機輪著陸 的英文怎麼說

中文拼音 [jīlúnzhāoliù]
機輪著陸 英文
wheel landing
  • 機 : machineengine
  • 輪 : Ⅰ名1 （輪子） wheel 2 （像輪子的東西） wheel like object; ring; disc 3 （輪船） steamer; steamboa...
  • 著 : 著助詞1. （表示動作的持續） 2. （表示狀態的持續） 3. （用在動詞或表示程度的形容詞後面, 加強命令或囑咐的語氣） 4. （加在某些動詞後面, 使變成介詞）
  • 陸 : 陸數詞（六的大寫） six （used for the numeral 六 on cheques, etc. to avoid mistakes or alterations）
  • 機輪 : motor ship
  • 著陸 : landing; land; touch down
  1. From 1980 to 1996, the amount of accident jet plan and turbine aerotransport which taking off weight exceed 5700kg all over the world is 621 times. in which there were 287 times wretched accident in the approach and landing phase, occupying 46 percent

    從1980年至1996年，全世界最大起飛重量5700公斤以上的噴氣式和渦輪螺旋漿運輸機發生重大死亡事故621起，其中發生在進近著陸階段的重大死亡事故287起，佔46 。
  2. Large modern-day aircraft utilizes either bicycle or tricycle landing gears.

    大型的現代飛機不是採用雙輪式著陸架，就是採用三輪式著陸架。
  3. Up to now, the dynamic simulation for aircraft landing and taxiing by the software adams based on the full aircraft model has not been found. in this paper, dynamic analysis for landing gear landing and taxiing is conducted for a large transportation aircraft with a post nose landing gear and two truck main landing gears. a dynamic analysis model of the landing gear and a full - scale aircraft model used in the simulation are developed by applying dynamics basic theory

    論文以我國某大型運輸飛機起落架為研究對象，應用動力學基本原理，基於adams aircraft模塊建立了起落架著陸動態性能分析模型以及由機身、前起落架緩沖支柱、前起落架機輪、主起落架緩沖支柱和主起落架機輪五個子系統構成的全機模型，進行落震、全機著陸與滑跑動力學模擬。
  4. Now, it is worthwhile to conduct the research on the ground load of landing gear with multi - wheels and multi - struts according to the basic theories of the mechanics, the dynamics analysis model of the full - aircraft during its landing process is established in this paper

    本文首先以某多輪多支柱飛機的起落架作為研究對象，應用動力學基本原理，建立了全機的著陸動力學模型。然後，通過利用大型動力學模擬軟體adams對該飛機進行了對稱著陸模擬，並對模擬結果進行了對比分析。
  5. Secondly, a full - aircraft assembly model in software adam is defined, which includes an airframe subsystem, a strut subsystem of the nose landing gear, a wheel subsystem of the nose landing gear, a strut subsystem of the forward main landing gear, a wheel subsystem of the forward main landing gear, a strut subsystem of the after main landing gear and a wheel subsystem of the after main landing gear

    在adams軟體中建立了一個由機身、前起落架緩沖支柱、前起落架機輪、前主起落架緩沖支柱、前主起落架機輪、後主起落架緩沖支柱和後主起落架機輪七個子系統構成的全機模型，並對該模型進行了對稱著陸模擬分析。
  6. At last, the researchers discussed and analyzed the results of the simulation contrastively. firstly, according to the conditions of the aircraft being researched, differential coefficient equations of the aircraft during its symmetric landing are established systemically in this paper

    文章的主要內容包括:以某多輪多支柱飛機的起落架為例，依據該起落對稱著陸的實際情況，系統地建立了該飛機的全機著陸動力模型以及飛機主起落架數學模型。
  7. It is proved by the analysis that, during the symmetric landing of that airplane, the impact load of the after main landing gear is the largest among those landing gears and the nose landing gear comprised of about 18 percent of the total impact load

    分析表明:該樣機在對稱著陸過程中，後主起落架承受的地面載荷最大，前起落架輪胎僅承擔了全機18 %的沖擊載荷，載荷分佈較普通的前三點式起落架有明顯的改善。
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