民用飛機繫統與結構適航性設計
作 者: (烏克蘭)蒂尼亞科夫·德米特裡(Tiniakov Dmytro),李龍彪,蘇艷 編
定 價: 79
出?版?社: 北京航空航天大學出版社
出版日期: 2019年02月01日
頁 數: 366
裝 幀: 平裝
ISBN: 9787512427624
●Part 1 General Aircraft Structure with Accordance to Airworthiness 1
1.1 Specifics of Civil Aircraft 1
1.1.1 The flight performances of the aircraft 1
1.1.2 Aerodynamic and strength performances 13
1.1.3 Design process and airworthinessrequirements 24
1.1.4 Aircraft classification by functions 26
1.1.5 Weight calculation by statistical data 28
1.2 Classification of Aircrafts on Aerodynamic Configuration and DesigningFeature 30
1.2.1 Classification by the wing arrangement invertical and horizontal planes 30
1.2.2 Classification by the aircraft unitsarrangement (tail unit, engines,landing gear, etc.) 36
1.3 General Requirements to Aircraft Structure 49
1.3.1 General requirements to the aircraft 49
1.3.2 Main stages of aircraft cyclic life 53
1.4 General Knowledge About Wings 63
1.4.1 Purpose of the wing and requirements to it 63
1.4.2 Geometrical parameters and different shapes ofthe wing 67
1.4.3 Main structural members of the wing 71
1.4.4 Load-carry structure of the wing 77
1.5 Tail Unit of the Aircraft 82
1.5.1 Purpose of the tail unit and requirements toit 82
1.5.2 Geometrical parameters and different shapes ofa tail unit 86
1.5.3 Load-carry structure of the tail unit 91
1.6 Control Surfaces and High-lift Devices (CS&HLD) of theAircraft 95
1.6.1 Purpose of CS&HLD and requirements toit 95
1.6.2 Geometrical parameters of CS&HLD 101
1.6.3 Load-carry structure of H-LD and CS 110
1.7 Fuselage of the Aircraft 111
1.7.1 Purpose of the fuselage and requirements to it111
1.7.2 Geometrical parameters and different shapes ofthe fuselage 130
1.7.3 Load-carry structure of the fuselage 134
1.8 Other Structural Members of the Aircraft 141
1.8.1 Purpose and specific requirements for thelanding gear 141
1.8.2 Configuration of the landing gear 148
1.8.3 Purpose and specific requirements for thecontrol system 172
1.8.4 Classification of the control system 178
Questions 194
Part 2 Conformity Verification and Validation of Aircraft Power PlantSystem 195
2.1 Definition of Concept Power Plant 195
2.1.1 General questions 195
2.1.2 Aviation power plant improvementdirections 200
2.1.3 Over-all technical requirements to
aircraft power plants 204
2.1.4 Requirements to aircraft power plants inairworthiness 205
2.2 Classification of Power Plants (Types of Aircraft Engines and TheirArrangement on Aircraft 214
2.2.1 General analysis of aircraft engine types
and areas of their application 214
2.2.2 Auxiliary power unit 224
2.2.3 Engine selection 224
2.2.4 Number of Engines 225
2.2.5 Analysis of scheme of engine arrangement onaircraft 227
2.3 Engine Mounts 239
2.3.1 General information 239
2.3.2 Requirements to engine mount 241
2.3.3 Airframes of engine mounts 243
2.4 Fuel Systems of Power Plant 255
2.4.1 Purpose of fuel systems and requirements tothem 255
2.4.2 Aviation fuels and their properties 270
2.4.3 Structure of fuel systems 274
2.4.4 Layouts of fuel system 274
2.4.5 Calculations of fuel systems 278
2.4.6 Venting and pressurization of fuel system 286
2.4.7 Designing the scheme and calculation of fueldump system 291
2.4.8 Fueling system 294
2.4.9 Structural components of fuel system 296
2.5 Lubrication Systems of Power Plants 305
2.5.1 Purpose of lubrication systems andrequirements 305
2.5.2 Aviation oils 310
2.5.3 General characteristics of lubricationsystems 311
2.5.4 Lubrication system schemes (methods ofseparation air from oil) 313
2.5.5 Calculation of lubrication system 320
2.5.6 Oil cooling, coolers 322
2.5.7 Oil tank structure 324
2.6 Nacelles and Cowlings of Engines 326
2.6.1 Purpose and components of nacelles andcowlings 326
2.6.2 Airframe of nacelles for various types ofengines 330
2.7 Air-Intakes 332
2.7.1 Air suction system, its purpose, requirements andcomponents 332
2.7.2 Air intake classification 335
2.7.3 Designing model and design algorithm ofsubsonic air intakes 338
2.7.4 Subsonic air intake design 341
2.8 Exhaust Units of Power Plants 342
2.8.1 Exhaust units, their purpose, requirements andstructure 342
2.8.2 Types of exhaust 345
2.8.3 Thrust reverse devices, their Purpose andRequirements(types of thrust reverse devices) 347
2.8.4 Aircraft noise sources. noise abatementprocedures 349
2.9 Vibrations of Power Plants. Shock-Absorption of Engine Mounts 351
2.9.1 Airworthiness about powerplant vibrations 351
2.9.2 Common information about aircraft enginesribrations 352
2.9.3 Stiffness of engine mounts 355
2.9.4 Shock-absorption of engine mounts 358
2.9.5 Design of shock absorbers 359
Questions 361
References 362
內容簡介
Thisbook is intended to explain the purposes and general structures of the mainmembers and systems of airplanes, to analyze the characteristics and thestructural features of aircrafts, with accordance to airworthinessrequirements. Also it is intended to describe the methodology for the designingand modifying of aircrafts, their units and systems, assembly units, withaccordance to the requirements ......
