內容大鋼
蒂尼亞科夫·德米特里、李龍彪、蘇艷主編的《民用飛機系統與結構適航性設計（航空器適航技術系列教材）（英文版）》 is intended to explain the purposes and general structures of the main members and systems of airplanes, to analyze the characteristics and the structural features of aircrafts, with accordance to airworthiness requirements. Also it is intended to describe the methodology for the designing and modifying of aircrafts, their units and systems, assembly units, with accordance to the requirements of airworthiness regulations. And it is intended to describe the purpose, layout and principal diagrams, operation and basic parameters, structure of assemblies and elements of systems of aircraft power plants with accordance to airworthiness. The emphasis is put on the operation of systems of aircraft power plants.
It is shown that the classification of aircraft by aerodynamic configuration, a main units structure (as wing, fuselage, tail unit, landing gear, etc.), general requirements to the units, the airworthiness requirements to units, the geometrical parameters of the units, advantages and disadvantages of different units configurations, load carry structures of units, structural members of units, etc.. And it is shown that the functionality, design features, arrangement, operational principles, methods of equipment design of aircraft power plant systems, which meet both general and specific requirements. The operation,structure design of aircraft power plant systems (engine selection, engine mount, systems: fuel, lubrication, air ingestion, exhaust, protection, electro mechanical, etc.) are presented in interaction with other components and systems of airplane.
This book will be suitable for students majoring in airworthiness, designers, manufacturing engineers, etc.
目錄
Part 1 General Aircraft Structure with Accordance to Airworthiness
1.1 Specifics of Civil Aircraft
1.1.1 The flight performances of the aircraft
1.1.2 Aerodynamic and strength performances
1.1.3 Design process and airworthiness requirements
1.1.4 Aircraft classification by functions
1.1.5 Weight calculation by statistical data
1.2 Classification of Aircrafts on Aerodynamic Configuration and Designing Feature
1.2.1 Classification by the wing arrangement in vertical and horizontal planes
1.2.2 Classification by the aircraft units arrangement (tail unit, engines,landing gear, etc.)
1.3 General Requirements to Aircraft Structure
1.3.1 General requirements to the aircraft
1.3.2 Main stages of aircraft cyclic life
1.4 General Knowledge About Wings
1.4.1 Purpose of the wing and requirements to it
1.4.2 Geometrical parameters and different shapes of the wing
1.4.3 Main structural members of the wing
1.4.4 Load-carry structure of the wing
1.5 Tail Unit of the Aircraft
1.5.1 Purpose of the tail unit and requirements to it
1.5.2 Geometrical parameters and different shapes of a tail unit
1.5.3 Load-carry structure of the tail unit
1.6 Control Surfaces and High-lift Devices (CS&HLD) of the Aircraft
1.6.1 Purpose of CS&HLD and requirements to it
1.6.2 Geometrical parameters of CS&HLD
1.6.3 Load-carry structure of H-LD and CS
1.7 Fuselage of the Aircraft
1.7.1 Purpose of the fuselage and requirements to it
1.7.2 Geometrical parameters and different shapes of the fuselage
1.7.3 Load-carry structure of the fuselage
1.8 Other Structural Members of the Aircraft
1.8.1 Purpose and specific requirements for the landing gear
1.8.2 Configuration of the landing gear
1.8.3 Purpose and specific requirements for the control system
1.8.4 Classification of the control system
Questions
Part 2 Conformity Verification and Validation of Aircraft Power Plant System
2.1 Definition of Concept Power Plant
2.1.1 General questions
2.1.2 Aviation power plant improvement directions
2.1.3 Over-all technical requirements to
aircraft power plants
2.1.4 Requirements to aircraft power plants in airworthiness
2.2 Classification of Power Plants (Types of Aircraft Engines and Their Arrangement on Aircraft
2.2.1 General analysis of aircraft engine types
and areas of their application
2.2.2 Auxiliary power unit
2.2.3 Engine selection
2.2.4 Number of Engines
2.2.5 Analysis o
2.3 Engine Mounts
2.3.1 General information
2.3.2 Requirements to engine mount
2.3.3 Airframes of engine mounts
2.4 Fuel Systems of Power Plant
2.4.1 Purpose of fuel systems and requirements to them
2.4.2 Aviation fuels and their properties
2.4.3 Structure of fuel systems
2.4.4 Layouts of fuel system
2.4.5 Calculations of fuel systems
2.4.6 Venting and pressurization of fuel system
2.4.7 Designing the scheme and calculation of fuel dump system
2.4.8 Fueling system
2.4.9 Structural components of fuel system
2.5 Lubrication Systems of Power Plants
2.5.1 Purpose of lubrication systems and requirements
2.5.2 Aviation oils
2.5.3 General characteristics of lubrication systems
2.5.4 Lubrication system schemes (methods of separation air from oil)
2.5.5 Calculation of lubrication system
2.5.6 Oil cooling, coolers
2.5.7 Oil tank structure
2.6 Nacelles and Cowlings of Engines
2.6.1 Purpose and components of nacelles and cowlings
2.6.2 Airframe of nacelles for various types of engines
2.7 Air-Intakes
2.7.1 Air suction system, its purpose, requirements and components
2.7.2 Air intake classification
2.7.3 Designing model and design algorithm of subsonic air intakes
2.7.4 Subsonic air intake design
2.8 Exhaust Units of Power Plants
2.8.1 Exhaust units, their purpose, requirements and structure
2.8.2 Types of exhaust
2.8.3 Thrust reverse devices, their Purpose and Requirements(types of thrust reverse devices)
2.8.4 Aircraft noise sources. noise abatement procedures
2.9 Vibrations of Power Plants. Shock-Absorption of Engine Mounts
2.9.1 Airworthiness about powerplant vibrations
2.9.2 Common information about aircraft engines ribrations
2.9.3 Stiffness of engine mounts
2.9.4 Shock-absorption of engine mounts
2.9.5 Design of shock absorbers
Questions
References
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