ofAn aircraft gas turbine engine is provided with a starting air turbine (50) that is directly connected through the starter gearbox (48) to the high pressure (HP) shaft (38) and is provided with a means to extract excess energy from engine compressor bleed air, return it to the engine,...
航空发动机系列:航空燃气涡轮发动机控制 [Aircraft Gas Turbine Engine Control] pdf epub mobi txt 电子书 下载 具体描述 内容简介 《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...
作者:Treager 出版年:1995-11 页数:677 定价:$ 163.00 ISBN:9780028018287 豆瓣评分 评价人数不足 评价: 写笔记 写书评 加入购书单 分享到 推荐 内容简介· ··· Aircraft Gas Turbine Engine Technology provides a comprehensive, easy-to-understand treatment of the background, development, and applications...
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...
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 ...
1.TitleAircraftgasturbineengineavionicignitionsystemsmaintenance 2.CodeEMAMBX415A 3.RangeAircraftgasturbineignitionsystemsmaintenanceactivityisusually carriedoutontheaircraftinthehangar. 4.Level4 5.Credit2 6.CompetencyPerformanceRequirement 6.1Knowledge♦Understandtheoperationprinciplesofgas ...
1.TitleAircraftgasturbineenginepoweraugmentationorrestorationsystems maintenance 2.CodeEMAMBG417A 3.RangeMaintenanceofenginepoweraugmentationsystemsinanaircraft hangarorworkshopduringtheaircraftgroundedtime.Thisunitof Competencycoverswatermethanolordematerializedwaterinjection enginepoweraugmentationorrestorationsystems. 4....
A gas turbine engine blade for aircraft which has a 3-dimensional blade surface shape twisted around a center line at an angle of 45 degrees or more and 70 degrees or less, wherein the aforementioned blade is provided with multiple composite material prepregs which contain reinforced fiber and...
A gas turbine engine for an aircraft, including engine length, is arranged to be mounted beneath a wing of the aircraft, and has an engine core having a turbine, a compressor, and a core shaft, the turbine having a lowest pressure rotor stage; a fan located upstream of the engine core,...
Fuel control system for gas turbine engine A fuel control system for a gas turbine engine of the kind having at least one compressor (12, 14) and turbine spool (20, 22) and a free turbine (24), comprising a pneumatic fuel metering device (34) whose metering valve is controlled by......