飛行用水 的英文怎麼說

中文拼音 [fēihángyòngshuǐ]
飛行用水 英文
inflight water
  • : Ⅰ動詞1 (鳥、蟲等在空中活動) fly; flit 2 (利用動力機械在空中行動) fly 3 (在空中飄浮遊動) fly...
  • : 行Ⅰ名詞1 (行列) line; row 2 (排行) seniority among brothers and sisters:你行幾? 我行三。where...
  • : Ⅰ動詞1 (使用) use; employ; apply 2 (多用於否定: 需要) need 3 (敬辭: 吃; 喝) eat; drink Ⅱ名...
  • : 名詞1 (由兩個氫原子和一個氧原子結合而成的液體) water 2 (河流) river 3 (指江、河、湖、海、洋...
  • 飛行 : flight; flying; aviate; voyage; volitate; hop
  • 用水 : category:drinking water
  1. Aircraft - connection for water of drinkable quality

    器.可飲的供連接
  2. The method of wing shape optimization of space shutlle has been developed with penalty function approach in which the objective function is the mass of the wing and the constraints are the hypersonic re - entry flight cross range, lift / drag ratio, and subsonic flight lift / drag ratio, the margin of the longitudial static stability and the magnitude of the horizontal landing speed etc

    摘要介紹了在滿足高超音速再入橫向機動航程,高超音速再入時的升阻比,亞音速進場時的升阻比,縱向靜穩定性裕度和平著陸速度等性能設計要求下,罰函數法尋求使航天機機翼質量為最小的外形優化方法並給出了算例。
  3. The evolution course of chinese solid rocket propulsion technology for space missions since 1950s is presented. the technical features, development process, ground tests and flight records of nine typical solid motors are described. these motors were developed for sounding rockets, upper stages of launch vehicles and orbit transfer systems in application satellites respectively. the evolution of basic technology of chinese solid rocket motors and future developing concept are briefly introduced. the information in the paper are all based on the published literatures

    敘述了20世紀50年代以來中國航天固體火箭推進技術的發展歷程,介紹了9種最具代表性的固體火箭發動機的技術特徵、研製過程、地面試驗和情況,這些發動機分別應於中國的探空火箭、運載火箭上面級和應衛星變軌系統.文中還簡要地評述了中國固體推進各單項技術的發展
  4. Abstract : the evolution course of chinese solid rocket propulsion technology for space missions since 1950s is presented. the technical features, development process, ground tests and flight records of nine typical solid motors are described. these motors were developed for sounding rockets, upper stages of launch vehicles and orbit transfer systems in application satellites respectively. the evolution of basic technology of chinese solid rocket motors and future developing concept are briefly introduced. the information in the paper are all based on the published literatures

    文摘:敘述了20世紀50年代以來中國航天固體火箭推進技術的發展歷程,介紹了9種最具代表性的固體火箭發動機的技術特徵、研製過程、地面試驗和情況,這些發動機分別應於中國的探空火箭、運載火箭上面級和應衛星變軌系統.文中還簡要地評述了中國固體推進各單項技術的發展
  5. This had a hovercraft like engine and also worked on the magnetic energy fields like the space crafts

    它有一個象翼船一樣的引擎,工作原理與器一樣,也是利磁能場。
  6. Application the retrieval coefficients of the city of changchun in april to a field experiments in jilin province, on april 22 demonstrate the airborne up - looking microwave radiometer can detect cloud liquid water and supercooled liquid water content

    此外,本文將求得的長春地區4月的反演系數應到長春4月22日的一次實驗中,結果表明,能夠探測出雲中液態和過冷含量及其變化。
  7. The gfs undertakes a variety of roles which include supporting the hong kong police force in law enforcement duties, assisting the fire services department by water - bombing hill fires with underslung fire buckets, and assisting the lands department in aerial mapping and survey. in 1998, the gfs also transported

    政府服務隊負責多項不同種類的工作,包括支援警務處的執法動;利外掛的救火桶投擲彈,協助消防處撲滅山火;以及協助地政總署進高空繪圖和測量工作。
  8. The gfs undertakes a wide variety of roles which include supporting the police force in law enforcement duties, assisting the fire services department by water - bombing hill fires with under - slung fire buckets, and assisting the lands department in aerial mapping and survey. in 2000, the gfs transported

    政府服務隊負責多項不同種類的工作,包括支援警務處的執法動;利外掛的救火桶投擲彈協助消防處撲滅山火;以及協助地政總署進高空繪圖和測量工作。
  9. Today s exercise involved aerial search demonstration by a z9 helicopter from the pla, followed by water winching demonstrations by an eurocopter super puma as332 l2 helicopter from the gfs, which is one of the new aircraft acquired by the gfs to greatly enhance its capability as an emergency response service provider

    今日的演習包括由駐香港部隊派出一架直九直升機示範進搜索,而政府服務隊則利一架超級美洲豹as332l2直升機示範從中拯救傷者。這架直升機是政府服務隊最近添置的其中一架機,可以大大加強其提供緊急應變服務的能力。
  10. Second, by computing the trajectory of the missile and the method of analyzing cep, influences that the fighter ' s height, speed, pitch angle, the deflection angle between fighter and target, and the target moving characters make on the times of fighter attack and missile launch are deeply developed. third, by relating the motion of the missile and the fighter, the influences that fighter ' s dive angle and the deflection angle between fighter and target make on the attack field of the fighter are discussed in this paper when the fighter perform vertical and horizontal attack. criterion of attack effect is proposed focusing on attack time of the fighter, trajectory of the missile and destruction probability to the target

    本文主要完成了以下幾個方面的工作:對導彈可發射區和機可攻擊區進建模,通過對導彈彈道的模擬計算,並運典型的圓概率偏差精度分析方法,詳細討論了機實施攻擊時,機的高度h 、速度v 、俯仰角、與目標的偏離角_ x及目標運動特性等對機攻擊時機和導彈發射時機的影響;因此,將機和導彈結合起來,詳細研究了機在垂直平面和平平面內實施攻擊時,機俯沖角和與目標的偏離角_ x對機的攻擊范圍的影響;以機實施攻擊的時間t 、彈道特性和對目標的殺傷概率p來評判對地攻擊的效果;最後給出典型算例,通過對空地攻擊過程的模擬實現,對過載提出要求。
  11. In addition, airway winds, which are essentially grid - point wind and temperature data over the south china sea for 15 flight levels between 10, 000 and 43, 000 ft, are disseminated to the radar data processing and display system ( rdpds ) of the cad for calculation of the expected arrival time of aircraft at check points

    除此之外,氣象數據處理系統將機航道風的數據傳送至民航處的雷達數據處理及顯示系統,這些數據是風和溫度的網格點值,其平范圍覆蓋南海,垂直范圍是由10 , 000至43 , 000尺之間的15個高度;以上資料可來計算航機抵達各定位點的時間。
  12. In addition, airway winds, which are essentially grid - point wind and temperature data over the south china sea for 15 flight levels between 10, 000 and 43, 000 ft, are disseminated to the radar data processing and display system rdpds of the cad for calculation of the expected arrival time of aircraft at check points

    除此之外,氣象數據處理系統將機航道風的數據傳送至民航處的雷達數據處理及顯示系統,這些數據是風和溫度的網格點值,其平范圍覆蓋南海,垂直范圍是由10 , 000至43 , 000尺之間的15個高度以上資料可來計算航機抵達各定位點的時間。
  13. This paper presents a wider research field - risk analysis. through the study of the effects that threat factors and error factors impact on the flight risk and adjusting performance rules, the horizontal safe corridor, threat avoidance, vertical altitude real - time modification and the fastest trajectory programming are progressed

    總結前人在該方面的研究成果,提出一個更加廣義的研究角度? ?風險分析。通過對威脅因素、誤差因素對風險的作,調整性能準則而進平安全走廊設計、威脅迴避、垂直離地高度實時修正以及最快速航跡規劃。
  14. In the course of developing and before application, the performance of carrier - borne aircraft illuminated guidance system under the environmental state of movement should be tested firstly, especially the performances and state measures of glide indicator, rolling indicator and gyrohorizon which offer ship ' s movement postures to carrier - borne aircraft in the illuminated guidance system, this needs to offer a artificial carrier on the land that can imitate ship ' s movement in the water. at present, simulating table only has single degree of freedom at home application to carrier - borne aircraft illuminated guidance system which need change test and measurement situation and adjust benchmark in the course of experiment

    艦載機燈光引導系統作為艦載機著艦引導特輔裝置是載機艦船上不可或缺的特種裝置,是保證員的生命安全和艦載機安全回收的重要手段。其在開發過程中以及正式安裝使前,首先要通過在運動環境狀態下的性能測試,特別是燈光引導系統中為艦載機提供艦船運動姿態的下滑指示器、橫搖指示器以及陀螺地平儀的性能和狀態檢測,這就需要在陸地上為它們提供一個可模擬艦船在面運動的載體。
  15. His neighbor always let his chickens loose, and they ran over to reach the garden to dig out the roots and eat the flowers and make a mess everywhere. and he told his neighbor to keep the hens within his fence. but the neighbor said, " i don t believe in this kind of restriction, imprisonment

    有一架機發生故障,員就無線電向機場塔臺求救:呼叫塔臺,呼叫塔臺,緊急求救,緊急求救,我離陸地有300英里,離面有600英尺,機快沒油了,引擎著火,儀錶板也出問題了,副駕駛又心臟病發,請趕快指示我該怎麼辦?
  16. This thesis, which is devoted to the research on the smart rotor with actively controlled trailing - edge flap for hub oscillatory load reduction, offers a potential approach for the vibration reduction of helicopter

    本文對帶有主動控制后緣附翼的智能旋翼於降低槳轂交變載荷進探索性的研究,為降低直升機中機體振動平提供一條有效的新途徑。
  17. In this paper aircraft has made vertical and synthetic detecting flying purposefully on 9. 17, 2003 according to cloud ' s macro and microstructure. vertical layers and representative places of stratiform cloud on 9. 17, 2003 are analyzed using the observational data of particle measurement system ( pms ), combined with satellite data, radar data, and precipitation data on ground. by this we have got cloud ' s microphysical structure and physical process of the natural precipitation, and the physical effect evidence has been testified according to observational data after lco2 seeding

    本文綜合觀測的方法,利機載pms雲粒子探測系統,根據雲系的宏微觀結構特徵進有針對性的垂直探測,配合衛星、雷達、地面雨量、雨強計網觀測資料對2003年9月17日延安降性層狀雲系中那些有代表性的部位或垂直分層做細致的觀測分析,獲得雲系的微物理結構和自然降形成的物理過程,並觀測事實來驗證人工增雨引晶催化后的物理響應判據。
  18. With the improvement of aviation technology, the controlled flight into terrain ( cfit ) accidents / instances result from human factor has become the main cause result in the air disaster

    隨著航空設備技術平迅速提高,人為因素造成的可控撞地cfit已經成為商機機毀人亡的主要原因。
  19. For passengers on long - haul flights, we offer specially selected amenity kits for him acca kappa products from italy and victorinox travel bags from switzerland and for her darphin products from france and ipa - nima travel bags from vietnam as well as basic essentials including toothbrushes, toothpaste and mouthwash

    對于遠程的乘客,我們為您提供來自elemis的一些旅必須品,包括精選護膚品,牙刷,牙膏和漱口
  20. This thesis is a fem analysis of opening process of the folded horizontal tail wing of some aircraft, and the work includes modeling the detailed mechanic assembly of the tail wing, and computing its elastic dynamic process by large - scale fem software system, ansys and ls - dyna3d, as well with the postprocessor tool - lspost to take the computational results into visualization

    本文運大型有限元cae軟體ansys和ls - dyna3d對某具體平折疊尾翼的機構運動進了細致的有限元建模和動力學計算分析,運lspost對計算結果進了詳細的后處理,運可視化技術對數值分析結果進了圖形及曲線描述。
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