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Structural form of core beam of main beam of full-bridge aeroelastic model for long-span double-box girder

An aeroelastic, structural form of technology, used in aerodynamic testing, testing of machine/structural components, measuring devices, etc., can solve the problems of small lateral size, unusable, distorted test results, etc., to reduce the overall stiffness, Easy-to-process, simple-structured effects

Pending Publication Date: 2019-03-29
SOUTHWEST JIAOTONG UNIV
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

According to the existing processing methods and the requirements for the core beam, the transverse bridge stiffness is often far greater than the design value of the model, which cannot meet similar requirements
If the theoretical design requirements are compulsively met, the thickness of the core beam in the transverse bridge direction must be less than 1 mm. This has two problems: (1) The core beam itself is warped and unstable in the transverse direction due to the small transverse dimension of a single core beam, making it unusable; (2) The existing processing methods are difficult and cannot be connected with the external mold
Based on the above reasons, the lateral stiffness of the aeroelastic model of double box girder has always been a difficult problem, which cannot meet the needs of actual operation at all, and is often ignored, resulting in distortion of test results

Method used

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  • Structural form of core beam of main beam of full-bridge aeroelastic model for long-span double-box girder
  • Structural form of core beam of main beam of full-bridge aeroelastic model for long-span double-box girder

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Embodiment Construction

[0010] The specific embodiment of the present invention will be further described below in conjunction with the accompanying drawings. The interpretation of each label in the figure is: beam section outer mold 1, secondary core beam 2, right-angle groove 3, transverse connecting beam 4, main core beam 5, double box Beam outer mold 6, core beam 7.

[0011] The present invention includes a double box girder outer formwork 6 and a core beam 7 .

[0012] The double box girder external formwork 6 includes a left box girder external formwork and a right box girder external formwork with the same structure, and the left box girder external formwork and the right box girder external formwork are arranged parallel to each other and symmetrically. Both the left box girder external form and the right box girder external form include a plurality of beam section external forms 1 arranged at intervals along the bridge direction, and the corresponding beam section external forms 1 of the lef...

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Abstract

The invention discloses a structural form of a core beam of a main beam of a full-bridge aeroelastic model of a long-span double box girder, including outer molds of the double-box girder and core beams. The outer molds of the double-box girder include an outer mold of a left-box girder and an outer mold of a right-box girder. Each outer mold of the left-box girder and the right-box girder includes a plurality of spaced section outer molds arranged along the bridge. The core beams include main core beams disposed along the bridge and secondary core beams disposed along the transverse directionof the bridge. The main core beam and the secondary core beam are integrated structures. The main core beam is respectively arranged in the outer mold of the left-box girder and the right -box girder, and the main core beams run through all the section outer molds along the bridge. Each middle portion of the main core beams protrudes inwardly to form a right angle groove, which is corresponding to each section outer mold. The section outer molds corresponding to each outer mold of the left-box girder and the right -box girder are connected through one of the secondary core beams. According tothe structural form of the core beam of the main beam of the full-bridge aeroelastic model for the long-span double-box girder, the structural form of the core beam of the main beam of the full-bridge aeroelastic model is changed, and the pull-pressing rigidity of the single core beam of the double core beam is converted into the bending stiffness of the core beam, thereby greatly reducing the total stiffness of the main beam of the full-bridge aeroelastic model along the bridge.

Description

technical field [0001] The invention relates to the technical field of bridge engineering wind tunnel tests, in particular to a main girder core girder structure form of a large-span double box girder full bridge aeroelastic model. Background technique [0002] The wind tunnel test of the aeroelastic model of the long-span bridge is an important test method to ensure the safety of the bridge against wind. According to the requirements of the similarity ratio of the scaled-down experiment, the vertical stiffness, lateral stiffness and torsional stiffness of the bridge girder model must meet the similarity requirements. In order to meet the above stiffness requirements, the general bridge model is simulated by a metal core beam, such as a steel core beam. For the single-box girder, the single-core beam simulation is generally used, and very good results have been achieved; for the double-box girder, the simulation method of the single-box girder is generally used for referenc...

Claims

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Application Information

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IPC IPC(8): G01M9/08
CPCG01M9/08
Inventor 马存明靖洪淼廖海黎孙延国张天翼
Owner SOUTHWEST JIAOTONG UNIV