Large tank hanging static testing device

A static test and suspension technology, applied in the direction of measuring devices, machine/structural component testing, instruments, etc., can solve the problem of increased test installation height

Inactive Publication Date: 2015-12-30
BEIJING INST OF STRUCTURE & ENVIRONMENT ENG +1
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

The test structure required by this project is a multi-section joint assembly, and the test installation height will naturally increase a lot; in order to make the local area of ​​the primary oxygen box 3 close to the front bundle 4 be in a low temperature environment, the test piece must be properly At the same time, the upper end of the test boundary is required to be fixed; the application point of the concentrated force load of the bundled support 5 is relatively close to the test piece, and the single point load can reach 300 tons; plus the section axial compression load of the front short shell 7 of the first-level hydrogen tank , the axial load that needs to be balanced by the test installation frame exceeds 1240 tons; at the same time, considering the size limit of the test platform of the test site and the difficulty of the site conditions such as the small tonnage of the bearing points of the foundation, these all bring great challenges to the design of the test scheme and the process of test implementation

Method used

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Embodiment Construction

[0021] Hereinafter, the present invention will be further described in conjunction with the accompanying drawings and specific embodiments.

[0022] Such as figure 2 As shown, the large-scale storage tank suspension type static test device of the present invention comprises: afterburner cap 9, upright post 10, steel frame 11, pull rod 13, connecting nut 16, test platform 25, ground bearing point 26, force Loading equipment 27, load-bearing ground rail 28, and foundation 29; wherein, the outer diameter of the test platform 25 is 5600 mm, and 32 load-bearing points 26 of 50 tons are evenly distributed around the test platform 25 at a position of 6800 mm. First, 8 groups of 16-meter-high upright columns 10 are evenly distributed in the four quadrants of the test platform 25 . There are 32 cantilevers evenly distributed on the periphery of the afterburner cap 9, and there are through holes with a diameter of Φ74 on each cantilever. The diameter of the distribution circle of thes...

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Abstract

The present invention relates to a large tank hanging static testing device which comprises a strengthening cap (9), upright columns (10), a steel frame (11), pull rods (13), a test platform (25), ground force bearing points (26), force loading equipment (27), force bearing ground rails (28), and a foundation (29). Multiple cantilevers are uniformly distributed in a radial way at the hanging part at the top end of the testing device and the periphery of the strengthening cap (9). Each of the cantilevers is provided with a through hole, and the force bearing points (26) around the test platform (25) and the through holes in the strengthening cap (9) cantilevers are orderly connected by multiple groups of pull rods (13). A test piece is fixedly connected to the strengthening cap (9) through the static force loading equipment steel frame (11) and is suspended in a cylindrical space with the strengthening cap (9) as the ceiling and the upright columns (10) as support walls. By using the large tank hanging static testing device, chip level front bonding low temperature combined static test of a model is smoothly completed, and a solid test technology reserve is made for the implementation and development of the low temperature static test of follow-up models.

Description

technical field [0001] The invention relates to structural static test technology, in particular to a suspension type static test device for a large storage tank. technical background [0002] With the continuous progress and development of aerospace science and technology, it is an inevitable trend in the development of rockets in the world that major scientific and technological countries develop large-scale and even heavy-duty launch vehicles. Low-temperature fuel is the propulsion energy of contemporary advanced spacecraft, and these fuels are contained in pressurized storage tanks , while the storage tank is subjected to loads such as axial pressure, bending moment, shear force, internal pressure and temperature during production, storage, hoisting, parking, transportation and flight, so the structural strength, stiffness and low temperature comprehensiveness of the storage tank during use Performance is very important to design and manufacturing, and needs to be verifi...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): G01M99/00
Inventor 杨蓉吴兵白鹭杜珺倪径达王鸿博刘砚涛陈昊毛丽娜刘彦毛郭冰顾海贝尹伟王斐然郑斌张凯徐国梁张辉朱玉强龚淑英江雅婷丁文淇王莉敏
Owner BEIJING INST OF STRUCTURE & ENVIRONMENT ENG
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