aero control 中文意思是什麼

aero control 解釋
航空防治
  • aero : adj. 1. 飛機的；航空的，飛行的。2. 〈口語〉（指汽車等）流線型的。n. 〈口語〉飛機；飛船；飛行。
  • control : n 1 支配，管理，管制，統制，控制；監督。2 抑制（力）；壓制，節制，拘束；【農業】防治。3 檢查；核...
  1. Since the aero maintenance cost takes a very great portion of the total operation cost of airlines, it is important to control the maintenance cost effectively for total cost control

    航空維修成本在航空企業總成本中占據非常大的比例，有效控制維修成本對航空公司控制總成本具有重要作用。
  2. Aero - engine multivariable learning fuzzy decouple control

    航空發動機多變量自學習模糊解耦控制
  3. The study work in the dissertation is an important part of the tenth five - year defence advanced research project of “ study on control technology of the machining distortion for complex structure parts ” supported by pla general armament department of china. theoretical analysis and experimental study are carried out on the initial residual stresses and their effects on milling distortion for thick aero - aluminum - alloy plate

    本文作為總裝備部「十五」預研項目「復雜結構件加工變形控制技術研究」的主要組成部分，以航空鋁合金厚板為對象，研究重點定位在其初始殘余應力分佈規律及其對數控銑削加工變形的影響。
  4. Then, depending on this result, through mending some relative parts of the control system, the optimal acceleration process for the x - model aero - engine is achieved

    並以此結果為依據，對發動機加速控制系統中的某些部件進行改進。使其能起到控制發動機完成最優加速過程的目的。
  5. This research is the scientific research project done by civil aviation college of nuaa cooperating with pratt & whitney ( china ). the project is of great significance for airlines, aero - engine manufacturers and repair shops to evaluate and control the engine maintenance cost ( emc )

    本項研究是南京航空航天大學民航學院與普惠中國公司合作的一項科研課題，該科研項目對于幫助航空公司、航空發動機研製廠商和修理廠商評估和控制發動機維修成本具有重要意義。
  6. With the development of multi - variable control technology and aero - propulsion technology, future excellent engine must have the character, which is high ratio in thrust and weight low fuel and long use life. therefore the control system of aero - engine has also been becoming more and more complicated. the precision of control system is also extra higher

    隨著高推重比、低油耗、長使用壽命、高機動性航空發動機的研製，現代航空發動機需要控制的變量越來越多、精度越來越高，因此，航空發動機控制系統變得越來越復雜，傳統的航空發動機控制系統是採用機械液壓控制。
  7. A general control system simulation platform of aero engines is constructed on the basis of performance simulation platform. kinds of control laws are discussed

    在控制系統模擬平臺上搭建某大型渦扇發動機和某中小型渦扇發動機的控制系統，通過模擬對控制系統模型類庫進行了驗證。
  8. Simulation is one of the important technologies in the processes of investigation, test, design, and application for aero propulsion control system

    模擬技術是航空推進控制系統研究、試驗、設計和使用中的一項極為重要的技術。
  9. Development of simulation technology and its application in aero propulsion control system are introduced firstly, then the engineering design are carried out based on the concept design for monitoring system of the simulation test platform. starting with analysis of function requirement of the monitoring system, signal interface, resource configuring and monitoring software are designed

    論文首先介紹了模擬技術的發展以及在航空推進控制系統中的應用，接著對半物理模擬平臺的監控系統在概念設計的基礎上進行了工程化設計，從監控系統功能需求分析入手，設計了監控系統的信號介面、資源配置以及監控軟體。
  10. The loosing control by their governments in today ' s globalization is a globe trend, and the alliance among those airlines, airline net optimize, code share technology could let them enter into their target market with lower cost through their partner ' s surplus resource without broken the government control, then the great repay to their shareholders. to most of aero corporate, they could make furthest profits via the maximized revenue for the cost stability

    近20年來的全球航空業發展歷程告訴我們，民用航空業放開管制已是大勢所趨、全球企業間戰略聯盟方興未艾、各大航空企業集團的航線網路正不斷優化、航空公司之間的代碼共享使得航空公司得以繞開各國政府的航權管制利用對方剩餘資源低成本進入目標市場，嶄新的收益管理技術則為各大航空公司迅速發展提供了巨大而穩定的現金流量支持，同時為股東們帶來了巨額的回報。
  11. In the matter - in - loop simulation experiment of aero - engine control system, the turbine outlet temperature, which characteristics with high and quick change, is hard to be simulated

    航空發動機控制系統半物理模擬試驗中，渦輪出口氣體溫度高、變化快，難以模擬。
  12. Based on this scheme, the control system architecture is designed. based on this system ’ s necessary, the signal conditioning interface box is designed, it is used in the conditioning of sensor and the design of drive circuit, the software of controller is also developed, finally, the performance index of controller is validated by a closed - loop simulation test system with aero - engine model and digital controller

    根據此方案，確定了模擬平臺中控制系統的體系結構，根據系統的需要，設計了信號調理介面機箱，實現了對傳感器信號的調理及驅動電路的設計，並進行控制器軟體的開發，最後利用發動機數學模型和數字電子控制器組成閉環模擬環境，以驗證控制器的各種性能指標。
  13. Self - adapting structure for the aerodynamic control, which arrayed by a lot of the same mems devices, became the important issue in the aero - mems field

    將許多相同的mems器件組成陣列，構成自適應結構控制飛機氣動性能已成為mems研究在航空領域的主要發展方向之一。
  14. The characters of bank - to - turn control technology determine that the btt missile ' s mathematical model having kinematical coupling, aero dynamical coupling, inertial coupling and control coupling. so the widely used stt missile ' s autopilot, which is designed to be three - channel independent ca n ' t meet the btt missile ' s control need

    Btt控制技術的控制特點決定了btt導彈的數學模型存在運動學耦合、氣動耦合、慣性耦合和控制耦合等多種耦合因素，因此目前側滑轉彎（ stt ）導彈廣泛採用的自動駕駛儀三通道獨立設計方法已不能滿足btt導彈控制系統的設計要求。
  15. Abstract : the paper presents the development and applications of thermal barrier coating, seal ( clearance control ) and wear resistance coating for aero gas turbine engine

    文摘:介紹了在現代航空燃氣渦輪發動機上熱噴塗熱障、封嚴、耐磨塗層的開發應用實例。
  16. The results indicates that the fuzzy control and moga has wide prospect in the aspect of control of the aero - engine

    研究結果表明，模糊控制以及多目標遺傳演算法在航空發動機控制中具有廣闊的應用前景。
  17. In this dissertation, the basic theory, and its applications in aero - engine control system design of fuzzy control, fuzzy pid control, and moga is studied

    本文對模糊控制、模糊pid控制和多目標遺傳演算法的基本理論以及在航空發動機控制系統中的應用進行了較為全面的研究。
  18. Aero - engines are developing in the miniaturization, totalization, high performance, and high dependability direction. distributed control will become the important and promising direction of aero - engine control

    航空發動機控制正在向小型化、綜合化、高性能、高可靠性方向發展，分散式控制系統是一個很有前途的新型控制系統。
  19. Combined with the self - designed project of shanghai ground transportation center - wind tunnel center, we bring out some methods to study and control aero - acoustic noise accompanying with wind tunnel experiments, these conclude some successful experiences of foreign countries and we also developed some self - designed ways to supervise our experiments, and especially we point out some difficulties during the experiments

    結合上海地面交通工具風洞中心的自主設計項目，提出了風洞設計中氣動聲學噪聲的研究和控制路線，既包括了國外一些成功的經驗，也提到了自行設計試驗的方案的思路，以及自主開發所需要涉及的一些難點。
  20. In order to be pull into practice use in engineering application, a real time emluator of the the closed - loop control system for the x - model aero - engine acceleration process has been established through combining the engine model and the controller model. the sqp ( sequential quadratic programming ) is used to get the optimal acceleration process result for the x - model aero - engine

    為了達到工程上實用的目的，在對某研究所提供的某型發動機實時模型作了詳細分析並進行了加速過程的模擬計算后，本文將控制器模型和發動機模型聯立在一起，構成了閉環形式的發動機加速過程實時模擬計算模型。
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