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A Static Loading Method for Large Curvature Radome

A radome, static load technology, applied in the direction of applying stable tension/pressure to test the strength of materials, instruments, measuring devices, etc., can solve the problem that the radome cannot apply uniform large loads

Active Publication Date: 2020-04-07
THE RES INST FOR SPECIAL STRUCTURES OF AERONAUTICAL COMPOSITE AVIC
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0005] The technical problem to be solved by the present invention is to overcome the problem that a large curvature radome with a small size area cannot apply a uniform large load

Method used

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  • A Static Loading Method for Large Curvature Radome

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Embodiment Construction

[0012] The static load loading method of the large-curvature radome of the present invention adopts a loading airbag 1 and a loading chamber 3, and the method also adopts a loading sandbag 2, a radome 7 is placed in the loading chamber 3, and a radome is placed on the radome. Place the loading sandbag 2 in the area near the large curvature of 7, cover the loading airbag 1 above the radome 7, and load the radome 7 by inflating the loading airbag 1.

[0013] The air source 4 inflates the loading airbag 1 through the valve 6, and the pressure is measured through the air gauge 5.

[0014] The loading airbag 1 and the loading sandbag 2 are made according to the size of the loading chamber 3, the shape of the radome 7 and the size of the test load.

[0015] The number of the sandbags 2 is one or more.

[0016] Adopt the process of the method of the present invention to carry out test, comprise the following contents:

[0017] First, according to the size of the loading cavity, the...

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Abstract

The invention belongs to the field of mechanical tests on radar domes, particularly relates to a static load application method for a large-curvature radar dome, and solves the problem on loading of ahigh-load static test of a radar dome having a small-size region. For such a phenomenon that the radar dome is partially layered by extremely high partial stress of the radar dome, which is easily caused when a high load is applied to the large-curvature radar dome having the small-size region by using a canvas belt and an operator type wood block, a test result is too harsh. According to the static load application method for the large-curvature radar dome, a loading air bag and a loading cavity are adopted, and a loading sand bag is further adopted. The radar dome is placed in the loading cavity; the loading sand bag is placed in a region near to the large-curvature position of the radar dome; the loading air bag covers the radar dome; the loading air bag is inflated to load the radar dome. Therefore, the radar dome can be uniformly and fully loaded, and the efficiency of the static test can be improved.

Description

technical field [0001] The invention belongs to the mechanical test field of radar radome, in particular to a static load loading method of a large curvature radome, which solves the problem of large-load static test loading of a radome with a small size area. Background technique [0002] Static test is a technical key to the design of radome. The technical agreements of various types of radome have put forward requirements for the static test of radome. [0003] At present, the load loading methods of each static test mainly use the loading canvas belt to apply the tensile load, use the symbol-shaped wooden blocks to apply the compressive load, and use the loading airbag to apply the load. For the large curvature radome with a small size area, the canvas The large load applied by the belt and symbol-shaped wooden blocks will easily lead to excessive local stress of the radome and local delamination of the radome, and the test results are too harsh. [0004] At the same ti...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): G01N3/12G01N3/02
CPCG01N3/02G01N3/12
Inventor 曲秀晓
Owner THE RES INST FOR SPECIAL STRUCTURES OF AERONAUTICAL COMPOSITE AVIC
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