提出了大型民機余度飛控計算機的兩個設計準則 :滿足系統的可靠性指標和滿足 FO/ FO/ FO容錯等級。然后 ,根據這兩個基本準則 ,為中國大型民機余度飛控計算機新方案的設計提供了 7個設計建議 ,確定了大型民機余度飛控計算機新方案的余度數和余度結構。此外 ,介紹了大型民機余度飛控計算機新方案的工作方式 ,分析了新方案的可靠性 ,并與 B777和 A320的余度方案進行了比較。通過比較 ,可以證明該方案能夠滿足中國民機的可靠性要求 ,而且結構簡單合理 ,節約硬件資源 ,完全可以應用到中國民機的飛行控制系統中。
參 考 文 獻
[1] Yeh Y C. Triple2triple redundant 777 primary flight computer
[C] ∥IEEE Aerospace Applications Conference proceedings. 1996 ,1 :2932307.
[2] Andrade L , Tenning C. Design of the Boeing 777 electric system[ C] ∥Proceedings of the IEEE 1992 National Aero2 spaceand ElectronicsConference. 1992,3:128121290.
[3] BriereD,Traverse P.AirbusA320/A330/A340electrical flight control —a family of fault2tolerant systems[C] ∥The Twenty2third International Symposium on Fault2tolerant Computing. Piscataway : IEEE , 1993 :6162623.
[4] NaiduA K. Case study : airbus A340 flight control system
[R]. Charlottesville: Universityof Virginia,2002.
[5] 陳宗基 ,秦旭東 ,高金源 .非相似余度飛控計算機 [J ].航空學報 ,2005 ,26 (3) :3202327. ChenZongji,Qin Xudong,GaoJinyuan.Dissimilar redun2 dant flight control computer system[J ]. Acta Aeronautica et Astronautica Sinica ,2005 ,26 (3) :3202327. (in Chinese)
[6] 姚一平 ,李沛瓊 .可靠性及余度技術 [M].北京 :航空工業出版社 ,1991. Yao Yiping , Li Peiqiong. Reliability and redundant tech2 niques[M]. Beijing: Aviation Industry Press, 1991. (in Chinese)
[7] Collinson R P G. Fly2by2wire flight control[J ]. Compu2 ting and Control Engineering Journal , 1999 ,10 (4) :1412
152.
[8] Allen J G. Digital computer design guidelines for a full au2 thority fly2by2wire flight control system [ C ] ∥AIAA Digital Avionics System Conference. 1975.
[9] KarlssonJ.Reliable andfault2tolerant computer systems[R].
trol and Decision ,2005 ,20(10) :117321176. (in Chinese)
[ 11 ] 秦旭東 .非相似余度飛控計算機及虛擬樣機技術研究
[D].北京 :北京航空航天大學 ,2006.
Qin Xudong. Research on disimiliar redundant flight con2
trol computers and technology of virtual prototype[D].
Beijing : Beijing University of Aeronautics and Astronau2
tics , 2006. (in Chinese)
[ 12 ] Tai A T , Meyer J F , Avizienis A . Performability en2 hancement of fault2tolerant software[J ]. IEEE Transac2 tions on Reliability , 1993 ,42 (2) : 2272237.
[13 ] Wu J , Fernandez E B , Zhang M. Design and modeling of hybrid fault2tolerant software with cost constraints[J ]. Journal of Systems and Software , 1996 , 35 (2) :1412149.
[ 14 ] Sha L. Dependable system upgrade[C] ∥Proceedings of Real2time Systems Symposium. 1998 :4402448.
[ 15 ] Popov P , Littlewood B. The effect of testing on reliability of fault2tolerant software[C] ∥Proceedings of the Interna2 tional Conference on Dependable Systems and Networks. Piscataway : IEEE , 2004 :2652274.
[ 16 ] Kienzle J. Software fault2tolerance : an overview [ C ] ∥ LNCS 2655. 2003 :45267.
[ 17 ] Littlewood B , Strigini L. A discussion of practices for en2 hancing diversity in software designs[R]. KISPO Project Technical Report LS_DI_TR204 , 2000.
作者簡介 :秦旭東 (1976 -) 男 ,博士 ,工程師。主要研究方向 :余度飛行控制系統、運載火箭姿態控制總體設計。
E2mail :qinxudong @buaa. edu. cn (責任編輯 :張利平 ,孔琪穎 )
. 1994-2009 China Academic Journal Electronic Publishing House. All rights reserved. http://www.cnki.net
文章編號 :100026893 (2008) 0320721207
大型整體壁板成形技術
曾元松 ,黃遐 (北京航空制造工程研究所 ,北京 100024)
Forming Technologies of Large Integral Panel
Zeng Yuansong , Huang Xia
(Beijing Aeronautical Manufacturing Technology Research Institute , Beijing
100024 , China)
摘 要 :大型整體壁板是現代先進民用飛機的重要結構件 ,大型整體壁板成形技術是整機研制過程中所必須要解決的重大關鍵技術。從大型整體壁板的結構特點出發 ,介紹了整體壁板的結構形式和分類 ,重點闡述了整體帶筋壁板噴丸成形技術和時效成形技術的國外研究應用進展及發展趨勢
,分析了國內現有整體壁板成
中圖分類號 : T G306 文獻標識碼 :A Abstract : Large integral panels are the main structure parts of the modern advanced civil airplanes. The form2 ing technology of the large integral panels is an important key technology which must be solved during the de2 veloping process of an airplane. Starting from the structure characteristics of the large integral panels , the structure forms and classification of the integral panels are introduced , and the oversea research situation and the developing tendency of the shot peen forming and the creep age forming technologies for the panel with in2 tegral stringers are emphatically presented. The research basis and the existing problems of forming technolo2 gies of the integral panels in China are also analyzed. Especially , the newest achievements obtained during the developing process of ARJ21 regional jet plane are introduced. Finally , some suggestions and research empha2 ses are proposed for developing as quickly as possible the forming technologies of fuselage and wing panels of large aircraft. Key words : integral panel ; shot peen forming ; creep age forming ; large aircraft ; aluminum
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