撞擊試驗機 的英文怎麼說

中文拼音 [zhuàngjīshìyànjī]
撞擊試驗機 英文
ram tester
  • 撞 : 動詞1 （猛然碰上） collide; strike; knock; bump against; run into 2 （碰見） bump into; run into;...
  • 試 : 名詞（古代占卜用的器具） astrolabe
  • 驗 : 動詞1. （察看; 查考） examine; check; test 2. （產生預期的效果） prove effective; produce the expected result
  • 機 : machineengine
  • 撞擊 : 1 （撞） impact; ram; dash against; strike; knock; hit against 2 [工業] liquid knockout; percussi...
  • 試驗 : trial; experiment; test
  1. The accidents of bird impact have caused huge loss to human being. it is important to establish the predicting system to definite the response of the blade for the improvement the strength of the blade on the design of the resistance of the blade under the bird strike

    減少此類事故發生的措施之一是:針對易受鳥撞擊的發動機等主要部件，從理論與實踐方面研究鳥撞擊的機理，對其進行結構、強度及性能的計算與試驗分析，指導工程設計，提高這些部件自身的抗鳥撞擊能力。
  2. Electromechanical components for electronic equipment. basic testing procedures and measuring methods. part 5 : impact tests free components, static load tests fixed components, endurance tests and overload tests

    電子設備用機電元件基本試驗規程及測量方法第5部分:撞擊試驗
  3. It is observed from the result of test that the bird bodies basically show liquid characteristics in the process of impact and that the relative pa rts of the plane affect the dynamic response ' of windshield glass

    從高速攝像和攝像結果中發現，鳥體在撞擊過程中基本表現出流體特性，飛機的附件對鳥撞試驗有較大的影響。
  4. 3. wth application of large - scale computational software anasys - dyna, the case of elastic impact to each other of two recta - ngular cross - section rods has been implemented and also compared with theoretical results, which maks good agreement and draws very helpful practical experiences to use some techncal parameters in the program. eventually, the a real - world aircraft windshield shell structure impacted by a flying bird has been simulated through fem numerical computation, and meanime, an engineering predical experimeni of bird sttiking to the windshield in some type of aircraft has been performed

    3 、應用大型科學計算程序anasys - dyna ，對彈性體碰撞進行了數值計算驗證並與理論結果對比，獲得了計算參數應用的實踐經驗；在此基礎上，進行了鳥體撞擊飛機風擋結構動力學響應的實際數值計算，與此同時安排了工程鳥體撞擊試驗，並就兩者計算結果給予了細致分析對比，獲得了良好的一致性結論。
  5. It was found in preliminary tests that sound pressures of the oscillations were diminished with tripping wires or side jets when the wires or the jets were introduced into the impinging shear flow in certain ways

    初步的試驗表明，在一定條件下絆線或旁射流削弱了流動的自激振蕩。為探求它們削弱自激振蕩的機理，在非撞擊剪切層上進行一組可控實驗。
  6. An losipescu - type of fixture, which had been previously used for the static shear strength tests of unidirectional laminates or metal materials, was proved useful for the shear static and fatigue tests of multidirectional laminates

    （ 6 ）進行mdyb - 3座艙蓋有機玻璃撞擊損傷剩餘強度和疲勞裂紋擴展試驗，發現撞擊損傷引致的疲勞裂紋的擴展規律與理想的表面裂紋明顯不同。
  7. The cumulative damage modes and their distribution regions on 7t / 4 quasi - isotropic laminates were reasonably simulated and the predicted fatigue lives agree well with the test results. residual strength evaluation is playing a significant role in damage tolerance analysis of structures. chapter 4 describes a simple procedure for the evaluation of residual strength of metallic structures with cracks developed b

    提出按剩餘西北工業大學博士學位論文:飛機結構疲勞和斷裂分析中若干問題的研究強度等效和按疲勞壽命等效兩種途徑將撞擊損傷當量化為表面裂紋，並根據有限的試驗結果進行了嘗試，得到了一些初步結果。
  8. Standard test method for field measurement of tapping machine impact sound transmission through floor - ceiling assemblies and associated support structures

    通過地板和天花板組件及相關支承結構的夯擊機撞擊聲的現場測量的標準試驗方法
分享友人
分享到 Line

分享到臉書