公路工程
公路工程
공로공정
JOURNAL OF HIGHWAY ENGINEERING
2014年
2期
49-53
,共5页
桥梁工程%抗风性能%风洞试验%颤振%涡激共振%气动措施
橋樑工程%抗風性能%風洞試驗%顫振%渦激共振%氣動措施
교량공정%항풍성능%풍동시험%전진%와격공진%기동조시
bridge engineering%wind-resistant performance%wind tunnel test%flutter%vortex-in-duced vibration%aerodynamic mitigation measure
采用节段模型风洞试验的方法对某峡谷底斜拉桥---西藏迫龙沟斜拉桥的抗风性能进行了改善研究。首先,借助于地形风洞试验结果获得了桥位处风攻角和风偏角大小,并确定了大桥颤振检验风速和颤振试验的风攻角范围;然后,考察了大桥原方案的颤振稳定性并通过气动措施改善了原方案的颤振性能;最后检验了施加气动措施前后大桥涡激共振特性。研究结果表明:峡谷底大跨度桥梁的设计基准高度可参照桥面高度确定,但有必要进行地形试验确定桥位处风攻角和风偏角的实际情况;迫龙沟大桥颤振稳定性出现了±3°和0°风攻角下满足要求而5°风攻角下不满足要求的现象,因此峡谷底大跨度桥梁颤振稳定性检验只进行《规范》建议的风攻角试验可能存在安全隐患;颤振性能改善措施选取时,应考虑斜风的不利影响,确保大桥有足够的颤振稳定性安全储备。
採用節段模型風洞試驗的方法對某峽穀底斜拉橋---西藏迫龍溝斜拉橋的抗風性能進行瞭改善研究。首先,藉助于地形風洞試驗結果穫得瞭橋位處風攻角和風偏角大小,併確定瞭大橋顫振檢驗風速和顫振試驗的風攻角範圍;然後,攷察瞭大橋原方案的顫振穩定性併通過氣動措施改善瞭原方案的顫振性能;最後檢驗瞭施加氣動措施前後大橋渦激共振特性。研究結果錶明:峽穀底大跨度橋樑的設計基準高度可參照橋麵高度確定,但有必要進行地形試驗確定橋位處風攻角和風偏角的實際情況;迫龍溝大橋顫振穩定性齣現瞭±3°和0°風攻角下滿足要求而5°風攻角下不滿足要求的現象,因此峽穀底大跨度橋樑顫振穩定性檢驗隻進行《規範》建議的風攻角試驗可能存在安全隱患;顫振性能改善措施選取時,應攷慮斜風的不利影響,確保大橋有足夠的顫振穩定性安全儲備。
채용절단모형풍동시험적방법대모협곡저사랍교---서장박룡구사랍교적항풍성능진행료개선연구。수선,차조우지형풍동시험결과획득료교위처풍공각화풍편각대소,병학정료대교전진검험풍속화전진시험적풍공각범위;연후,고찰료대교원방안적전진은정성병통과기동조시개선료원방안적전진성능;최후검험료시가기동조시전후대교와격공진특성。연구결과표명:협곡저대과도교량적설계기준고도가삼조교면고도학정,단유필요진행지형시험학정교위처풍공각화풍편각적실제정황;박룡구대교전진은정성출현료±3°화0°풍공각하만족요구이5°풍공각하불만족요구적현상,인차협곡저대과도교량전진은정성검험지진행《규범》건의적풍공각시험가능존재안전은환;전진성능개선조시선취시,응고필사풍적불리영향,학보대교유족구적전진은정성안전저비。
The wind-resistant performance of a cable-stayed bridge at the bottom of a canyon,Po-long canyon bridge in Tibet,was been improved via the sectional model wind tunnel test.Firstly,the flutter checking wind speed and the range of wind attack angles were confirmed on the basis of the topo-graphic experiment results.Then,the flutter stability was investigated by the wind tunnel test and im-proved by setting aerodynamic mitigation measures.Finally,the vortex-induced vibration performance of the girder before/after setting wind fair was checked by the sectional model wind tunnel test.The results show that,for the bridge at the bottom of the canyon,the design standard height can be calculated refer-ring to the elevation of the bridge deck but the wind attack and yaw angle should be measured by the top-ographic experiment.If the flutter stability is only checked under the attack angle range suggested by the specification,there may be some potential safety hazard,because it is possible that the flutter stability does not satisfy under the larger wind attack angle.The adverse effect of yaw wind should be taken into account for the choice of aerodynamic mitigation measures,and there should be enough security capacity for the flutter stability.