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C_C复合材料飞机刹车盘的三维温度场_雷宝灵.pdf

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1、 26 1 2 2009 MActa Materiae Compositae Sinica Vol.26 No.1 February 2009cI|:1000-3851(2009)01-0113-05l :2007-12-25; l :2008-03-12 “:SE$ “(2006CB600906)YT: ,p V, q,p V 3 =,Z_:C/C 、 、 V E-mail:C/C f 雷宝灵, 易茂中, 徐惠娟( 2vx 8SE L i, 410083)K 1: C/C f(B757) V V 4V5,KZE8 L s。 . , Ks、HHqFV。YV_) V M,4VCs 。TV :“

2、d ? Hq/W )46 s HrK659; 548.5 s HrK,V5 6,W Kv,6K y, Q, Kl。1 L _T, z, Lr。1oM: C/C ; ;Kms |: TB332 DS :A3-D temperature field for C/C composite braking discsLEI Baoling, YI Maozhong, XU Huijuan(State Key Laboratory of Powder Metallurgy, Central South University, Changsha 410083, China)Abstract: The tem

3、perature fields of C/C composites braking discs (B757)were studied by the finite elementmethod and experiment, as they were difficult to measure and reveal during the braking process.The loads,boundary conditions and loading processes in the finite element analysis of temperatures were discussed acc

4、ording tothe heat transfer theory and braking principle of the braking discs.The postprocessing of simulation describes thetemperature fields of braking discs during braking clearly and visually.The results show that the temperature of themidial stator rises to the maximum 659at 46 s;the temperature

5、 of the pressure bearing disk and pressurizing diskrises to the maximum at 48.5 s and the temperature of each test point increases firstly and then decreases in thewhole braking process, while the midial stator endures the biggest thermal load, followed by the pressure bearingdisk and the pressurizi

6、ng disk endures the least thermal load.The simulation results are consistent with theexperiment data, which verifies the validity of the temperature field results.Keywords: C/C composite;braking discs;temperature field;temperature test;finite elementC/C 、 p 、 ?、/ , , U,u .t b C/C J. , 2002,12(1):101

7、-105.Yi Maozhong, Ge Yicheng, Liu Bin, Huang Qizhong, XiongXiang, Huang Baiyun.Oxidation behaviour of C/C compositefor airplane brake disc J.The Chinese Journal of NonferrousM etals, 2002, 12(1):101-105.2 El Abdi R, Smarout H.Anisothermal modeling applying tobrake discs J. International Journal of N

8、on-linearM echanics, 1999, 34(5):797-805.3 ZS,R W. T E J., 2006, 19(1):31-35.Lu Guofu, Guo Shiyong.Numerical simulation of transienttemperature field of disc-pad brake J.Mechanical Research&Application, 2006, 19(1):31-35.4 , C. 9 J.M, 2002, 24(6):34-38.Ding Qun, Xie Jilong.T he temperature field and

9、 stress fieldcalculation of brake disc based on 3-dimension model J.Journal of the China Railway Society, 2002, 24(6):34-38.5 *,fy, . E K J.M, 2006, 28(2):39-43.Chen Deling, Zhang Jianwu , Zhou Ping.FEM T hermal stressanalysis of hig h speed locomotive braking discs J.Journal ofthe China Railway Soc

10、iety 2006, 28(2):39-43.6 uZ ,fZ ,k, r, . y VKs J. bv, 2004, 54(5):589-592.Zhao Haiyan, Zhang Haiquan, T ang Xiaohua, Lin Jian, CaiZhipeng.T hermal FEM analysis of passenger railway carbrake discs J.J T singhua Univ:Sci &Tech, 2005, 45(5):589-592. 7 Gao C H, Lin X Z.Transient temperature field analys

11、is of abrake in a non-axisymmetric three-dimensional model J.Journal of Material Processing Technology, 2002, 129(1/3):513-517. 8 - , ,U,u .x 8t b J.x 8 S, 2005, 10(4):241-246.Yao Pingping, Wang Lin, Xiong Xiang, Huang Baiyun.Research on temperature field of powder metallurgy aviationbrake assemblag

12、e J.Materials Science and Engineering ofPowder Metallurgy, 2005, 10(4):241-246. 9 !, V.f s J. =, 2006(6)104-107.Li Tao, Wu Ruixiang.3-D transient temperature field analysisfor aircraft brake system J.Mechanical Engineer, 2006(6):104-107. 10 ,e,- .fV E J.x 8 S, 2007, 12(5):305-309.Zhou Ping, Jian Zhe

13、ngzhu, Yao Pingping. Numericalcalculation and research on temperature field of brake foraircraft during braking J.Materials Science and Engineeringof Powder Metallurgy, 2007, 12(5):305-309. 11 Choi Ji-Hoon, Lee In.Finite element analysis of transientthermoelastic behaviors in disk brakes J.Wear, 2004, 257(1/2):47-58. 12. . M.: S, 1998:139-226.Wang Buxuan.Engineering heat and mass transfer M.Beijing:Science Press, 1998:139-226.117 2,:C/C f

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