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Test loading device of airplane joystick type control system

A control system and loading device technology, which is applied in the testing of measuring devices, machine/structural components, and the use of repetitive force/pulse force to test the strength of materials, etc. Small and other problems to achieve the effect of large practical application value

Inactive Publication Date: 2012-07-25
CHINA AIRPLANT STRENGTH RES INST
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

Moreover, the previous manipulation system tests generally used force as the control quantity, and the displacement of the joystick was very small, so it was difficult to truly simulate the actual use of the joystick.

Method used

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  • Test loading device of airplane joystick type control system
  • Test loading device of airplane joystick type control system
  • Test loading device of airplane joystick type control system

Examples

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Comparison scheme
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Embodiment Construction

[0016] The utility model is described in further detail below by means of specific embodiments:

[0017] Please also see figure 1 with figure 2 ,in, figure 1 It is a structural schematic diagram of the test loading device of the aircraft control system of the utility model, figure 2 is the schematic diagram of its principle. In this embodiment, the test loading device for the control system of the aircraft control rod includes a sliding rail 1 , a sliding surface 2 , a double-action ball 3 , a dummy control rod 4 , a hydraulic cylinder 5 and a frame 6 containing the sliding surface 2 .

[0018] Wherein, the slide rail 1 is a horizontal slide guide rail, including a heading slide rail and a side slide rail, and the heading slide rail and the direction-finding slide rail are arranged on the upper and lower levels, not in the same plane, and the two are connected end to end form a rectangular frame. Please also see image 3 , which is a structural schematic diagram of the...

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Abstract

The invention relates to a loading device, in particular relating to a test loading device of an airplane joystick type control system. The test loading device of the airplane joystick type control system provided by the invention comprises a slide rail, slide surfaces, double acting balls, a false joystick and frames comprising the slide surfaces, wherein the slide rail is a horizontal slide rail and comprises a heading slide rail and a lateral slide rail; the heading slide rail and the lateral slide rail are respectively arranged on upper and lower layers, and the heading slide rail and thelateral slide rail are connected end to end; the slide surfaces are elongated slot slide surfaces which are arranged in the frames; the number of the frames is two, and the two ends of each frame arearranged in the slide rail; and the double acting balls are arranged in the slide surfaces, and the centers of the double acting balls pass through the false joystick. The test loading device provided by the invention can be used for finishing the tests of displacement follow-up loading and composite operation loads, thereby more truly simulating the service condition of a joystick, and having greater actual application value.

Description

technical field [0001] The utility model relates to a loading device, in particular to a test loading device related to an aircraft driving stick type control system. Background technique [0002] Usually, the static and fatigue tests of the aircraft control system are basically a ground strength verification test that is independent of the aircraft body structure and is also very important and directly related to flight safety. [0003] In the past, the control system test was generally a single independent operation test, that is, the respective tests of the steering system of the elevator (or full-motion horizontal tail), aileron, rudder and other control systems. The maneuvering flight of the aircraft (especially fighter jets) reflects that the operation of the control system is often a composite operation. Therefore, a test with both a single operating load and a compound operating load can better reflect the actual operation, and a device is needed to complete this ta...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): G01N3/34G01M99/00
Inventor 薛铁军高治应唐吉运王全红黄太誉李晓宁
Owner CHINA AIRPLANT STRENGTH RES INST
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