能的高壓壓氣機。
總之 ,為了進一步提高中國高性能大涵道比風(fēng)扇/高壓壓氣機的研制能力 ,不僅需要加強軟件開發(fā) ,提高軟件精度 ,更應(yīng)提高試驗研究水平 ,提高測試精度 ,提高理論、計算與試驗相結(jié)合的綜合研究分析能力。
4 結(jié) 論
大涵道比渦扇發(fā)動機以其高循環(huán)參數(shù)、低耗油率、低污染、低噪聲、高可靠性和長壽命等顯著特點 ,代表了一個國家民用航空發(fā)動機技術(shù)的最高水平 ,也是一個國家科技水平和創(chuàng)新能力的重要標志。
大飛機的立項 ,使我們面臨著嚴峻的挑戰(zhàn) ,也帶來了前所未有的良好發(fā)展機遇。作者相信 ,統(tǒng)一規(guī)劃 ,精心組織 ,抓住契機 ,迎頭趕上 ,就能盡快趕上國際先進水平。
參 考 文 獻
20 (4) :5772595.
[3] 陳光 .波音 787用發(fā)動機設(shè)計特點 [R].北京 :北京航空航天大學(xué) ,2007. Chen Guang. Advanced technologies of the engines for Boeing787[R]. Beijing:BeijingUniversityofAeronautics and Astronautics ,2007. (in Chinese)
[4] WislerDC. Compressorandfanaerodynamicdesign[R]. Beijing: Tsinghua University , 2006.
[5] Huff D. Technologies for turbofan noise reduction[C] ∥ 10th AIAA/ CEAS Aeroacoustics Conference. 2004.
[6] Dowling A , Greitzer E. The silent aircraft initiative2over2 view[ C] ∥45th AIAA Aerospace Sciences Meeting. 2007.
[7] Gliebe P R. The GE90 : quiet by design[ C] ∥Presentation for 2003 Berkeley Airport Noise Symposium. 2003.
[8] Smith L H. Axial compressor aerodesign evolution at gen2 eral electric[J]. Journal of Turbomachinery, 2002,124
(7) :3212330.
[9] Wadia A R. Some advances in fan and compressor aero at GE aircraft engines[R]. Beijing: Tsinghua University, 2005.
[ 10 ] Gliebe P , Dodds W. Practical technology solutions for fu2 ture aircraft engine noise and emissions reduction [C] ∥ AIAA/ AAAF Aircraft Noise and Emissions Reduction Symposium. 2005.
[ 11 ] Lord W K. Aircraft noise source reduction technology [C] ∥
21世紀航空動力發(fā)展研討會 .北京 :中國航空學(xué)會動力專業(yè)分會 ,2000 :74287. Chen Maozhang. Fan/compressor technology development and the suggestions on future research[C] ∥Symposium on the Proceedings of Aero2engine in 21st Century , Pro2 pulsionBranchof the AeronauticandAstronautics,2000: 74287. (in Chinese)
[ 20 ] 陳懋章 .葉輪機氣動力學(xué)研究及其發(fā)展趨勢 [ C]∥航空百年學(xué)術(shù)論壇動力分論壇 ,中國航空學(xué)會第五屆動力年會論文集 . 2003 :17239. Chen Maozhang. Some progresses and tendency of turbomach2 inery aerodynamics[C] ∥Propulsion Branch of the Aeronautic and Astronautics. 2003 :17239. (in Chinese)
作者簡介 :陳懋章 (1936 -) 男 ,教授 ,博士生導(dǎo)師 ,中國工程院院士。主要研究方向 :航空發(fā)動機 ,葉輪機氣動力學(xué)。 Tel : 010282314180 E2mail : chenmz @buaa. edu. cn
劉寶杰 (1971 -) 男 ,博士 ,教授 ,碩士生導(dǎo)師。主要研究方向 :葉輪機氣動力學(xué)。
Tel : 010282316419 E2mail : liubj @buaa. edu. cn (責(zé)任編輯 :劉振國 ,趙利 )
文章編號 :100026893 (2008) 0320734207
大型飛機自動化裝配技術(shù)
許國康
(北京航空制造工程研究所數(shù)字化與柔性裝配技術(shù)研究室 ,北京 100024)
Automatic Assembly Technology for Large Aircraft
Xu Guokang
(Numerical and Flexible Assembling Technology Department , Beijing Aeronautical Manufacturing
Technology Research Institute , Beijing 100024 , China)
摘 要 :簡述了大型飛機及其結(jié)構(gòu)特點 ,通過比較人與機器兩種裝配系統(tǒng)的特性 ,及分析裝配自動化水平與裝配成本等諸因素的關(guān)系曲線 ,指出了自動化裝配技術(shù)在保證大型飛機結(jié)構(gòu)長壽命、高效率、低成本研制和生產(chǎn)等方面的意義 ;對國外大型飛機的裝配自動化發(fā)展狀況進行了綜述 ,簡要分析了國外發(fā)展的幾種主要自動化裝配系統(tǒng) ,總結(jié)了國外大型飛機的自動化裝配水平 ;對西方國家在大型飛機自動化裝配中采用的先進的裝
配理念和方法
,如決定性裝配方法等進行了概述。最后針對國內(nèi)自動化裝配水平低的現(xiàn)狀和大型飛機研制和
assembly cost , points out the meaning of automatic assembly technology which ensures long life , high effi2 ciency and low cost of large aircraft structure , both in research and in manufacture. Also , the paper analy2 zes the overseas actuality of automatic assembly of large aircraft and several systems of automatic assembly and level of automatic assembly , and summarizes the advanced thought and means of automatic assembly of large aircraft of western countries , for example , determinant assembly. Finally , aiming at the actuality at home , such as the low level of automatic assembly and the demands for developing and manufacturing large aircraft , some suggestions are put forward , including developing the modularization automatic assembly system , carrying out the means of concurrent engineering and realizing the designs for manufacturing and assembly. Key words : automatic assembly; large aircraft; long life; flexible assembly; modularization; determinant as2 sembly
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