Advanced Search
Volume 37 Issue 12
Dec.  2012
Turn off MathJax
Article Contents
Abstract
References
Journal of Beijing University of Aeronautics and Astronautics  > 2011  >  37(12): 1546-1551.
Yao Shuzhen, Jin Maozhong. Strategy of state transition in UML based on Petri net[J]. Journal of Beijing University of Aeronautics and Astronautics, 2008, 34(01): 79-83. (in Chinese)
Citation: Zhao Zhe, Jia Yuhong, Zheng Xin, et al. Security evaluation of nose wheel steering systems based on GSPN methods[J]. Journal of Beijing University of Aeronautics and Astronautics, 2011, 37(12): 1546-1551. (in Chinese)
shu

Security evaluation of nose wheel steering systems based on GSPN methods

  • School of Aeronautic Science and Engineering, Beijing University of Aeronautics and Astronautics, Beijing 100191, China

  • Received Date: 12 Nov 2010
  • Publish Date: 30 Dec 2012
    Abstract
  • To solve the problem of how to evaluate the safety of a system without relative statistical data, the generalized stochastic petri nets(GSPN) and classical evaluating method were hung together. Taking a certain type of airplane's nose wheel steering system, which was still at the stage of design, as an example, the failure modes and effects analysis (FMEA) list was set up by analyzing system's function structure figure. The failure rate, maintenance rate, the mean time between failure and the mean time of the maintenance were calculated by the experiential formula. According to these parameters and the nose wheel steering system's GSPN model, the steady failure probabilities were calculated by the TimeNET software package. The safety of the nose wheel steering system was evaluated with the experiential formula and the risk matrix. After the evaluation, this nose wheel steering system conforms to the design demands.

     

    • FullText(HTML)
    • References(1)
  • [1] 王永华,李本威,孙涛.FMECA在某发动机涡轮部件上的应用[J].航空工程与维修2002(4):27-28 Wang Yonghua,Li Benwei,Sun Tao.Application of FMECA on engine turbine parts[J].Aviation Engineering & Maintenance,2002(4):27-28(in Chinese) [2] 葛志浩,徐浩军,胡飞.某型飞机横向操纵系统的飞行安全评估及改进措施[J].飞行力学,2005,23(2):39-42 Ge Zhihao,Xu Haojun,Hu Fei.Flying security evaluation and improving measures of a certain plane lateral-directional control system [J].Flight Dynamics,2005,23(2):39-42(in Chinese) [3] 曾德容.地铁供电系统可靠性和安全性分析方法研究 .西南交通大学电气工程学院:2008 Zeng Derong.Research on reliability and safety evaluation method of metro power supply system .School of Electrical Engineering,Southwest Jiaotong University,2008(in Chinese) [4] 刘涛,蔡增杰.基于FMECA和模糊综合评判的飞机起动电磁阀安全性评估[J].机械,2009(12):65-68 Liu Tao,Cai Zengjie.Accessory safety assessment of airplane start-up electromagnetic valve based on FMECA and fuzzy comprehensive evaluation methods[J].Machinery,2009(12):65-68(in Chinese) [5] Von Mayrhauser A,Dube D.Simple and fast approximations for generalized stochastic petri nets[J].J Systems Software,1993,21(2):63-177 [6] 汪一亭,魏臻.基于Markov模型的离散事件系统稳态与暂态的分析[J].计算机工程与应用,2009,45(3):226-228 Wang Yiting,Wei Zhen.Research on steady states and transient states of discrete event system based on markov modle [J].Computer Engineering and Application,2009,45(3):226-228(in Chinese) [7] Chen M F.From Markov chains to non-equilibrium particle systems[M].Singapore:World Scientific Publishing Co Pte Ltd,1992 [8] Anderson W J.Continuous-time Markov chains[M].Berlin:Springer,1991 [9] Meyn S P,Tweedie R L.Markov chains and stochastic stability[M].Berlin:Springer,1993 [10] 陈永,胡晓辉.基于GSM-R铁路无线通信系统的越区切换分析研究[J].计算机工程与设计,2009,30(18):4342-4345 Chen Yong,Hu Xiaohui.Analysis of handover based on GSM-R wireless railway communications system[J].Computer Engineering and Design,2009,30(18):4342-4345(in Chinese)
    • Relative Articles

  • Relative Articles

    [1]ZHANG Xin-ze, LI Qin, WENG Yi-hui, YOU Yan-cheng. Numerical analysis and flow state prediction of double wedge steady/unsteady flow at different Ma∞、Re[J]. Journal of Beijing University of Aeronautics and Astronautics. doi: 10.13700/j.bh.1001-5965.2023.0758
    [2]SHI Tong, HE Yunqin, LIANG Guozhu, PAN Hui, ZHU Pingping. Theoretic model of flow resistance for gas-filled accumulators in liquid rockets[J]. Journal of Beijing University of Aeronautics and Astronautics. doi: 10.13700/j.bh.1001-5965.2023.0748
    [3]WU Z Y，GAO Z X，CHEN X M，et al. Mach number effect in shock-wave/turbulent-boundary-layer interaction flow[J]. Journal of Beijing University of Aeronautics and Astronautics，2024，50（11）：3484-3494 （in Chinese）. doi: 10.13700/j.bh.1001-5965.2022.0857.
    [4]CUI Y P，LI Z H，ZHENG G L. Computing convex hull of a generic polygon with simulation of progressive support for an elastic line[J]. Journal of Beijing University of Aeronautics and Astronautics，2024，50（1）：216-223 （in Chinese）. doi: 10.13700/j.bh.1001-5965.2022.0246.
    [5]ZHANG X J，XU C，TIAN F，et al. Utility-enhanced synthesis method of differentially private trajectories[J]. Journal of Beijing University of Aeronautics and Astronautics，2024，50（12）：3615-3631 （in Chinese）. doi: 10.13700/j.bh.1001-5965.2022.1013.
    [6]CHEN B，LUO L，JIANG A L，et al. Numerical simulation of separation characteristics for internally buried weapon at high Mach number[J]. Journal of Beijing University of Aeronautics and Astronautics，2024，50（7）：2113-2122 （in Chinese）. doi: 10.13700/j.bh.1001-5965.2022.0627.
    [7]XUAN L M，ZOU Z P，ZENG F. Analyzing and modeling flow in tip clearance of transonic turbine rotor[J]. Journal of Beijing University of Aeronautics and Astronautics，2023，49（9）：2374-2384 （in Chinese）. doi: 10.13700/j.bh.1001-5965.2021.0635.
    [8]ZHANG P H，TANG Y，TANG J，et al. Simulation of cavity flow at high Mach number based on adaptive unstructured hybrid mesh[J]. Journal of Beijing University of Aeronautics and Astronautics，2023，49（6）：1311-1318 （in Chinese）. doi: 10.13700/j.bh.1001-5965.2021.0424.
    [9]HAN Y F，HU X S，GAO Y，et al. Comparison of turbulence models for unsteady flow simulation in a long and narrow cabin[J]. Journal of Beijing University of Aeronautics and Astronautics，2023，49（4）：957-964 （in Chinese）. doi: 10.13700/j.bh.1001-5965.2021.0335.
    [10]HE Z P，ZHOU J X，XIN J，et al. Unsteady flow characteristics of turbine rotor passage under rim seal effect[J]. Journal of Beijing University of Aeronautics and Astronautics，2023，49（2）：273-283 （in Chinese）. doi: 10.13700/j.bh.1001-5965.2021.0223.
    [11]WANG Wei-jie, WANG Zhou, PANG Wei-kun, YANG Yang. Research on Angular Momentum Envelope Analysis Method of Frame Momentum Exchange Device[J]. Journal of Beijing University of Aeronautics and Astronautics. doi: 10.13700/j.bh.1001-5965.2023.0268
    [12]ZHANG P H，CHENG X H，CHEN H Y，et al. Unsteady flow mechanism of high Mach number cavity[J]. Journal of Beijing University of Aeronautics and Astronautics，2023，49（8）：1940-1947 （in Chinese）. doi: 10.13700/j.bh.1001-5965.2021.0609.
    [13]MENG L K，ZHU Y C，DING J J，et al. Influence of wedge erosion deformation on working characteristics of jet pipe servo valve[J]. Journal of Beijing University of Aeronautics and Astronautics，2023，49（11）：3177-3187 （in Chinese）. doi: 10.13700/j.bh.1001-5965.2022.0041.
    [14]BI Y P，ZHANG T，HE Y T，et al. Corrosion and fatigue life prediction of aircraft typical lap structures based on life envelope[J]. Journal of Beijing University of Aeronautics and Astronautics，2023，49（8）：2200-2206 （in Chinese）. doi: 10.13700/j.bh.1001-5965.2022.0604.
    [15]LYU Z Y，NIE X Y，ZHAO A B. Prediction of wing aerodynamic coefficient based on CNN[J]. Journal of Beijing University of Aeronautics and Astronautics，2023，49（3）：674-680 （in Chinese）. doi: 10.13700/j.bh.1001-5965.2021.0276.
    [16]WANG R C，ZHANG G X，WANG X Y，et al. Aerodynamic performance analysis of supercritical airfoil with lower surface jet[J]. Journal of Beijing University of Aeronautics and Astronautics，2023，49（7）：1671-1679 （in Chinese）. doi: 10.13700/j.bh.1001-5965.2021.0489.
    [17]ZHANG P H，CHEN H Y，ZHANG J，et al. Passive flow control for weapon bay at high Mach number[J]. Journal of Beijing University of Aeronautics and Astronautics，2023，49（11）：2913-2920 （in Chinese）. doi: 10.13700/j.bh.1001-5965.2021.0790.
    [18]CHEN Z L，LU Z X，XIAO T H，et al. Effect of local oscillation on aerodynamics of thin airfoil in Mars environment[J]. Journal of Beijing University of Aeronautics and Astronautics，2023，49（11）：2938-2950 （in Chinese）. doi: 10.13700/j.bh.1001-5965.2022.0032.
    [19]FANG Yifang, XIANG Gaoxiang, TANG Chun'e, SHI Yuejuan. Numerical simulation on internal flow performances of multi-stage pressure drop valve[J]. Journal of Beijing University of Aeronautics and Astronautics, 2022, 48(10): 1915-1924. doi: 10.13700/j.bh.1001-5965.2021.0070
    [20]YANG Lijun, HUANG Dongqi, HAN Wang, LI Jingxuan, FU Qingfei. Influence of flow topology on instability and atomization of liquid jets[J]. Journal of Beijing University of Aeronautics and Astronautics, 2022, 48(9): 1757-1766. doi: 10.13700/j.bh.1001-5965.2022.0608
    • Supplements(0)
    • Cited By
  • 加载中

Catalog

    通讯作者: 陈斌, bchen63@163.com
    • 1. 

      沈阳化工大学材料科学与工程学院 沈阳 110142

    1. 本站搜索
    2. 百度学术搜索
    3. 万方数据库搜索
    4. CNKI搜索
    Get Citation
    PDF
    XML

    Article Metrics

    Article views(3314) PDF downloads(586) Cited by()
    Proportional views
    Related

    Copyright © Journal of Beijing University of Aeronautics and Astronautics

    Address: Editorial Department of Journal of Beijing University of Aeronautics and Astronautics, 37 Xueyuan Road, Haidian District, Beijing Post Code: 100191 Email: jbuaa@buaa.edu.cn

    Supported by: Beijing Renhe Information Technology Co., Ltd.    

    /

    DownLoad:  Full-Size Img  PowerPoint
    Return
    Return