?airfoil

airfoil發(fā)音

英：[?e?f??l]　　美：[??r?f??l]

英：　　美：

airfoil中文意思翻譯

n. 機翼；螺旋槳

airfoil常見(jiàn)例句

1 、an airfoil mounted on the rear of a car to reduce lift at high speeds.───安裝在汽車(chē)尾部的高速行使中減少升力的螺旋槳。

2 、Adaptive airfoil with shape memory alloys───帶有形狀記憶致動(dòng)器的自適應機翼

3 、My seat near the airfoil, Java is over there.───今次坐機翼位，下面是爪哇島。

4 、As design studies progressed it was found that several airfoil shapes could be used to satisfy the new performance criteria.───當進(jìn)行設計的研究工作后，發(fā)現有幾種翼型可以用來(lái)滿(mǎn)足新的性能指標。

5 、Research on the Airfoil of Multi-blade Centrifugal Fan───多翼離心通風(fēng)機葉片翼型的研究

6 、When I was in seventh grade, my father invented an airfoil.─── 我七年級的時(shí)候 我爸發(fā)明了一個(gè)機翼翼型

7 、Two pieces of foam are sandwiched onto the center piece and sanded to an airfoil shape.───兩件是泡沫夾心到中心片和磨光的機翼形狀。

8 、The flowfield around an airfoil with a spoiler is numerically simulated in a time-accurate manner using a 2D compressible Navier-Stokes solver.───基于2D可壓N-S方程,對帶擾流板的翼型繞流流場(chǎng)進(jìn)行非定常數值模擬。

9 、two-dimensional airfoil model───二元機翼模型

10 、Software for cascade airfoil design using aerodynamic hybrid method───葉型氣動(dòng)設計的雜交型方法計算軟件

11 、THE PIV EXPERIMENTAL RESEARCH TO INCREASE THE LIFT COEFFICIENT OF WINID TURBINE BLADE AIRFOIL───振蕩射流提高風(fēng)力機葉型升力的PIV實(shí)驗

12 、In addition to JTB series Roots blower, our company also produces and sales low-noise DT tank centrifugal fan, T35/BT35, T30 axial fans, CF more airfoil centrifugal fan and axle roof ventilator.───我公司除生產(chǎn)銷(xiāo)售JTB系列羅茨風(fēng)機外，同時(shí)還生產(chǎn)銷(xiāo)售DT低噪聲柜式離心風(fēng)機、T35/BT35、T30軸流風(fēng)機、CF多翼型離心通風(fēng)機及DWT型軸流式屋頂通風(fēng)機等。

13 、STUDY ON PERFORMANCE OF AIR-FLOW MEASURING DEVICE WITH MULTI-DUCT AIRFOIL PROFILE───多風(fēng)道翼型測風(fēng)裝置性能研究

14 、By using the Baldwin-Lomax turbulent model, the formation of the leading edge separation bubble, as well as the convection of vortex along the airfoil surface and unsteady phenomena of vortex are simulated at high angle of attack.───應用BaldwinLomax湍流二層代數模型模擬了大攻角時(shí)前緣分離渦的形成,旋渦對流及其非定?，F象。

15 、Numerical Simulation of the Flowfield of an Airfoil with Spoiler───帶擾流板翼型的流場(chǎng)數值模擬

16 、Unsteady Flow Around Airfoil with a Rapidly Deploying Spoiler───擾流片快速張開(kāi)誘發(fā)的非定常流動(dòng)研究

17 、A new approach to modeling the unsteady rotor aerodynamic forces is established based on the insight into the nonuniform induced velocity distribution,inflow dynamics and unsteady airfoil behavior.───在考察非均勻誘速分布、入流動(dòng)力學(xué)和非定常翼型性能的基礎上，建立了一種模擬非定常旋翼氣動(dòng)力的新方法。

18 、It is one of approaches for unsteady inverse problems of oscillating airfoil to solve unsteady Bluer equations with finite difference method.───利用有限差分法解非定常歐拉方程是振蕩機翼非定常氣動(dòng)反問(wèn)題的一種求解方法。

19 、Scanlan, R.H., and Tomko, J.J., (1971) “Airfoil and bridge deck flutter derivatives,” Journal of the Engineering Mechanics Division, ASCE, 97(EM6), 1717-1737.───姚忠達、楊永斌，(2000)，高速鐵路車(chē)-橋互制理論，圖文技術(shù)服務(wù)有限公司。

20 、Bifurcation of Motions of an Airfoil in Incompressible Flow───不可壓縮流中二元翼運動(dòng)的分支問(wèn)題

21 、Genetic Algorithms for Airfoil Optimization Using Euler Equation Solver───基于Euler方程的翼型優(yōu)化設計高效基因算法研究

22 、Inverse design of airfoil based on variable-domain variational FEM───基于變域變分有限元的翼型反設計

23 、flow past a two-dimensional airfoil───二維翼型繞流

24 、Sidewall Effects and Suction Technique in Two-Dimensional Transonic Airfoil Wind Tunnel Test───二元翼型風(fēng)洞的側壁干擾與抽氣研究

25 、A slightly arched surface, as of a road, a ship's deck, an airfoil, or a snow ski.───弧面稍呈弧形的表面，如路面、船甲板、機翼面或滑雪板

26 、The results detected the surface boundary layer transition positions by three techniques were excellent identical for two dimensional NACA-0012 airfoil model.───對二元NACA-0012翼型表面邊界層轉捩點(diǎn)位置測量，三種方法都給出了相吻合的結果。

27 、The analytical results showed that Reynolds number and Mach number have a rather obvious effect on airfoil aerodynamic performances.───分析結果表明：雷諾數和馬赫數對翼型氣動(dòng)性能有較大的影響。

28 、MULTIOBJECTIVE OPTIMIZATION DESIGN OF A COMPRESSOR AIRFOIL USING EVOLUTIONARY ALGORITHMS───基于進(jìn)化算法的壓氣機葉型多目標優(yōu)化設計

29 、The advantages of FRP over other material, the rapid development of FW technology and the wide use of computer technology establish solid matter and technology foundation for the airfoil FW moulding.───FRP的優(yōu)越性能、FW技術(shù)的迅猛發(fā)展以及計算機技術(shù)廣泛的應用為機翼的FW成型奠定了物質(zhì)和技術(shù)基礎。

30 、NUMERICAL SIMULATION OF VISCOUS FLOW FOR MULTI-ELEMENT AIRFOIL USING MULTI-BLOCK GRIDS───多段翼型粘性繞流多塊網(wǎng)格數值模擬

31 、The Effects of Elastic Vibration on the Flow Field near Stall-incidence of the Airfoil───彈性振動(dòng)對翼型失速迎角附近流場(chǎng)的影響

32 、A method has been derived for the determination of the downwash in the field of an airfoil extending through a circular jet.───對于采用鋼橋面板系統做為主梁之細長(cháng)型橋梁系統而言，往往采用側向支撐系統以提高鋼橋面板及主梁之抗扭轉勁度。

33 、High efficient evolutionary algorithms for multi-criteria optimization of multi-element airfoil in aerodynamics───多段翼型氣動(dòng)力優(yōu)化設計的多標準高效進(jìn)化算法

34 、The flow fields of an airfoil and simplified aircraft are calculated parallelly under MPI/PVM environmcent.───在MPI／PVM環(huán)境下用分區方法作了二維翼型和三維機翼繞流的并行計算。

35 、Incremental Harmonic Balance Method for Airfoil Flutter With Multiple Strong Nonlinearities───多自由度強非線(xiàn)性顫振分析的增量諧波平衡法

36 、Analysis of Bifurcation of an Airfoil with an External Store in Incompressible Flow───不可壓縮流中機翼**系統的分叉分析

37 、How does the brake act on the paraglider airfoil?───剎車(chē)是如何作用于滑翔傘的翼型?

38 、Finally the flow over two-element airfoil iscalculated.In the process of solving RANS equations, pressure-velocity coupling ishandled by using of SIMPLE algorithm.───在求解雷諾平均N-S方程的過(guò)程中，壓力和速度的耦合是通過(guò)SIMPLE壓力修正算法來(lái)實(shí)現的。

39 、The wake survey cannot be used to measure the drag of stalled airfoil or of airfoils with flaps down.───尾流測量不能用來(lái)測量失連狀態(tài)下的冀型或襟翼偏轉后的翼型阻力。

40 、TWO DIMENSIONAL SIMULATION OF THE TRANSONIC FLOW OVER NACA 0012 AIRFOIL───二維翼型跨音速繞流的數值模擬

41 、Experimental investigation of aerodynamics performance of multi-element airfoil with leading-edge slat───帶縫翼多段翼型氣動(dòng)特性的實(shí)驗研究

42 、Numerical Investigation of Unsteady Flow on Airfoil with a Spoiler───帶擾流片的二維翼型非定常計算及分析

43 、Somers,D.M.Design and experimental results for a natural-laminar-flow airfoil for general aviation applications.NASA TP 1861.June 1981.───華漢金.翼剖面優(yōu)化理論在螺旋槳設計和減荷切削中的應用.船舶工程,2002(6).

44 、The bionic model could reduce air noise because the non-smooth shape has the characteristic of rectify flow around the airfoil and the control the turbulent breakaway .───仿生前緣非光滑形態(tài)具有整流及控制氣流分離的特性，可減少由于翼表面氣流壓力脈動(dòng)及渦流脫離引發(fā)的氣流噪聲。

45 、PATRAN and the process in developing load module of airfoil FEM.───PATRAN進(jìn)行二次開(kāi)發(fā)程序編制的方法,以及開(kāi)發(fā)機翼有限元模型加載模塊的過(guò)程,為在msc.

46 、Design of a Sine Driving Mechanism for the Dynamic Experiment of the Airfoil Model───一種用于翼型動(dòng)態(tài)實(shí)驗的正弦驅動(dòng)機構設計

47 、Provide an airfoil at the sill of the sash opening.It shall be mounted to provide a 1 inch slot above the hood interior counter top.───開(kāi)口拉門(mén)處有一個(gè)翼面，安裝時(shí)應在內部臺面上留有1英寸的狹縫。

48 、Calculation of lift-drag characteristics of OAF and NACA63a312 airfoil at low speed using Jameson/TVD mixed scheme was carried out.───以Jameson/TVD混合格式對低速時(shí)的OAF和NACA63a312翼型的升阻特性進(jìn)行了計算。

49 、Effect of Gurney flaps on aerodynamical characters of single airfoil───Gurney襟翼對單段翼型動(dòng)態(tài)氣動(dòng)特性的影響

50 、The ideal curvature in front part of designed blade may reasonably form shock position, so the shock loss is reduced greatly.Two kinds of airfoil are modified by means of this new method.───葉型入口段理想的曲率分布可以合理組織進(jìn)口激波結構和位置，大幅降低激波損失。

51 、Optimization Design of a High-Lift Airfoil at Low Reynold Numbers Based on Genetic Algorithm───基于遺傳算法的低雷諾數高升力翼型的優(yōu)化設計

52 、To put the method in some perspective, it helpful to briefly outline the two general approaches to airfoil design.───把一些觀(guān)點(diǎn)方法,它有助于扼要介紹兩個(gè)一般方式翼型設計.

53 、A small moveable airfoil on the side of the fuselage transmittng airplane angle relative to airstream for the stall warning system.───位于機身側的可動(dòng)小翼面，為失速警告系統傳輸飛機對氣流的相對角度。

54 、Airfoil flutter is one of the important problems in aeroelasticity.───在氣動(dòng)彈性力學(xué)中,機翼振顫是一個(gè)非常典型的問(wèn)題。

55 、An unstructured grid was applied to the zone near the iced airfoil, whereas a structured grid was applied to save the storage and computational time.───在靠近積冰邊界的內層采用了非結構網(wǎng)格，在非結構網(wǎng)格外采用結構化網(wǎng)格以節省存儲空間和計算時(shí)間。

56 、Application of Hybrid Grid to Analyzing Complex Iced Airfoil Aerodynamic Performance───應用混合網(wǎng)格分析復雜積冰翼型氣動(dòng)性能

57 、a hinged airfoil on the upper surface of an aircraft wing that is raised to reduce lift and increase drag───在飛機機翼上方的用來(lái)增加浮力減少拉力的裝置

58 、It appears that using NLF airfoil section can get a better aerodynamic efficiency and self-starting capability.───實(shí)驗結果還表明，采用自然層流翼型的斜 軸式風(fēng)力機比采用普通翼型的斜軸式風(fēng)力機具有更好的氣動(dòng)效率和起 動(dòng)能力。

59 、Thus, it would be more advantageous to specify the velocity distribution from the outset and from that determine the airfoil shape.───因此,它會(huì )更有利,指明速度分布,從一開(kāi)始就確定,從機翼形狀.

60 、In this regard, several airfoil templates are given based on existing designs, eg, the SD7037 airfoil and others.───在這方面,有幾個(gè)版本,基于現有翼型設計,例如,sd7037翼型等.

61 、With the application of the above models, we research the influence of ground-effect on the flow near the surface of airfoil, the pressure distribution, and the moving of the vortices in the wake.───利用上述模型研究了地面對翼型表面流動(dòng)和壓力分布的影響，并對有地面存在條件下的尾渦發(fā)展規律進(jìn)行了討論。

62 、Near the midchord, the suction can provide a higher lift force for the airfoil.───吸氣孔位置在翼面的中部附近增升效果較好;

63 、Studies on Sidewall Effects in Two-Dimensional Airfoil Testing───二維翼型實(shí)驗的側壁影響研究

64 、A rotating airfoil on the tail of a single-rotor helicopter,keeps the helicopter from spinning in the direction opposite to the rotation of the main rotor.───單轉子直升飛機尾部上的旋轉機翼，防止直升飛機的旋轉方向與主轉子相反。

65 、Aeroelastic Analysis of a Two-Dimensional Airfoil with Control Surface Freeplay Nonlinearity───具有操縱面間隙非線(xiàn)性二維翼段的氣動(dòng)彈性分析

66 、Transonic Euler Equation Airfoil Aerodynamic Optimization Based on Genetic Algorithms and Game Theory───基于基因算法與博奕論的翼型跨音速Euler方程氣動(dòng)優(yōu)化

67 、AN INVESTIGATION OF AIRFOIL FLUTTER CHARACTERISTICS WITH STRUCTURE NONLINEARITY AT TRANSONIC SPEED───帶有結構非線(xiàn)性的跨音速翼型顫振特性研究

68 、Adverse Lift on Airfoil with a Rapidly Deploying Spoiler───擾流片快速張開(kāi)誘發(fā)的非定常升力過(guò)沖

69 、Aerodynamic Properties of Circulation Control Airfoil with Multi-Slot Blowing───多噴口環(huán)量控制翼型流動(dòng)的研究

70 、Starting with airfoil 2, the pitching moment is increased from -.15 to -.25 to provide more aft loading and aft camber.───從翼型2俯仰時(shí)刻由原來(lái)的15年至今25年至今,以提供更多后部后部拱落.

71 、3 Multi-objective optimization design of airfoil and wing,───5簡(jiǎn)化自適應機翼的氣動(dòng)外形優(yōu)化設計

72 、Aerodynamic Optimization Design of Cascade Airfoil Using Hybrid Evolutionary Algorithms───應用復合進(jìn)化算法的葉柵氣動(dòng)優(yōu)化設計方法的研究

73 、Rogue Amoeba today announced the release of Airfoil 3.3.───仿生學(xué)單細胞蟲(chóng)今天宣布發(fā)型了3.3版機翼。

74 、The challenge of adequately cooling the nozzle guide vane directly downstream of the combustor is compounded by a complex vortical secondary flow at the junction of the endwall and the airfoil.───為了使空氣在管道中能克服更大的阻抗，本研究設計管道風(fēng)扇出口導流葉片，試圖將流出葉輪之流體由迴旋流動(dòng)導為直接流出風(fēng)機，以達到提升風(fēng)機性能的目的。

75 、Visbal, M.R. and Shang, J.S., "Numerical Investigation of the Flow Structure Around A Rapidly Pitching Airfoil," AIAA Paper 87-1424, June. 1987.───劉泰然,"次音速非均勻流對二維翼剖面流場(chǎng)的影響"成功大學(xué)航太所碩士論文,1999年六月。

76 、The thickness ratio appeared to have little effect on lift coefficient at zero angle of attack, since the angle of zero lift was largely determined by the airfoil camber.───在迎角為零時(shí)，由于零升力主要由機翼中弧線(xiàn)決定，相對厚度對升力幾乎沒(méi)有影響。

77 、Optimization Design of Airfoil Based on Hybrid Genetic Algorithm and Compound Form Method───基于混合遺傳算法和復合形法的翼型優(yōu)化設計

78 、Hierarchial Evolutionary Algorithms and Its Application in Transonic Airfoil Optimization in Aerodynamics───分級型進(jìn)化算法及其在翼型跨聲速氣動(dòng)優(yōu)化中的應用

79 、Mean geometric chord of airfoil───平均幾何弦長(cháng)

80 、The problem of unsteady separated flow of rapidly pitching airfoil with oscillating motion is computationally studied.───對帶振蕩的快速上仰翼型的非定常分離流問(wèn)題進(jìn)行了計算研究。

81 、In this paper, the optimization design of the transonic airfoil is performed by the Response Surface Methodology(RSM).───基于響應面方法進(jìn)行了跨聲速翼型的氣動(dòng)優(yōu)化設計。

機務(wù)工作常用英語(yǔ)

機務(wù)工作常用英語(yǔ)

　機務(wù)朋友們，看完之后要好好學(xué)習，為祖國現代化做貢獻。下面是我為大家帶來(lái)的關(guān)于機務(wù)工作常用英語(yǔ)的知識，歡迎閱讀。

　機務(wù)實(shí)用英語(yǔ)詞匯

　輪檔擋好-- Chocks in

　地面電源設備接好--Ground power connected

　收到-- Roger

　現在關(guān)閉發(fā)動(dòng)機--Shutting down engines

　準備牽引-- Ready for pushback

　所有艙門(mén)已關(guān)好--All doors checked closed >松剎車(chē)-- Brakes off 松剎車(chē)-- Release parking brakes

　剎車(chē)已松-- Brakes off

　剎車(chē)已松-- parking brake Released

　可以牽引 --Clear for pushback

　23號跑道起飛--Runway( or face)two three

　05號跑道起飛--Runway( or face)zero five

　牽引完成 --Pushback complete 剎車(chē) --Brakes on

　剎車(chē) --Set parking brake 剎車(chē)剎好 --Brakes on

　剎車(chē)剎好-- Parking brake set

　準備啟動(dòng)1(或2)號發(fā)動(dòng)機--Start number one(or two)

　可以啟動(dòng)1(或2)號發(fā)動(dòng)機--Clear number one(or two)

　已經(jīng)供氣(如需氣源車(chē))--Pressure on

　啟動(dòng)結束 --Start complete

　斷開(kāi)地面設備-- Disconnect ground equipment

　**銷(xiāo)移開(kāi) --Ping Removed

　稍等 --Standby

　Air Conditioning System (空調系統)

　PACK空調主件

　HOT BLEED AIR熱引氣

　OUTLET DUCT外流管

　BYPASS VALVE旁通活門(mén)

　RAM AIR 沖壓空氣

　INLET SCOOP 進(jìn)氣口

　TRIM AIR VALVE 調節空氣

　PACK FLOW SWITCH空調主件流量

　EXTRACTOR FAN 排氣風(fēng)扇

　GUARDED FLAP 有保護蓋的導片

　ISOLATION VALVE 隔離活門(mén)

　“LIGHT OUT”AUTO POSITION “燈滅”自動(dòng)狀態(tài)

　BLOWER 鼓風(fēng)機

　EXTRCTOR排風(fēng)扇

　OVERBOARD 機外

　ONBOARD機上

　OPEN-CIRCUIT開(kāi)路

　CLOSED-CIRCUIT閉路

　CONFIGURATION 形態(tài)

　PASSENGER LOAD乘客載荷

　DOWNSTREAM下游

　STANDING WATER積水

　ATLN(ALTERNATE)備份

　CHANNEL通道

　PNEUMATIC氣源

　DUAL 雙的

　SWITCH OVER交換

　PRE-COOLER預冷機

　COOLANT冷卻劑

　AMBER琥珀色

　VENTILATION通風(fēng)

　CIRCUIT BREAKER跳開(kāi)關(guān)

　PRESSURIZATION (增壓)

　FLAPPER VALVES 瓣狀活門(mén)

　PROFILE 剖面

　TOGGLE 扳鈕開(kāi)關(guān)

　VACUUM 真空

　ISAO BARIC 等壓

　BAROMETRIC 氣壓

　PRESSURE DIFFERENTIALS 壓差

　ANEROID SWITCH 膜盒氣壓

　STBY (STANDBY)備份

　DC DIRECT CURRENCY 直流電

　PSI (POUND PER SQUARE INCH)磅/平方英尺

　DITCH 水上迫降

　SUPERCHARGER 增壓器

　INADVERTENT 偶然的

　LEAKAGE 漏、滲

　APRON 停機坪

　CEILING 頂板

　FREIGHT 貨機

　ACCESSORY 副件

　THROTTLE LEVER 油門(mén)桿

　CRUISE 巡航

　NEGATIVE RELIEF VALVE 負壓釋放活門(mén)

　POSITIVE PRESSURE 正壓

　AIRPORT ELEVATION 機場(chǎng)標高

　AUTOPILOT(自動(dòng)駕駛)

　MOMENTUM 動(dòng)量

　MIMICKING 模仿

　GLARE-SHIELD 遮光板

　ACTUATORS 制動(dòng)器

　SURVEILLANCE 監視

　TRAJECTORY 軌跡

　QUADRANT 油門(mén)操縱桿

　FLEX(FLEXIBLE)靈活的

　MCT(MAXIMUM CONTINUE THRUST) 最大連續推力

　ELEVATORS 升降舵

　AILERON 副翼

　NAVAID 助航

　SID(STANDARD INSTRUMENT DEPARTURE) 標準儀表離場(chǎng)

　STAR(STANDARD TERMINAL ARRIVAL ROUTE)標準進(jìn)場(chǎng)程序

　MISSED APPROACH (GO AROUND) 復飛

　DYNAMIC 動(dòng)力的

　AUGMENTATION 增加、增益

　FLIGHT ENVELOPE 飛行包線(xiàn)

　CDU(CONTOL DISPLAY UNIT)控制顯示組件

　FMA(FLIGHT MODE ANNUNCIATOR)飛行方式顯示器

　ADIRS(AIR DATA AND INERTIAL REFERENCE SYSTEM)大氣數據及慣性基準系統

　MCP(MODE CONTROL PANEL)方式控制面板

　GPS(GLOBAL POSIITON SYSTEM)全球**系統

　FLARE 平飄

　TOUCHDOWN 接地點(diǎn)

　FLY-BY-WIRE 電傳操縱

　ACCELEROMETER 加速器

　ALIGNMENT 對準、校準

　SERVOMOTOR 伺服馬達

　GYROSCOPE 陀螺

　THRUST REDUCTION ALT 減推力高度

　REVERSE 反推

　ARM 預位

　FPA(FLIGHT PATH ANGLE)飛行航徑角

　LOCALIZER 航向道

　IDLE 慢車(chē)

　DETENT 卡位

　FPV(FLIGHT PATH VECTOR)飛行航徑矢量

　CRM(COCKPIT RESOURCE MANAGEMENT)駕駛艙資源管理

　PF(PILOT-FLIGHT)把桿飛行員

　PFD(PRIMARY FLIGHT DISPLAY)主飛行顯示

　PULLEY 滑輪 ROLL 滑跑

　SCROLL 翻動(dòng)、卷起

　SLEW 上下選頁(yè)

　VELOCITY 速度

　DATA BASE LOADER 數據庫裝載機

　ALPHA/NUMERIC KEY BOARD 字母/數字鍵盤(pán)

　SCRATCH PAD 草稿欄

　DYNAMIC AND BACKGROUD DATA 動(dòng)態(tài)和背景數據

　TROPOPAUSE 對流層頂

　CYAN 深藍色

　COST INDEX 成本指數

　ALIGNMENT 校準

　PROMPT 提示符

　EFOB(ESTIMATED FUEL ON BOARD) 預計機上燃油

　MAGENTA 品紅色、洋紅色

　EAT(ESTIMATED TIME OF ARRIVING)預計到達時(shí)間

　ADC(AIR DATA COMPUTER)大氣數據計算機

　CRT(CATHODE RAY TUBE)陰極射線(xiàn)管

　BITE (BUILD-IN TEST EQUIPMENT) 內裝測試設備

　DEFAULT 缺席

　LSK(LINE SELECT KAY)行選鍵

　ASYMMETRIC 不對稱(chēng)

　TERMINAL AREA 終端區域

　COORDINATE 經(jīng)緯度

　RNVA AREA NAVIGATION 區域導航

　EN-ROUTE 在航路上

　CFDS(CENTRALIZED FAULT DISPLAY SYSTEM)集中顯示系統

　COMMUNICATION (通訊)

　VIBRATIONS 振動(dòng)

　IMPULSES 脈沖

　ANTENNA 大線(xiàn)

　MEGAHERTZ 兆赫茲

　CURVATURE 彎曲 曲度

　IONOSPHERE 電離層

　TRANSCEIVER 無(wú)線(xiàn)電收發(fā)機

　RACK 設備架

　SQUELCH 靜噪、噪聲控制

　PASSENGER ADDRESS 旅客廣播

　CABIN INTEROHONE 客艙內話(huà)

　INTERPHONE 內話(huà)機

　EVACUATION 疏散

　ROTARY 旋轉的

　KNOB 旋鈕

　DEDICATED 專(zhuān)用的`

　BUZZER 蜂鳴聲

　BOOM SET 吊桿耳機

　HEAD SET 耳機

　SELCAL 選擇呼叫

　ACTIVE 正在使用

　HOT MIKE

　PRESS TO TALK (PTT)按下發(fā)話(huà)

　LATCHED 鎖住

　PREEMPT 優(yōu)先占有

　STUCK 阻塞

　PLUG **入

　STRAIN 濾網(wǎng)

　SHIELD 過(guò)濾

　ROCK SWITCH 搖式電門(mén)

　FLIGHT CONTROL SYSTEM(I)

　(飛行控制(一))

　REJECTED T/O 中斷起飛

　CONVENTIONAL 通用的

　WHEEL 駕駛盤(pán)

　COLUMN 駕駛桿

　PEDAL 腳蹬

　SURFACE 舵面

　RUDDER 方向舵

　SPEED-BRAKE 減速板

　FLAP 襟翼

　STAB TRIM 調整片

　OVERRIDE SWITCH 超控電門(mén)

　YAW DAMPER 偏航阻尼器

　CENTERING MECHANISM 定中機械

　SWEEP BACK 后掠

　SPOILER 擾流板

　JAM 卡阻

　ROLL 滾轉(橫滾)

　PITCH 俯仰

　STABILIZER 安定面

　YAW 偏航

　YAW DAMPER RATE GYRO 偏航率陀螺儀

　LONGITUDINAL AXIS 縱軸

　VERTICAL AXIS 垂軸

　LATERAL AXIS 橫軸

　ACTUATING CYLINDER 作動(dòng)筒

　FAIRED POSITION 中立位

　FALL INTO SPIN 進(jìn)入螺旋

　AIRFOIL 翼部面

　FLIGHT CONTROL SYSTEM(II)

　(飛行控制(二))

　SECONDARY FLIGHT CONTROL 輔助飛行操縱

　HIGH LIFT DEVICE 增升裝置

　TRAILING EDGE(TE)后緣

　LEADING EDGE(LE)前緣

　POWER TRANSFER UNIT(PTU)動(dòng)力傳輸裝置

　STALL 失速

　MANEUVER 機動(dòng)飛行

　INBOARD 內側

　OURBOARD 外側

　SLOTTED 開(kāi)縫的

　THREE SLOTTED FLAP 三開(kāi)縫襟翼

　DRAG 阻力

　COMPARATOR 比較儀

　ROLL RATE 滾轉率

　MIXER 混合器

　DEFLECTION 偏轉

　AERODYNAMIC MEAN CHORD 平均空氣動(dòng)力弦

　TORQUE 扭力

　JACK 千斤頂

　FIRE PROTECTION(I)

　(防火(一))

　FIRE PROTECTION 防火

　OVERHEAT 超溫

　FIRE DETECTION

　稍等啟動(dòng)-- Standby for start

　稍等推出-- Standby for pushback

　在左(或右)方打手勢--Hand signal on the left(or right)

　aircraft crew， air crew 機組， 機務(wù)人員

　pilot 駕駛員， 機長(cháng)

　co-pilot， second pilot 副駕駛員

　navigator 領(lǐng)航員

　steward 男服務(wù)員

　stewardess， hostess 空中**

　radio operator 報務(wù)員

　Bairliner 班機

　monoplane 單翼飛機

　glider 滑翔機

　trainer aircraft 教練機

　passenger plane 客機

　propeller-driven aircraft 螺旋槳飛機

　jet (aircraft) 噴射飛機

　amphibian 水陸兩用飛機

　seaplane，hydroplane 水上飛機

　turbofan jet 渦輪風(fēng)扇飛機

　turboprop 渦輪螺旋槳飛機

　turbojet 渦輪噴射飛機

　transport plane 運輸機

　helicopter 直升機

　supersonic 超音速

　hypersonic 高超音速

　transonic 跨音速

　subsonic 亞音速

　Airbus 空中客車(chē)

　Boeing 波音

　Concord 協(xié)和

　Ilyusin 依柳辛

　McDonald-Douglas 麥道

　Trident 三叉戟

　Tupolev 圖波列夫

　hatch 艙口

　aeroengine， air engine 航空發(fā)動(dòng)機

　navigation light 航行燈

　fuselage， body 機身

　nose 機頭

　wing 機翼

　aileron 副翼

　wing flap 襟翼

　tail plane 水平尾翼

　starboard wing 右翼

　port wing 左翼

　pilot"s cockpit 駕駛艙

　parachute 降落傘

　passenger cabin 客艙

　propeller 螺旋槳

　pressurized cabin 密封艙

　undercarriage 起落架

　undercarriage wheel 起落架輪

　elevator 升降舵

　radio navigation device 無(wú)線(xiàn)電導航設備

　radio directive device 無(wú)線(xiàn)電定向設備

　luggage compartment 行李艙

　(fuel) tank 油箱

　auxiliary (fuel) tank 副油箱

　main (fuel) tank 主油箱 autopilot 自動(dòng)駕駛儀

　ground crew 地勤人員

　airport 航空港， 民航機場(chǎng)

　airfield， aerodrome， airdrome 機場(chǎng)

　airport beacon 機場(chǎng)燈標

　airport meteorological station 機場(chǎng)氣象站

　main airport building， terminal building 機場(chǎng)主樓

　emergency landing runway， forced landing runway

　緊急著(zhù)陸跑道

　taxiway 滑行跑道

　runway 跑道

　omnirange radio beacon 全向式無(wú)線(xiàn)電航空信標

　fuel depot 燃料庫

　control tower 塔臺

　tarmac 停機坪

　radio beacon 無(wú)線(xiàn)電信標

　boarding check 登機牌

　plane ticket 飛機票

　flight， flying 飛行

　bumpy flight 不平穩的飛行

　smooth flight 平穩的飛行

　ramp 扶梯

　altitude， height 高度

　air route， air line 航線(xiàn)

　extra flight 加班

　economy class， tourist class 經(jīng)濟座

;

用英語(yǔ)介紹飛機

What is  aircraft?

An aircraft is a machine that is able to fly by gaining support from the air. It counters the force of gravity by using either static lift or by using the dynamic lift of an airfoil,or in a few cases the downward thrust from jet engines.

The human activity that surrounds aircraft is called aviation. Crewed aircraft are flown by an onboard pilot, but unmanned aerial vehicles may be remotely controlled or self-controlled by onboard computers. Aircraft may be classified by different criteria, such as lift type, aircraft propulsion, usage and others.

The history of  aircraft:

Flying model craft and stories of manned flight go back many centuries, however the first manned ascent – and safe descent – in modern times took place by larger hot-air balloons developed in the 18th century. Each of the two World Wars led to great technical advances. Consequently, the history of aircraft can be divided into five eras:

Pioneers of flight, from the earliest experiments to 1914.

First World War, 1914 to 1918.

Aviation between the World Wars, 1918 to 1939.

Second World War, 1939 to 1945.

Postwar era, also called the jet age, 1945 to the present day.

Impacts of aircraft use:

Aircraft permit long distance, high speed travel and may be a more fuel efficient mode of transportation in some circumstances. Aircraft have environmental and climate impacts beyond fuel efficiency considerations, however. They are also relatively noisy compared to other forms of travel and high altitude aircraft generate contrails, which experimental evidence suggests may alter weather patterns.

Uses for aircraft:

1. Military

A military aircraft is any aircraft that is operated by a legal or insurrectionary armed service of any type. Military aircraft can be either combat or non-combat.

2. Civil

Civil aircraft divide into commercial and general types, however there are some overlaps.

Commercial aircraft include types designed for scheduled and charter airline flights, carrying passengers, mail and other cargo. The larger passenger-carrying types are the airliners, the largest of which are wide-body aircraft. Some of the smaller types are also used in general aviation, and some of the larger types are used as VIP aircraft.

General aviation is a catch-all covering other kinds of private (where the pilot is not paid for time or expenses) and commercial use, and involving a wide range of aircraft types such as business jets (bizjets), trainers, homebuilt, gliders, warbirds and hot air balloons to name a few. The vast majority of aircraft today are general aviation types.

3. Experimental

An experimental aircraft is one that has not been fully proven in flight, or that carries an FAA airworthiness certificate in the "Experimental" category. Often, this implies that the aircraft is testing new aerospace technologies, though the term also refers to amateur and kit-built aircraft—many based on proven designs.

4. Model

A model aircraft is a small unmanned type made to fly for fun, for static display, for aerodynamic research or for other purposes. A scale model is a replica of some larger design.