基于MSC/PATRAN的飞机结构强度静力试验数据实时跟踪与处理系统开发

ACTA AERONAUTICAET ASTRONAUTICA SINICA ›› 2007, Vol. 28 ›› Issue (1): 84-89.

Previous Articles Next Articles

Development of Test Data Tracking, Analyzing and Processing System for Aircraft Structural Strength Based on MSC/PATRAN Platform

LIU Yalong¹,WANG Shengnan¹,LIU Haifeng²,RAO Yonggang²,QU Weijian²

1Institute of Aircraft Structure Strength, Northwestern Polytechnical University, Xi′an 2Technical Center, Chengdu Aircraft Industry Company(Ltd)

Received:2005-07-18 Revised:2005-12-02 Online:2007-01-10 Published:2007-01-10
Contact: WANG Shengnan¹

Abstract

Abstract:

Under windows operation system, a system for test data tracking, analyzing and processing of aircraft structural strength (TestDTAS) is developed on MSC/PATRAN platform. The work is performed with adding special commands and windows by using the PCL language provided by MSC/PATRAN and C++ language. During the test of aircraft structural strength, the TestDTAS is able to timely monitor and display the structure stresses and displacements which also can be compared with the theoretical analysis results in the same time.

Key words: MSC/PATRAN, , PCL, , C++, , test , of , aircraft , structural , strength, , TestDTAS

CLC Number:

V216.1

LIU Yalong;WANG Shengnan;LIU Haifeng;RAO Yonggang;QU Weijian. Development of Test Data Tracking, Analyzing and Processing System for Aircraft Structural Strength Based on MSC/PATRAN Platform[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2007, 28(1): 84-89.

[1]	Jitao LI, Guangzhao HAN, Jun XIONG, Tian ZHOU, Lixun CAI. Novel small punch testing method and its application to conversion of mechanical properties for aerospace materials [J]. Acta Aeronautica et Astronautica Sinica, 2024, 45(3): 428708-428708.
[2]	Kaiming ZHANG, Kelu WANG, Shiqiang LU, Mutong LIU, Ping ZHONG, Ye TIAN. Thermal deformation behavior of S280 ultra-high strength stainless steel based on response surface methodology [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2023, 44(8): 427293-427293.
[3]	Ping CHEN, Xia YE, Huaqiang LIU, Yiliang HU, Xin YU. Axial stress measurement of bolts based on ultrasonic energy attenuation [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2023, 44(7): 227250-227250.
[4]	Liping LIU, Yuyang QI, Yueguo LIN, Rui BAO, Jianxin XU, Zhenyu FENG, Guanghui QING. Tensile failure of carbon fiber composite material bonded-rivet hybrid repaired structure [J]. Acta Aeronautica et Astronautica Sinica, 2023, 44(24): 428676-428676.
[5]	Zhiqiang ZHANG, Qingze GOU, Xuecheng LU, Hao WANG, Yiran CAO, Zhiyong GUO. Droplet transfer behavior of high strength aluminum alloy CMT+P arc additive manufacturing [J]. Acta Aeronautica et Astronautica Sinica, 2023, 44(13): 427881-427881.
[6]	Dahua DU, Bin LI. Key structural dynamic design technologies in liquid rocket engines: Review [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2023, 44(10): 27554-027554.
[7]	WAN Aoshuang. Probabilistic assessment on damage tolerance of composite helicopter horizontal tail structure [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2022, 43(6): 525557-525557.
[8]	WANG Houbing, WANG Xiahan, LIN Guowei, LI Xinxiang, YANG Shengchun. Residual strength evaluation of curved hat-stiffened composite panels with discrete-source damage [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2022, 43(6): 525899-525899.
[9]	LIU Zhendong, ZHENG Xitao, FAN Wenjing, ZHANG Dongjian. Effect of process-induced residual stress on strength of UAV composite wing [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2022, 43(6): 526117-526117.
[10]	SUN Cong. Development status, challenges and trends of strength technology for hypersonic vehicles [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2022, 43(6): 527590-527590.
[11]	WANG Binwen, NIE Xiaohua, WAN Chunhua, WU Cunli. Research and application of virtual test technology for static strength of full scale aircraft structure [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2022, 43(6): 526273-526273.
[12]	YANG Siyuan, WANG Ying, WANG Jilai, YANG Zhenwen, WANG Dongpo. Interfacial microstructure and mechanical properties of vacuum-brazed Al₂O₃ ceramic and GH3536 joint [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2022, 43(4): 525806-525806.
[13]	LIU Xin, YANG Jingchao, LI Heng, ZHANG Yanhong, YANG Zhiwei, GU Jingfei, LI Guangjun, HUANG Dan. Critical review on tube joining by plastic deformation [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2022, 43(4): 525258-525258.
[14]	ZOU Qi, YE Yiyun, JIAO Junke, WU Zhisheng, XU Zifa, ZHANG Wenwu. Performance analysis of carbon fiber reinforced thermalsetting composite-titanium alloy laser joint [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2022, 43(2): 625037-625037.
[15]	CAI Xiaoqiang, WANG Dongpo, WANG Ying, YANG Zhenwen. Interfacial microstructure and mechanical properties of TiB₂-TiC-SiC ceramics joints fabricated by contact reactive brazing technique [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2022, 43(2): 625006-625006.

Development of Test Data Tracking, Analyzing and Processing System for Aircraft Structural Strength Based on MSC/PATRAN Platform

PDF (PC)

Knowledge

Abstract

Cite this article

share this article

References

Related Articles 15

Recommended Articles

Metrics

Comments