Box-type hangar

A hangar and box-type technology, applied in the field of construction engineering, can solve the problems of increasing construction costs, increasing the height of the roof section and large span requirements, and the effect is not obvious, so as to improve the seismic performance, enhance the structural rigidity and stability, reduce the height effect

Pending Publication Date: 2022-07-26
CHINA AVIATION INT CONSTR & INVESTMENT CO LTD
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

In order to obtain the required bending stiffness, it can only be obtained by adding roof members or sections, but the effect is not significant, and the construction cost is greatly increased
[0004] Therefore, the hangar of the prior art has the technical problem of being unable to meet the large-span requirement by increasing the section height of the roof due to the height limit

Method used

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  • Box-type hangar
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Embodiment Construction

[0038] The technical solutions of the present application will be described in detail below with reference to the accompanying drawings and in conjunction with the embodiments.

[0039] The present application provides a hangar, wherein the hangar includes a roof structure 10 and a support structure 20, and the roof structure 10 is rigidly connected to the support structure 20 as a whole, so that the roof structure 10 is connected to the support structure 20. The structure 20 forms a folded plate, and the support structure 20 supports both sides of the roof structure 10 in the length direction and one side of the roof structure 10 in the width direction, so that the hangar forms a box-type structure.

[0040] The roof structure 10 is just connected to the support structure 20, so that the roof structure 10 and the support structure 20 form a folded plate, so that the support structure 20 can be used to effectively reduce the internal force peak of the roof structure and reduce ...

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Abstract

The invention discloses a box type hangar which comprises a roof structure (10) and a supporting structure (20), and the roof structure (10) is integrally and rigidly connected to the supporting structure (20) so that the roof structure (10) and the supporting structure (20) can form a folded plate. The supporting structure (20) supports the two sides, in the length direction, of the roof structure (10) and the side, in the width direction, of the roof structure (10) so that the hangar can form a box-shaped structure. The roof structure is rigidly connected to the supporting structure, so that the roof structure and the supporting structure form a folded plate, the internal force peak value of the roof structure can be effectively reduced through the supporting structure, the structural height of the roof structure is reduced, the limitation of airspace height limitation on the height of a large-span roof structure is broken through, the structural rigidity and stability of a hangar are enhanced, and the anti-seismic property is improved.

Description

technical field [0001] The present application relates to the field of construction engineering, and more particularly, to a box-type hangar. Background technique [0002] The hangar is a structure with three sides enclosed and one side open, and the stress characteristic of the hangar roof is three-sided support, which makes the design of large-span roof a key and difficult point in hangar design. In the prior art, such as Figure 1 to Figure 5 As shown, the roof is in the form of a combination of a mesh frame W and a truss T, wherein the mesh frame W is the main body and a truss T is set on the open side of the hangar of the main body. The whole roof is hinged to the support column S through the support P, so that the roof The overall performance is that the simply supported plate is bent, the bending moment is large at the mid-span, the bending moment at the supporting side is small, and the internal force distribution is extremely uneven. [0003] Moreover, since the fl...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): E04H6/44E04B1/19E04B7/10E04B1/342E04B1/98E04H9/02
CPCE04H6/44E04B1/19E04B7/107E04B1/342E04B1/98E04H9/021
Inventor 赵伯友郭鹏韩奇昊
Owner CHINA AVIATION INT CONSTR & INVESTMENT CO LTD
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