CN102134831A - Pneumatic wing plate structure for improving flutter stability of steel truss girder suspension bridge - Google Patents

Pneumatic wing plate structure for improving flutter stability of steel truss girder suspension bridge Download PDF

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Publication number
CN102134831A
CN102134831A CN 201110000731 CN201110000731A CN102134831A CN 102134831 A CN102134831 A CN 102134831A CN 201110000731 CN201110000731 CN 201110000731 CN 201110000731 A CN201110000731 A CN 201110000731A CN 102134831 A CN102134831 A CN 102134831A
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CN
China
Prior art keywords
wing plate
pneumatic
pneumatic wing
suspension bridge
girder suspension
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Pending
Application number
CN 201110000731
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Chinese (zh)
Inventor
彭运动
欧阳先凯
孟凡超
任仁
张勇
周平
纪为祥
门永斌
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
SICHUAN DEYANG CHEMISTRY CO Ltd
SICHUAN TENGZHONG HEAVY INDUSTRY MACHINERY Co Ltd
Original Assignee
SICHUAN DEYANG CHEMISTRY CO Ltd
SICHUAN TENGZHONG HEAVY INDUSTRY MACHINERY Co Ltd
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by SICHUAN DEYANG CHEMISTRY CO Ltd, SICHUAN TENGZHONG HEAVY INDUSTRY MACHINERY Co Ltd filed Critical SICHUAN DEYANG CHEMISTRY CO Ltd
Priority to CN 201110000731 priority Critical patent/CN102134831A/en
Publication of CN102134831A publication Critical patent/CN102134831A/en
Pending legal-status Critical Current

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Abstract

The invention discloses a pneumatic wing plate structure for improving flutter stability of a steel truss girder suspension bridge, which comprises a composite hollow wing plate and a plate-end linking mechanism, wherein the pneumatic wing plate adopts the asymmetrical wing surface structure, and the curvature radius of an upper wing surface of the pneumatic wing plate is larger than that of a lower wing surface; and the pneumatic wing plate structure can be mounted in a multi-layer superposition manner. By adopting the structure way and adopting the asymmetrical pneumatic layout, the pneumatic wing plate has better effect of eliminating flutter and is particularly applicable to large-span steel truss girder suspension bridges.

Description

A kind of pneumatic wing plate structure that is used to improve flutter stability of steel trussed girder suspension bridge
Technical field
The anti-flutter pneumatic wing plate of bridge engineering auxiliary, especially steel trussed girder suspension bridge of the present invention is made the field.
Background technology
Demand along with technological progress and Modern Traffic transportation, build increasing Longspan Bridge and become inexorable trend, the lengthening in bridge span footpath makes structure greatly strengthen the sensitivity of wind, avoid the zitterbewegung of structure generation diversity also therefore to become the problem that to pay close attention in the long-span bridge beam design process, in bridge construction flutter and buffeting solution, pneumatic wing plate is being played the part of very important role.Pneumatic wing plate can increase the resistance coefficient of steel truss girder hardly, and it is simple in structure, the deadweight is very light, installs and checks easy to maintenancely, and economic performance is good.Chinese patent application CN200810226680.3 arranges continuously to full-bridge along vertical bridge in conjunction with central slot, has proposed the scheme as Fig. 1, bridge deck central slot 1 among the figure; Pneumatic wing plate 2; Bridge deck 3; Steel truss 4; Column 5; Longeron 6.Pneumatic wing plate 2 forms an integral body by most section assemblings, and pneumatic wing plate 2 two ends of shaping are for sealing; Each pneumatic wing plate sections length is 1/5 11 times of steel truss girder sections length, and the width of pneumatic wing plate 2 is 1,/30 one 1/10 times of steel truss girder width; Each pneumatic wing plate sections by bolt, rivet or be weldingly fixed on column 5 tops, column 5 lower ends are by bolt or be weldingly fixed on the longeron 6, longeron 6 two ends are by bolt or be weldingly fixed on inside, steel truss 4 both sides.And several schemes of symmetry wing plate have been proposed.
Summary of the invention
The objective of the invention is to develop a kind of pneumatic wing plate structure that is used to improve flutter stability of steel trussed girder suspension bridge, on the basis of existing technology, further optimize aerodynamic arrangement, make pneumatic wing plate have more good flutter and eliminate effect.
The objective of the invention is to realize by following means.
A kind of pneumatic wing plate structure that is used to improve flutter stability of steel trussed girder suspension bridge, form by composite material hollow wing plate and plate end coupling mechanism, pneumatic wing plate adopts asymmetrical airfoil surface configuration, and the radius of curvature of the top airfoil of pneumatic wing plate is greater than the radius of curvature of lower aerofoil; But multilayer build-up is installed.
Adopt make of the present invention, adopt asymmetrical aerodynamic arrangement, can make pneumatic wing plate have more good flutter and eliminate effect, be particularly suitable for the large span steel trussed girder suspension bridge and use.
Description of drawings
Fig. 1 is prior art pneumatic wing plate and bridge deck central slot combined pneumatic control device schematic diagram.
Fig. 2 is the outside drawing of pneumatic wing plate of the present invention.
Fig. 3 is the K-K sectional view of Fig. 2.
Fig. 4 is double-deck pneumatic wing plate arrangement diagram.
The specific embodiment
Below in conjunction with accompanying drawing structure of the present invention is described in further detail.
Can see the pneumatic wing plate structure that is used to improve flutter stability of steel trussed girder suspension bridge by Fig. 2, form by polyphenyl thioether composite material injection moulding wing plate and plate end coupling mechanism, pneumatic wing plate adopts asymmetrical airfoil surface configuration, and the radius of curvature of the top airfoil of pneumatic wing plate is greater than the radius of curvature of lower aerofoil; Last lower aerofoil wing height ratio (h1/h2) is 2-5; But multilayer build-up is installed.
Embodiment 1
Adopt the structure as Fig. 2 and Fig. 3, polyphenyl thioether composite material injection moulding wing plate adopts paraboloidal top airfoil of oval calotte and lower aerofoil, and the radius of curvature of top airfoil is greater than the radius of curvature of lower aerofoil, and top airfoil wing height is 0.2m, and lower aerofoil wing height is 0.04m.
Embodiment 2
Other is with embodiment 1, and top airfoil wing height is 0.1m, and lower aerofoil wing height is 0.05m.
Embodiment 3
Construct double-deck flutter with the pneumatic wing plate of embodiment 1 and eliminate structure, two wing plates all are fixed on the steel truss by column up and down, and the wide B of the wing is 1m, and the distance H of last lower aerofoil is 0.5 m.
Contract than wind tunnel test by the sections model, adopt central slot and pneumatic groups of vanes close the steel trussed girder suspension bridge critical wind speed of flutter of aerodynamic Measures (unit: m/s), data target such as following table:
The angle of attack The asymmetric oval calotte of embodiment 1 individual layer Embodiment 3 double-deck asymmetric oval calottes
-3 degree Greater than 130.6 Greater than 130.6
0 degree Greater than 103.7 Greater than 130.6
3 degree 72.8 76.1
Test shows, when multilayer build-up is installed up and down the ratio of the spacing H of pneumatic wing plate and wing plate width B be controlled at about 0.42 the most suitablely, depart from this ratio, critical wind velocity is lower.Find also in the test that on the pneumatic wing plate surface stagnation of the circulation of vital energy structure is set, as uniform (degree of depth is 2cm) circular arc pit, critical wind speed of flutter has the trend of further raising.

Claims (3)

1. pneumatic wing plate structure that is used to improve flutter stability of steel trussed girder suspension bridge, form by composite material hollow wing plate and plate end coupling mechanism, it is characterized in that pneumatic wing plate adopts asymmetrical airfoil surface configuration, the radius of curvature of the top airfoil of pneumatic wing plate is greater than the radius of curvature of lower aerofoil; But multilayer build-up is installed.
2. described being used to improves the pneumatic wing plate structure of flutter stability of steel trussed girder suspension bridge according to claim 1, it is characterized in that the pneumatic wing plate surface curve is an oval calotte.
3. described being used to improves the pneumatic wing plate structure of flutter stability of steel trussed girder suspension bridge according to claim 1, it is characterized in that the pneumatic wing plate surface is provided with stagnation of the circulation of vital energy structure.
CN 201110000731 2011-01-05 2011-01-05 Pneumatic wing plate structure for improving flutter stability of steel truss girder suspension bridge Pending CN102134831A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN 201110000731 CN102134831A (en) 2011-01-05 2011-01-05 Pneumatic wing plate structure for improving flutter stability of steel truss girder suspension bridge

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN 201110000731 CN102134831A (en) 2011-01-05 2011-01-05 Pneumatic wing plate structure for improving flutter stability of steel truss girder suspension bridge

Publications (1)

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CN102134831A true CN102134831A (en) 2011-07-27

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Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH1171712A (en) * 1997-08-28 1999-03-16 Nkk Corp Cable stayed bridge
CN1875160A (en) * 2003-11-04 2006-12-06 未来概念公司 Pneumatic two-dimensional structure
WO2007089398A2 (en) * 2006-01-27 2007-08-09 Powers James M Bridge assembled from ocean-mobile pontoon modules
CN101135135A (en) * 2006-09-02 2008-03-05 重庆交通大学 Concrete arch-type bridge rigidity variable intelligent damping control system
CN101736687A (en) * 2008-11-19 2010-06-16 中交公路规划设计院有限公司 Pneumatic control device for improving flutter stability of steel trussed girder suspension bridge
CN202012036U (en) * 2011-01-05 2011-10-19 四川腾中重工机械有限公司 Pneumatic wing plate construction for improving flutter stability of steel truss girder suspension bridge

Patent Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH1171712A (en) * 1997-08-28 1999-03-16 Nkk Corp Cable stayed bridge
CN1875160A (en) * 2003-11-04 2006-12-06 未来概念公司 Pneumatic two-dimensional structure
WO2007089398A2 (en) * 2006-01-27 2007-08-09 Powers James M Bridge assembled from ocean-mobile pontoon modules
CN101135135A (en) * 2006-09-02 2008-03-05 重庆交通大学 Concrete arch-type bridge rigidity variable intelligent damping control system
CN101736687A (en) * 2008-11-19 2010-06-16 中交公路规划设计院有限公司 Pneumatic control device for improving flutter stability of steel trussed girder suspension bridge
CN202012036U (en) * 2011-01-05 2011-10-19 四川腾中重工机械有限公司 Pneumatic wing plate construction for improving flutter stability of steel truss girder suspension bridge

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Application publication date: 20110727