核發動機 的英文怎麼說
中文拼音 [héfādòngjī]
核發動機
英文
atomic propulsion nuclear engine-
Flight training pilot license, flight training night rating, flight training imc rating, flight training multi - engine rating, flight training seaplane rating, flight training mountain flying, flight training helicopter, aircraft hire, aircraft charter, pleasure flying, aerial photography, banner towing
飛行員取得執照的飛行培訓，提供夜間培訓、 imc核定分級、多發動機培訓、水上飛機培訓、山間飛行培訓、直升機培訓及包機培訓等。The experimental results indicate that this primary module of an electronic aeroengine controller is viable
試驗結果表明，本文設計的基於dsp和can總線的航空發動機電子控制器核心模塊是可行的。In terms of the control object and the principles of the test - bed of lubricating oil system for aeroengine, the core of which is plc ( progmammable logic controller ) and also use the upper computer and the lower computer as the structure and the overall design ideals of the compute control system
論文結合某型航空發動機滑油系統試驗臺的工作原理和控制目標，提出了該滑油系統試驗臺以plc （ programmablelogiccontroller ，可編程邏輯控制器）為核心的採用上、下位計算機結構的控制系統的結構和總體設計方案。At the same time, we improved a two - stroke fueled engine 1e40fm into the one also using the direct injection of liquid petrol gas. the electronic control system is developed whose core is m68hc11 single - chip computer which is produced by motorola ltd., and matched by other electronically - controlled circuits
開發了以motorola公司生產的8位增強單片機m68hc11為核心，配以相應的外部電路構成摩托車發動機單片機控制系統，並以一臺二沖程1e40fm型化油器式汽油機為對象，將其改造為汽油、電控氣體噴射兩用發動機。According to the jet theory and the characteristics of the flow, the flow can be divided into 6 zones : supersonic core zone, supersonic mixing zone, subsonic mixing zone, secondary flow zone and expanding zone. the rules to distinguish these zones were established. 2
根據射流理論及引射流動特點，將引射流場結構劃分為超聲速核心區、超聲速混合區、亞聲速混合區、支板背壁迴流區、二次流流動區以及發動機後部膨脹區，並確定了各區域準確劃分的原則。Finally, by practical test, experimental data obtained show that the dynamic thrust measuring system is dramatically available and successful. especially, it shows that when the impulse width is 20ms and the duty ratio is 1 : 3, the measured results are stable and reliable. hence, the system designed here can meat the test requirements of the actual applications, and the technology studied in the thesis also give a good foundation to future research work
最後，系統建成以後，通過多次調試試車、考核試車和實際型號試車的考核，試車結果表明，該系統的設計是成功的，動態推力數據穩定、可靠，可滿足發動機以20ms脈寬工作，占空比為1 : 3的情況下，進行發動機的動態推力性能指標測試，滿足實際應用的需求，為進一步進行動態推力測試技術研究奠定了良好的基礎。Thus the safe and reliable operation of the aeroengine, which supplies the major motive power to the modern aircraft, plays undoubtedly the first important role in this field ; and accordingly the status inspection of the aero - engine operation and the fault diagnosis technology have become the research focuses during the recent years
安全是現代航空工業尤其是民航運輸工業的首要要求，而作為現代飛行器的動力核心，航空發動機的安全、可靠運行則是重中之重，因此，航空發動機運行狀態監測與故障診斷技術也就成為當今的研究熱點。Then, the idea of integrating the standard configurable modules to building the basic model universal ats is brought forward, and the basic model universal ats fitting the rocket engine ground test is built by using the scheme of “ vxi ( or pxi ) and plc ”
將基本型通用ats應用到不同類型的固體火箭發動機、燃氣發生器和壓力恢復系統地面試驗中。經過近千次試驗考核，系統滿足試驗需求，達到了預期設計目標。試驗驗證了開放式柔性ats體系結構的合理性和基本型通用ats設計的可行性。Responsibility for product auditing engine assembly and adjustment
實施發動機裝調質量的產品審核。The prototype death star was never intended to be a practical weapon of war, so there was no need to install the maintenance and repair machinery, the immense computer core, or the hyperdrive engines that took up a huge amount of space in the actual death star space station
由於本身從來沒有被認為將成為一個可操作的戰爭武器，因而也沒有必要把在實際使用的死星空間站上佔去很大空間的那些維護修理機械、巨大的核心電腦和超空間驅動發動機安裝在死星原型上。The motor firing test with success met the design requirement for the motor
經地面熱試車考核，發動機性能滿足設計要求。With the development of morden aero - propulsion system, the simulation technology has became one of the most important means in aeroengine design. aeroengine nonlinear mathematical models, as the basis of engine performance simulation, are not convergence favorably in entire flight scope, because of the solution limitations of nonlinear equation and the engine balance equations
作為數值模擬的基礎與核心，目前廣泛應用的發動機非線性數學模型，由於平衡方程各種迭代解法與模型中非線性方程解法的不足，因而從根本上沒有解決模型在整個包線范圍內的收斂問題，極大地制約了發動機數值模擬技術的發展。The factors that have effect on the car ' s emission such as cleaning inside engine, size of three - way catalytic converter and leakage of exhaust system etc have been tested and analyzed, and some related parameters are determined. in order to ensure that the emission meets the requirements of the euro ii standard at one time, to pass the examination of 80000km durability, and to achieve excellent performance indicator while assuring the emission requirements, the design of intake manifold and camshaft profile is optimized, the test of engine performance and car ' s emission and environment performance have been conducted. through comparison by test, it is shown that the carburetor engine after retrofitting to electronic fuel injection engine has achieved good level in terms of emission and performance, and has been upgraded to the same level as the engine of japan mitsubishi and suzuki
為了滿足國家環保法規不斷提高的要求，本文對化油器式發動機改造成電控燃油噴射式發動機進行了研究與開發；確定了工程方案和開發目標；對機內凈化、三元催化器體積、排氣系統漏氣等對整車排放的影響進行了試驗和分析，確定了相關參數；為了確保對整車排放的影響進行了試驗和分析，確定了相關參數；為了確保排放一次通過歐標準，並完成8萬公里耐久性考核，在確保排放的同時達到良好的性能指標，對進氣歧管、凸輪軸型面的設計進行了優化；並進行了發動機性能測試，整車排入測試和環境性能測試。Since delays are often encountered in engineering systems, ecology systems, electricity systems, management systems and control systems such as the turbojet engine, microwave oscillator, nuclear reactor, controlability of systems and optimal control, etc. the phenomena of delays are investigated by more and more scientists
在工業工程、生態系統、電力系統、管理系統、控制系統等實際系統中常常遇到很多時滯問題，如渦輪噴氣發動機、微波振子、核反應、系統的可控性和最優控制等問題，所以時滯現象越來越受到眾多科學家的廣泛關注。This controlling way can make the passengers feel much comfortable and make the bus air - conditions work with a high efficiency. in this thesis, a single - chip microcomputer fuzzy controlling system with mcu : at89c51 is designed to deal with the bus whole air - condition composed with refrigerating system and heating system. via controlling the open of temperature door, turnaround speed of evaporator fan and subsidiary engine, it can control temperature of railway carriage
本論文針對獨立式全空調型（完全合一型）客車空調系統，設計了一個以at89c51為核心的採用模糊控制演算法的嵌入式單片機控制系統，通過控制溫度門的開口角度、蒸發器風扇的轉速、輔助發動機的轉速來控制車廂內的溫度，通過壓縮機的開、停對蒸發器除霜，系統具有溫度顯示、用戶設定的分擋多級溫度控制、在線控制參數修改等功能。This paper introduces the process of constructing a primary module based on dsp and can - bus for an electronic aeroengine controller, and the feasibility of the module is validated by experiments of matter - in - loop simulation
本文研製了一種基於dsp和can總線的航空發動機電子控制器核心模塊，並通過實物在迴路模擬試驗驗證了其可行性。The paper firstly analyzes the characteristics and demands of an electronic aeroengine controller, as a result, the design scheme of a primary module, which is based on dsp and can, is proposed for an electronic aeroengine controller. then, according to this scheme, a primary module is implemented by hardware design and software development. finally, a wpa aeroengine mathematical model is used to construct a matter - in - loop simulation system, with which a series of control system experiments are accomplished
論文首先分析了航空發動機電子控制器的特點，提出基於dsp帶can總線介面的航空發動機電子控制器核心模塊的設計方案；然後根據此方案，通過硬體電路的設計和軟體開發，實現了該核心模塊；最後利用渦噴a發動機的數學模型構成一個實物在迴路模擬試驗系統，並完成了模擬試驗。Responsibility for engine assembly cleanliness auditing
實施發動機總成清潔度的產品審核。Automatic mechanical transmission as so called amt, accomplishes automatic gearshift based on manual fixed - shaft and dry clutch, which takes ecu as kernel, and then uses hydraulic system to control clutch, gearshift and manipulates throttle by adopting electronics technique and automatic gearshift theory
電控機械式自動變速器（ amt ）是在傳統固定軸式變速器和乾式離合器的基礎上，採用電子技術和自動變速理論，以電子控制單元為核心，通過液壓執行系統控制離合器的分離與接合，選換檔操作以及發動機節氣門的調節來實現起步、換檔的自動操縱。The technology of full authority digital electronic control is a trend of aeroengine control, and the electronic controller is the primary part in an aeroengine control system
採用全權限數字式電子控制技術是航空發動機控制的一種發展趨勢，電子控制器是控制系統中最核心的部分。分享友人