airplane structure 中文意思是什麼

airplane structure 解釋
飛機結構
  • airplane : n. 〈美國〉 飛機〈英國說 aeroplane〉。2. vi. 坐飛機。
  • structure : n. 1. 構造,結構;組織;石理,石紋。2. 建造物。3. 【化學】化學結構。4. 【心理學】(直接經驗中顯現的)結構性,整體性;整體結構。adj. -d ,-less adj.
  1. This article gives the subsistent ability and the analysis result of intensity after repair in the open field airplane composite material structure by research the intensity, rigid and repair problem under a axis compress loads on a typical three stiffened composite laminate which has a penetrability crack ( a scatter damage ) by a shrapnel

    本文通過飛機典型復合材料三加筋層壓板結構在被彈片劃開一穿透性切口(離散源損傷)后,在軸向壓縮載荷作用下所產生的強度、剛度以及修理問題展開了技術研究及探討,給出軍機復合材料加筋板在彈擊後生存力以及外場修理后強度恢復分析結果。
  2. This article, through analysis different system radar ’ s superiority and limitation in target identification, proposes to unite the convention air defense radar ’ s echo characteristic and the electronic support sensory system ’ s aircraft - borne radiant characteristic, structure reasonable recognition system. it can satisfie the airplane target identification demand under the different background

    本文通過分析不同體制雷達在目標識別上的優勢和局限性,提出把常規防空雷達回波特徵和電子支援偵察系統得到的機載輻射源特徵聯合起來,構造合理的識別系統的新思路,以此來滿足不同背景下對飛機目標識別的需求。
  3. Abstract : problems existed in using combined jig to assemble airplane are analyzed and the principle of how to select integral structure configuration of jig for airplane assembly is introduced. correct setting of three supporting points of the integral jig is discussed in the paper as well

    文摘:分析歸納了飛機裝配中採用組合式型架存在的問題;介紹了飛機裝配中型架總體結構形式的選擇原則;討論了整體式型架3個支承點應如何正確設置。
  4. This paper investigates the condition and actual problems of civil airplane development, and then brings forward the plan that the correct management concept must be set up first, and we improve on the management process with this idea : in view of the complication and the condition of civil airplane development, general organizing structure in project management, we redesign the organizing structure - the strong matrix based the tetrahedral coordinates. analyze the management job of the civil airplane development, then research management process with the idea of project management, set up the new whole work flow. research some work flow such as risk management as a hotspot in project management

    本文針對民用飛機研製的現狀及存在的問題,提出了必須建立現代項目管理理念,用項目管理的思想來改進民機研製的管理流程:針對民機的復雜性,結合項目管理常用組織結構和民機研製項目現有的情況,對民機研製的組織結構進行了重組,建立了基於「四坐標」管理的強矩陣組織結構;在對民用飛機研製的管理工作充分分析的基礎上,按項目的生命周期,用項目管理的方法對民機研製的管理流程進行了研究,建立了新的、符合項目管理要求的民機研製項目總體流程;研究了民機研製項目具體工作流程。
  5. Because of the complicated structure and the long life cycle, the airplane r & d project needs configuration management much more

    航空工業中的型號產品研製由於其結構復雜、研製周期長,尤其需要進行技術狀態管理。
  6. It is suitable for : rc structure working such as bridge, road, airplane runaway, building, pre - casting, tar asphalt road, refractory material and etc

    適用: rc結構工程如橋梁道路機場跑道建築物預鑄結構柏油瀝青路面耐火材料等。
  7. Design requirements of mechanically fastened joint of composite structure for airplane

    飛機復合材料結構機械連接設計要求
  8. According to the principle of mrpii and its practical requirements, this paper presents the solution of management information system for the standard element workshop ( sew - mis ) of chengdu airplane industry company, and deals detailedly with the function model, operation flow, data flow, software structure and hardware environment of sew - mis

    本文以mrpii原理為指導,針對成都飛機工業(集團)有限責任公司標準件車間生產管理的實際需要,提出了標準件生產車間管理信息系統( standardelementworkshopmis , sew - mis )的解決方案。
  9. The applied technique for active vibration control of airplane structure

    飛機結構振動主動控制應用技術
  10. The quality of joint has much effect on the age limit of airplane. the fatigue strength can be improved by using interference - fit joint in metal joint - structure

    連接質量極大地影響著飛機的壽命,干涉配合連接能成倍提高接頭的疲勞強度。
  11. It is a potential high temperature structure material used in airplane engine and space shuttles. it is a long way to understand mechanical properties of three dimensional braided composite

    對於三維編織復合材料尤其是三維編織陶瓷基復合材料力學行為的認識還只是處于初級階段,還需要一個逐步認識逐步了解的過程。
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