The invention refers to an aircraft gas turbine engine including a core engine comprising at least a high pressure turbine and a downstream low pressure turbine a bypass duct surrounding the core engine as well as a mixer arranged in an inlet portion of the low pressure turbine into which a ...
压力比(EPR)仪表:Engine Pressure Ratio Gauge(用于涡喷/涡扇发动机) 压力比 = 涡轮排气口压力:压气机进气口压力 排气温度(EGT)仪表:Exhaust Gas Temperature Gauge 根据排气系统的不同位置,又细分为: 涡轮前温度(TIT)表:Turbine Inlet...
A turbojet is a type of gas turbine engine that was originally developed for military fighters during World War II. A turbojet is the simplest of all aircraft gas turbines. It consists of a compressor to draw air in and compress it, a combustion section where fuel is added and ignited, ...
1.TitleAircraftgasturbineenginepoweraugmentationorrestorationsystems maintenance 2.CodeEMAMBG417A 3.RangeMaintenanceofenginepoweraugmentationsystemsinanaircraft hangarorworkshopduringtheaircraftgroundedtime.Thisunitof Competencycoverswatermethanolordematerializedwaterinjection enginepoweraugmentationorrestorationsystems. 4....
Aircraft Gas Turbine one of the basic subsystems of an aircraft gas turbine engine. Aircraft gas turbines differ from stationary-plant gas turbines by their greater output combined with smaller size and smaller mass, which is achieved through design improvements, the high axial-flow velocities of ...
Aircraft GasTurbine Engine’s Control Based on (飞机GasTurbine引擎基础上的控制).pdf,11 Aircraft Gas-Turbine Engine’s Control Based on the Fuel Injection Control Alexandru-Nicolae Tudosie University of Craiova, Avionics Department Romania 1. Introducti
《航空发动机系列:航空燃气涡轮发动机控制》主要以大飞机用的航空燃气涡轮发动机为被控对象,以发动机全权限数字式电子控制(FADEC)为核心,阐述了发动机控制系统的基本原理、发展与展望;发动机建模;发动机稳态控制;发动机过渡态控制;发动机先进控制技术;发动机容错控制;发动机健康管理,并介绍了一种大飞机发动机典型控制系统。
1.TitleAircraftgasturbineengineavionicignitionsystemsmaintenance 2.CodeEMAMBX415A 3.RangeAircraftgasturbineignitionsystemsmaintenanceactivityisusually carriedoutontheaircraftinthehangar. 4.Level4 5.Credit2 6.CompetencyPerformanceRequirement 6.1Knowledge♦Understandtheoperationprinciplesofgas ...
5.An aircraft gas turbine engine as claimed in claim 4, further comprising the radially outer magnet rotor, the radially inner pole rotor, and the generator stator being concentric. 6.An aircraft gas turbine engine as claimed in claim 5, further comprising:the radially outer magnet rotor encircl...
A fan nacelle for an aircraft gas turbine engine. The nacelle includes an aft nacelle portion including a radially outer surface and a radially inner surface, the radially outer and