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A technology of load simulator and servo mechanism, which is applied in simulators, simulation devices and instruments of space navigation conditions, etc., can solve the problems of inaccurate simulated loads and large vibrations.
Inactive Publication Date: 2015-05-27
BEIHANG UNIV
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[0004] 1. Purpose: The purpose of the present invention is to provide a servomechanism load simulator, which is a brand-new servomechanism load simulator, with a symmetrical inertia disc structure, which solves the problem of large vibrations, severe To solve the problem of inaccurate load simulation, the elastic moment and frictional moment of the device are loaded in parallel, and the two moments can be loaded and measured independently
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[0077] See figure 1 , figure 2 , a servomechanism load simulator of the present invention, it is to do the ground load loading test to the servomechanism of rocket tail nozzle. The composition of the servo mechanism load simulator specifically includes:
[0078] One base 1, two side vertical plates 2, two elastic moment spring plate clamping plates 3, one elastic moment loading support 4, one elastic moment spring plate 5, one swing fork 6, one elastic moment rotating shaft 7, one Elastic moment sensor 8, two ball bearings 9, 12, a bearing cover 10, a bearing seat 11, a friction shaft 13, a small oil cylinder mounting seat 14, four friction torque loading small oil cylinders 15, four friction plates 16, A friction torque sensor 17, a mounting base 18, two roller bearings 19, a main shaft 20, an inertia base plate 21, an inertia counterweight plate 22, two spherical roller bearings 23, an upper lug 24, a A support spring plate cover plate 25, a support spring plate base 26,...
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Abstract
A servo mechanism load simulator comprises a base, side upright plates, elastic moment spring plate clamping boards, an elastic moment loading support, an elastic moment spring plate, a swing shifting fork, an elastic moment rotary shaft, an elastic moment sensor, ball bearings, a bearing cap, a bearing seat, a friction shaft, a small oil cylinder seat, friction moment loading small oil cylinders, friction sheets, a friction moment sensor, an installation seat, roller bearings, a main shaft, an inertia basic disc, an inertia balance weight disc, self-aligning roller bearings, an upper supporting lug, a supporting spring plate cover plate, a supporting spring plate base, a supporting spring plate, a lower supporting lug, a guide bar and a servo mechanism to be measured. According to the servo mechanism load simulator, the structural characteristics, comprising the inertia load, the elastic moment load, the friction moment load and the supporting rigidity, of a rocket engine tail nozzle can be simulated; the elastic moment and the friction moment can be respectively measured through a torque sensor. The servo mechanism load simulator has the advantages of being simple and compact in structure and capable of enabling the structural characteristics of the actual rocket tail nozzle to well reappear.
Description
technical field [0001] The invention relates to a servomechanism load simulator, which is used for simulating the mechanical characteristics of the mechanical structure of a rocket tail nozzle. The device can realize the loading of moment of inertia, loading of elastic moment, support stiffness, loading of friction moment, and continuous adjustment of the above moments within a certain range to meet the needs of different moment loading. At the same time, the friction moment and elastic moment can also be Real-time measurement is carried out respectively through torque sensors, belonging to the technical field of mechanical system test facilities. Background technique [0002] The servomechanism load simulator is a device used to simulate the structural characteristics of the rocket tail nozzle in the ground laboratory environment. With the development of science and technology, the requirements for the large carrying capacity, maneuverability and control precision of the r...
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