shows a shock absorber, General view; figure 2 is a graph of voltage as a function of temperature when the restoration of the Fort is s single crystals; on the figure 3 - chart of pseudoprophete single crystals.

The shock absorber includes a cylinder 1 within which are located the terminals of the single crystal 2, a piston 3 connected with the rod 4, the support 5, the unit heating and cooling 6.

The shock absorber works as follows.

At the moment of touch chassis ground terminals of the first level, heated by the electric-contact way up to the maximum design temperature, cooled also contact way, returning to its original state, taking the maximum load and reducing it by the amount pseudoproxy deformation of these rods. In the next moment of time involved in the work of the rods of the second level, which act similarly, and so on until complete absorption of the energy.

This construction of the shock absorber simpler.

Sources of information

1. Copyright certificate №1527815 published 20.10.95. Bulletin No. 29 (prototype).

2. Copyright certificate №2051073 published 27.12.95. Bulletin # 36.

The spring strut of the chassis, consisting of a cylinder, rod, piston, bearings and the working fluid, wherein the working fluid is made in the form of rods of single crystals, benevolence between the piston and the bearing, forming a surface which corresponds to the curve diagrams of a hydropneumatic shock absorber.

 

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