【摘要】：高位飛機庫是將常規(guī)飛機機庫適應高填方區(qū)機場地勢情況而延伸出的一種特種結(jié)構(gòu)形式的飛機機庫。通過將機庫層放置于建筑物的第二層或以上位置,從而實現(xiàn)減少土方填筑,降低工程造價,增加建筑有效使用面積,提供土地使用效率,減少環(huán)境破壞具有積極的意義。本文主要研究高位飛機機庫抗側(cè)力體系的布置,及其在地震作用下的響應,通過分析并對比與常規(guī)機庫抗側(cè)力體系布置的差異,從而提出高位飛機機庫抗側(cè)力體系設計的要點及注意內(nèi)容。本文主要內(nèi)容包括:1、研究分析高位飛機機庫建筑特點,分析其受力特性,并對高位飛機機庫的的抗側(cè)力體系布置原則進行探討,提出高位飛機機庫抗側(cè)力構(gòu)件的布置方法及設計特點,并對于與常規(guī)機庫抗側(cè)力體系設置要求進行對比,并提出本文中高位飛機機庫的研究模型。2、對高位飛機機庫的抗側(cè)力體系在多遇地震作用下的彈性分析,主要研究其在多遇地震作用下的結(jié)構(gòu)反應,進行振型分解反應譜分析和振型分解時程分析,并與重力荷載代表值下的靜力分析結(jié)果組合,分析高位飛機機庫在多遇地震作用下的基底剪力分布及各層最大位移等結(jié)構(gòu)反應,分析振型特點。3、對高位飛機機庫在罕遇地震情況下進行彈塑性靜力和動力時程分析。通過分析表明高位飛機庫在罕遇地震作用下機庫及機庫以下層的混凝土結(jié)構(gòu)構(gòu)件已經(jīng)進入彈塑性階段,對結(jié)構(gòu)在罕遇地震作用下的彈塑性時程分析,得到高位飛機機庫在罕遇地震下的基底剪力及柱頂最大位移等結(jié)構(gòu)反應,分析結(jié)構(gòu)的薄弱部位和塑性鉸的出現(xiàn),分布與發(fā)展等方面的情況。4、機庫層地坪飛機荷載較大,結(jié)構(gòu)優(yōu)化設計對于造價影響較大,文中用有限元軟件模擬板、主次梁在實際飛機輪壓下及單位均布荷載作用下產(chǎn)生的最大彎矩,求得不同梁板布置、機型下的高架機庫地坪等效均布活荷載取值,同時得到了主、次梁的均布荷載折減系數(shù),并對這些結(jié)果的適用性進行了分析,給出了使用建議。
[Abstract]:The high plane hangar is a special type of aircraft hangar which adapts the conventional aircraft hangar to the situation of the airport topography in the high filling area. By placing the hangar at the second or higher level of the building, it is of positive significance to reduce the earthwork filling, reduce the engineering cost, increase the effective use area of the building, provide the land use efficiency and reduce the environmental damage. In this paper, the arrangement of anti-lateral force system of high plane hangar and its response under earthquake are studied, and the difference between the arrangement of anti-lateral force system and that of conventional hangar is analyzed and compared. The main points and contents of the design of the anti-lateral force system of the high plane hangar are put forward. The main contents of this paper are as follows: 1. The characteristics of high plane hangar are studied and analyzed, and the principle of anti-lateral force system arrangement of high plane hangar is discussed. This paper puts forward the layout method and design features of the anti-lateral force components of the high plane hangar, and compares the setting requirements of the anti-lateral force system with that of the conventional hangar, and puts forward the research model of the high-position aircraft hangar in this paper. The elastic analysis of the anti-lateral force system of high plane hangar under the action of frequent earthquake is mainly studied, and the structural response under the action of frequent earthquake is studied, and the mode decomposition response spectrum analysis and mode decomposition time history analysis are carried out. Combined with the static analysis results under the representative gravity load, the structural responses of the base shear force distribution and the maximum displacement of each layer of the high plane hangar under the action of frequent earthquakes are analyzed, and the characteristics of the vibration modes are analyzed. The elastoplastic static and dynamic time history analysis of high plane hangar under rare earthquake is carried out. The analysis shows that the concrete structural members of the hangar and the lower layer of the hangar have entered the elastic-plastic stage under the rare earthquake, and the elastic-plastic time history of the structure under the rare earthquake is analyzed. The structural responses such as the base shear force and the maximum displacement of the column top of the high plane hangar under rare earthquakes are obtained, and the appearance, distribution and development of the weak part of the structure and the plastic hinge are analyzed. The optimum design of the structure has a great influence on the cost. In this paper, the maximum bending moment of the primary and secondary beams under the actual aircraft wheel compression and the unit uniform load is simulated by the finite element software, and the different beam-plate arrangement is obtained. At the same time, the average load reduction coefficient of the main and secondary beams is obtained, and the applicability of these results is analyzed, and some suggestions for use are given.
【學位授予單位】：清華大學
【學位級別】：碩士
【學位授予年份】：2015
【分類號】：TU318

【參考文獻】

相關(guān)期刊論文 前10條

1 趙均;徐小燕;朱丹;陳勝兵;;飛機庫結(jié)構(gòu)考慮罕遇地震多維輸入的彈塑性動力分析[J];北京工業(yè)大學學報;2011年07期

2 顧志福;楊樂天;陳青松;李燕;裴永忠;;大型機庫屋面風荷載特性研究[J];北京大學學報(自然科學版);2008年04期

3 徐慶陽;李愛群;沈順高;裴永忠;;西安某機庫彈塑性抗震分析[J];特種結(jié)構(gòu);2008年01期

4 沈順高;張微敬;朱丹;錢稼茹;裴永忠;;大跨度機庫結(jié)構(gòu)多點輸入地震反應分析[J];土木工程學報;2008年02期

5 朱丹;裴永忠;徐瑞;湯紅軍;曾荻;趙天佑;;北京A380機庫大跨度結(jié)構(gòu)設計研究[J];土木工程學報;2008年02期

6 錢稼茹;張微敬;朱丹;徐瑞;趙作周;胡曉斌;;北京A380機庫結(jié)構(gòu)地震反應分析[J];土木工程學報;2008年02期

7 裴永忠;寇巖滔;朱丹;沈順高;顧志福;;北京A380機庫風洞試驗及風振響應分析[J];土木工程學報;2008年02期

8 趙伯友;朱丹;裴永忠;劉子彥;;埃航B747飛機維修機庫鋼結(jié)構(gòu)設計[J];建筑結(jié)構(gòu);2006年09期

9 朱丹;裴永忠;曾荻;湯紅軍;徐瑞;趙天佑;;首都機場A380機庫的結(jié)構(gòu)方案優(yōu)化[J];建筑結(jié)構(gòu);2006年S1期

10 杜東升,李愛群,徐趙東,葉繼紅,沈順高;多點輸入下大跨度空間結(jié)構(gòu)的消能減震分析[J];特種結(jié)構(gòu);2005年02期

相關(guān)會議論文 前2條

1 陸賜麟;;預應力鋼結(jié)構(gòu)發(fā)展五十年[A];第二屆全國現(xiàn)代結(jié)構(gòu)工程學術(shù)研討會論文集[C];2002年

2 劉錫良;周學軍;許立準;;網(wǎng)架結(jié)構(gòu)超大直徑焊接空心球節(jié)點破環(huán)機理分析及其承載能力的試驗研究[A];第八屆空間結(jié)構(gòu)學術(shù)會議論文集[C];1997年

，

本文編號：2368454