level the aircraft 中文意思是什麼

level the aircraft 解釋
把飛機拉平
  • level : n 1 水平儀,水準儀;水準測量。2 水平線,水平面;水平狀態;平面,平地。3 水平,水準;水位;標準;...
  • the : 〈代表用法〉…那樣的東西,…那種東西。1 〈用單數普通名詞代表它的一類時(所謂代表的單數)〉 (a) 〈...
  • aircraft : 飛機(單復數同)
  1. The aircraft is lost control now, i can not maintain level flight at present altitude

    飛機現在失去操縱,我在現在的高度上不能保持平飛。
  2. Based on the mathematical model developed by the paper, the trim calculations are carried out in the conditions that the example aircraft converts from helicopter to airplane mode in level flight with zero longitudinal acceleration and angular rate

    本文依據所建立的樣例機縱向動力學模型,假定飛機在給定高度平飛,縱向加速度和角加速度均為零,完成過渡模式下的動力學配平。
  3. The losses in the low-level attacks on the bridges from the german anti-aircraft artillery were cruel.

    在低空轟炸浮橋時,英國空軍由於德國高射炮炮擊造成的損失是很慘重的。
  4. Their primary purpose is to enable the efficient transition of departing aircraft from the airport to the upper level airways

    該飛行程序主要目的是幫助離港航機迅速地從機場爬升到指定的航道。
  5. Low - level windshear and turbulence alerts for the approach and departure areas within 3 nautical miles of the runway thresholds are issued by the amo for relay by air traffic controllers to approaching and departing aircraft

    機場氣象所發出在跑道進口3海里內的機場升降區的低空風切變及湍流警報,由航空交通管制員轉送至正在升降的航機。
  6. The shear experienced by the departing aircraft was due to vertical shear as the plane passed through the low level jet. based on the winds measured on - board a flight departing 8 minutes earlier, there was a rapid increase in head wind component, from 13 kt at 1, 420 ft to 39 kt at 3, 100 ft

    起飛的飛機所遇到的風切變是由於該機經過低層急流的垂直切變所引致,根據一架在8分鐘前起飛的航機量度到的風速,顯示逆風由1 , 420尺的每小時13海里急速增加到在3 , 100尺的每小時39海里。
  7. An airline ' s share on a certain market is affected by the airline ' s level of service ( quality of product ), including flight frequency, ticket price and aircraft type offered to the market

    摘要航空公司在某一市場上的份額受該公司在該市場提供的服務水平(產品質量)的影響,包括航班頻率、票價、機型等。
  8. A large planar microphone array, which consists of 111 microphones, was successfully applied to obtain a two - dimensional mapping of the sound sources on a landing aircraft. the focus of study in this paper is on the landing gear noise source. the spectra, directivities and sound pressure levels of flap side - edge noise of 7 narrow - board commercial aircraft and 7 wide - board commercial aircraft are presented. it is found that the landing gear noise spectrum is broadband with some single tones in some cases. the directivity of the total sound pressure level of a landing gear noise resembles that of a horizontal dipole. the level differences between the various aircraft landing gears are larger than those expected from the airspeed differences. it is thus expected that the louder noise emission of the landing gears can be reduced by redesigning

    應用由111個傳聲器組成的平面傳聲器陣列對當前流行的民用客機進場著陸過程中的機體噪聲源進行了實驗測量,本文對七架窄體客機和七架寬體客機的起落架噪聲進行了分析,得到了起落架噪聲的頻譜特性、指向特性和聲級變化.研究發現,起落架噪聲的頻譜是由寬頻隨機噪聲與一些較為明顯的單音噪聲源組成,起落架噪聲的指向性類似於一個水平放置的偶極子.不同飛機起落架噪聲的聲級相差較大,這說明可以通過重新結構設計降低起落架噪聲。
  9. Under the order, the minimum levels of csl under the existing administrative requirement ( ranging from us $ 25 million to us $ 1 billion depending on aircraft weight ) will continue to apply. the only change is the addition of a us $ 15 million minimum csl level for light aircraft. this new level is to ensure adequate insurance cover while not imposing an excessive burden on light aircraft operators

    根據命令規定,現時透過行政措施訂立的最低合一限額保險的數額(按照飛機的重量,由2 , 500萬美元至10億美元不等)將繼續適用;而唯一的改變就是加入輕型飛機的最低保額( 1 , 500萬美元) ,以確保規定項目有足夠的保障,同時亦不致令有關經營者負擔過重。
  10. This thesis regard internal property reorganization in the group of pangang as the research object, from chengdu seamless steel pipe limited liability company with chengdu iron and steel works inside exterior environment reorganizing in front and back commences, making use of to exceed the makel - bot with of five factors competition models and the method of factors analysis, after analyzing the reorganization of the business enterprise a profession for facing competes the situation. develop the development the business enterprise with the profession industry from the international local profession rival circumstance after analyzing the reorganization should the market position of the establishment with develop the strategy target. make use of the swot the analysis the method, to after the reorganization the development strategy of the business enterprise, from manage the angle proceeded the fixed position analyzes, for after the reorganization business enterprise development provided four kinds of developments strategy that eligibility choose : the brave development strategy, request the resources advantage, funds advantage, human resource advantage, technique advantage that new company make the most of new business enterprise in empress in reorganization, is an essential condition to increases to manage the level, quickly technique reforms, develop the high and additional worth product with new product production line, as soon as quikly change to strong and large business enterprise, realizes soon steel aircraft carrier dream ; dispersion strategy, the technology market quota with deal with produce high additional worth product, completely promote business enterprise brand image, extend high carry product of the exaltation product, is a necessary means to increases business enterprise performance, realizes business enterprise target ; defense strategy, adjusting the business enterprise organizes construction, reducing the intensive type in labor and the low additional worth product line, lower bad the property saves the deal, alleviating the business enterprise burden, attaining the casual wear go to battle, benefitting to the challenge that make frontal attack the rival ; withdraw strategy, compress the production of the high depletion and high cost product, simplify the production craft, controlling the cost of the end product in the lower level, is a valid path to increases business enterprise competition ability

    本論文以攀鋼集團內部的資產重組為研究對象,從成都無縫鋼管有限責任公司與成都鋼鐵廠重組前後的內外部環境入手,運用邁克爾?波特的五力競爭模型及因素分析法,分析了重組后的企業所面臨的行業競爭態勢。從國際國內行業競爭對手情況和本行業發展動態分析了重組后企業應確立的市場地位和發展戰略目標。運用swot分析法,對重組后企業的發展戰略,從管理角度進行了定位分析,為重組后企業發展提供了可選擇的四種發展戰略:即大膽發展戰略,要求新公司充分運用重組后新企業的資源優勢,資金優勢,人力資源優勢,技術優勢,是提高管理水平,加快技術改造,開發高附加值產品和新產品生產線,盡快立於強勢企業之林,早日實現「鋼鐵航母」夢的必要條件;分散性戰略,提高產品的科技含量和生產高附加值的產品,全面提升企業品牌形象,擴大高端產品的市場份額,是提高企業效益,實現企業目標的必要手段;防禦性戰略,調整企業組織結構,削減勞動密集型和低附加值產品生產線,降低不良資產存量,減輕企業包袱,做到輕裝上陣,有利於迎擊競爭對手的挑戰;退出性戰略,壓縮高消耗、高成本產品的生產,降低低端產品的比例,精簡生產工藝,將最終產品的成本控制在較低水平,是提高企業競爭力的有效途徑。
  11. The total auto symbol recognition disposition method proposed in this paper can deal with the problem which converts papery of aircraft theory graphics or system graphics into vectorgraphs which can lose some useful information. furthermore, the display technique with multi - level buffer not only resolves the problem of high - speed for aircraft theory graphics or system graphics in cbt, but also ensures scrolling and zooming in / out smoothly and avoids the flashing phenomenon efficiently

    目前紙質的飛機系統圖、原理圖矢量化方法用基本的矢量圖元按其位置來再現原始圖,從而導致矢量后圖中各符號整體信息丟失問題,該文提出的自動符號識別方法可有效地解決該問題,此外改進多級緩沖顯示技術不但可有效地解決cbt中系統圖、飛機原理圖的快速顯示,而且也保證圖形可連續光滑滾動和消除放縮拖動時屏幕閃爍現象。
  12. Abstract : a large planar microphone array, which consists of 111 microphones, was successfully applied to obtain a two - dimensional mapping of the sound sources on a landing aircraft. the focus of study in this paper is on the landing gear noise source. the spectra, directivities and sound pressure levels of flap side - edge noise of 7 narrow - board commercial aircraft and 7 wide - board commercial aircraft are presented. it is found that the landing gear noise spectrum is broadband with some single tones in some cases. the directivity of the total sound pressure level of a landing gear noise resembles that of a horizontal dipole. the level differences between the various aircraft landing gears are larger than those expected from the airspeed differences. it is thus expected that the louder noise emission of the landing gears can be reduced by redesigning

    文摘:應用由111個傳聲器組成的平面傳聲器陣列對當前流行的民用客機進場著陸過程中的機體噪聲源進行了實驗測量,本文對七架窄體客機和七架寬體客機的起落架噪聲進行了分析,得到了起落架噪聲的頻譜特性、指向特性和聲級變化.研究發現,起落架噪聲的頻譜是由寬頻隨機噪聲與一些較為明顯的單音噪聲源組成,起落架噪聲的指向性類似於一個水平放置的偶極子.不同飛機起落架噪聲的聲級相差較大,這說明可以通過重新結構設計降低起落架噪聲。
  13. The result control system is demonstrated using post - stall maneuver simulation, the results show that this control law achieves a high level performance in post - stall maneuver conditions even if the aircraft model has large uncertain items

    結果表明,在存在較大模型誤差的情況下,所設計的飛控規律完全能在過失速機動條件下控制飛機跟蹤指令飛行。
  14. Aircraft noise is an important problem for the larger noise level. the ma60 is one of the new commercial aircraft in china. in the design and producer of this airplane, the noise from the apu of this plane is very large and need to be reduced

    我國中航一集團西飛公司最新研製的新舟60飛機的apu ( auxiliarypowerunit ,輔助動力裝置)在機場停靠時會產生較大的噪聲,極大的影響旅客乘坐飛機的舒適度。
  15. During the aircraft cockpit layout design, the database of knowledge and rule is reasonable and efficient, and reaches a request of the real - time assembly, and provides the methods by which the designer estimates an aircraft cockpit layout design, and enhances the design efficiency and precision, and improves the level of the aircraft cockpit layout design

    在飛機駕駛艙布局設計的實際應用中,表明了知識與準則數據庫高效、合理,達到了實時裝配要求,提供了飛機駕駛艙布局設計的評估手段,保證了設計效率和精度,提高了飛機駕駛艙布局設計水平。
  16. Departing flights were climbing at very steep angles, 9. 6 deg for the one shown above. as a result, the aircraft transit the low level jet very close to the end of the runway and the change in head wind was very rapid

    起飛的航機以非常陡的角度爬升,以上提及的飛機用9 . 6度,因此飛機在接近跑道末端經過低空急流而所感受到的逆風轉變非常快。
  17. The fdps processes the flight plan data from aeronautical messages and prints out flight progress strips automatically for use by air traffic controllers to updatemonitor the aircraft flight profile, such as flight route, estimated time of departurearrival, flight level, expected times at reporting points, cruising speed, etc

    飛行數據處理系統可作航機飛行計劃的數據處理,和即時印出飛行進度紙條,供航空交通管制員用以更新和監察航機的飛行狀況,例如航道、預計著陸起飛時間、飛行高度、位置報告的預計時間、飛行速度等。
  18. Forecast charts showing wind and temperature data appropriate to the cruising level of the aircraft

    適用於飛機巡航高度的風及溫度圖。
  19. With the progress of aviation technology, the factor of pilot has been becoming one of the issues that restrict the level of aircraft cockpit design greatly

    隨著航空科技的進步,人的因素成為制約戰斗機座艙設計水平提高的主要瓶頸之一。飛機座艙設計作為人機交互的關鍵具有重要的研究價值。
  20. The progress of aero - technology improves the level of aircraft cockpit layout design

    航空科技的進步為飛機駕駛艙布局設計水平的提高創造了條件。
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