C/C复合材料与高温合金GH600之间高温接触热阻的试验研究

ACTA AERONAUTICAET ASTRONAUTICA SINICA ›› 2010, Vol. 31 ›› Issue (11): 2189-2194.

• Solid Mechanics and Vehicle Conceptual Design • Previous Articles Next Articles

Experimental Investigation of High-temperature Thermal Contact Resistance Between C/C Composite Material and Superalloy GH600

Liu Donghuan, Zheng Xiaoping, Huang Quanzhang, Yao Fuyin, Liu Yinghua

School of Aerospace, Tsinghua University

Received:2010-01-25 Revised:2010-03-29 Online:2010-11-25 Published:2010-11-25
Contact: Zheng Xiaoping

Abstract

Abstract: The heat pipe cooled leading edge is a novel and efficient thermal protection method in hypersonic aircraft design, and the thermal contact resistance between the C/C composite material structure and high-temperature heat pipes plays a very important role in heat transfer efficiency and thermomechanical coupling. A testing platform of high-temperature thermal contact resistance is established, with which the thermal contact resistance between a three-dimensional braid C/C composite material and a superalloy GH600 specimen is tested under different interface pressures, interface roughnesses and temperatures. The results show that the present testing platform is feasible for the experimental investigation of high-temperature thermal contact resistance, and the thermal contact resistance between three-dimensional braid C/C composite material and superalloy GH600 is obtained, which can be an important reference for the design and safety evaluation of heat pipe cooled thermal protection structures.

Key words: thermal contact resistance, C/C composite material, superalloys, experimental investigation

CLC Number:

V214.9

Liu Donghuan;Zheng Xiaoping;Huang Quanzhang;Yao Fuyin;Liu Yinghua. Experimental Investigation of High-temperature Thermal Contact Resistance Between C/C Composite Material and Superalloy GH600[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2010, 31(11): 2189-2194.

[1]	Zhiting GAO, Zhuang MA, Yanbo LIU. Effect of CVD-SiC array structure on ablation resistance of ZrB₂/SiC coatings [J]. Acta Aeronautica et Astronautica Sinica, 2024, 45(3): 428842-428842.
[2]	LI Qian, ZHANG Fulu, ZHAO Zihua. Very high cycle fatigue of nickel-based single-crystal and directionally solidified superalloys: Review [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2021, 42(5): 524340-524340.
[3]	KONG Haohao, YANG Shufeng, QU Jinglong, DU Jinhui, HUANG Yancheng. Type and distribution of inclusion in GH4169 nickel based superalloy [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2020, 41(4): 423306-423306.
[4]	XIANG Honghui, GE Ning, GAO Jie, TANG Kai, YANG Rongfei. Effect of circumferential non-uniform tip clearance on performance of axial compressor [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2018, 39(2): 121491-121491.
[5]	YANG Xulei, ZHU Yuchuan, JI Liang, FEI Shangshu, GUO Yazi. Experimental investigation and characteristic analysis of a giant magnetostrictive materials-based electro-hydrostatic actuator [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2016, 37(9): 2839-2850.
[6]	DU Suigeng, JIANG Zhe, ZHANG Dinghua, JU Jiangtao, LI Na. Softening Mechanism of Grinding Surface Metamorphic Layer of GH4169DA [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2014, 35(5): 1446-1451.
[7]	SONG Laishou, XIA Pinqi. Experimental Investigation on Active Vibration Control of Elastic Beam by Using Piezoelectric Stack Actuator [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2014, 35(1): 171-178.
[8]	WANG Tao, CHEN Guoding, JU Jiangtao. Experimental Study of Constitutive Relationship of Superalloy GH4169 Under High Strain Rates [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2013, 34(4): 946-953.
[9]	DING Zhiping, ZENG Jun, CHEN Jiping. Study on Stress-weakening Damage and Low Cycle Fatigue of Ni-based Single Crystal Superalloy Under Multiaxial Asymmetric Loading [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2013, 34(12): 2768-2776.
[10]	LI Kemin, HAN Guangwei, DENG Bo. Influence of Aging Treatment on Microstructure and Properties of Cold-drawn Alloy GH350 [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2012, (6): 1156-1162.
[11]	LIU Donghuan, SHANG Xinchun. Effect of Thermal Contact Resistance on the Performance of Heat-pipe-cooled Thermal Protection Structures [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2012, 33(10): 1834-1841.
[12]	DU Suigeng, WANG Zhibin, LU Chao, JU Jiangtao, ZHANG Jing. Study on High-speed Milling Surface Microstructure of Superalloy [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2011, 32(6): 1156-1163.
[13]	ZHU Yu, WAN Min, ZHOU Yingke. Multi-stage Hydro-mechanical Deep Drawing of Complex Thin-walled Superalloy Parts [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2011, 32(3): 552-560.
[14]	WANG Zongren, ZHANG Weifang, TABG Qingyun, LIU Shengwang. Experimental Investigation of Thermal Contact Conductance Across GH4169/GH4169 Interface with Compensation Heater [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2011, 32(10): 1945-1950.
[15]	Bi Zhongnan;Dong Jianxin;Zhang Maicang;Zheng Lei;Zhang Qingquan. Experimental Study and Theoretical Calculation on Structure Stability of a Nickel-based Superalloy for Seals in Aero-engine [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2010, 31(3): 643-649.

Experimental Investigation of High-temperature Thermal Contact Resistance Between C/C Composite Material and Superalloy GH600

PDF (PC)

Knowledge

Abstract

Cite this article

share this article

References

Related Articles 15

Recommended Articles

Metrics

Comments