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Design and Development of Aircraft Systems 3rd edition [Kõva köide]

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Series edited by (University Of Liverpool), (BAE Systems, UK), Series edited by (MIT), (Smiths Industries, UK)
  • Formaat: Hardback, 400 pages, kõrgus x laius x paksus: 246x175x28 mm, kaal: 885 g
  • Sari: Aerospace Series
  • Ilmumisaeg: 02-Jan-2020
  • Kirjastus: John Wiley & Sons Inc
  • ISBN-10: 1119611504
  • ISBN-13: 9781119611509
Teised raamatud teemal:
Design and Development of Aircraft Systems 3rd editionSuurem pilt
  • Formaat: Hardback, 400 pages, kõrgus x laius x paksus: 246x175x28 mm, kaal: 885 g
  • Sari: Aerospace Series
  • Ilmumisaeg: 02-Jan-2020
  • Kirjastus: John Wiley & Sons Inc
  • ISBN-10: 1119611504
  • ISBN-13: 9781119611509
Teised raamatud teemal:
Püsilink: https://www.kriso.ee/db/9781119611509.html
Märksõnad:

Provides a significant update to the definitive book on aircraft system design

This book is written for anyone who wants to understand how industry develops the customer requirement for aircraft into a fully integrated, tested, and qualified product that is safe to fly and fit for purpose. The new edition of Design and Development of Aircraft Systems fully expands its already comprehensive coverage to include both conventional and unmanned systems. It also updates all chapters to bring them in line with current design practice and technologies taught in courses at Cranfield, Bristol, and Loughborough universities in the UK.

Design and Development of Aircraft Systems, 3rd Edition begins with an introduction to the subject. It then introduces readers to the aircraft systems (airframe, vehicle, avionic, mission, and ground systems). Following that comes a chapter on the design and development process. Other chapters look at design drivers, systems architectures, systems integration, verification of system requirements, practical considerations, and configuration control. The book finishes with sections that discuss the potential impact of complexity on flight safety, key characteristics of aircraft systems, and more.

  • Provides a holistic view of aircraft system design, describing the interactions among subsystems such as fuel, navigation, flight control, and more
  • Substantially updated coverage of systems engineering, design drivers, systems architectures, systems integration, modelling of systems, practical considerations, and systems examples
  • Incorporates essential new material on the regulatory environment for both manned and unmanned systems
  • Discussion of trends towards complex systems, automation, integration and the potential for an impact on flight safety 

Design and Development of Aircraft Systems, 3rd Edition is an excellent book for aerospace engineers, researchers, and graduate students involved in the field.

About the Authors xiii
Series Preface xv
Acknowledgements xvii
Glossary of Terms xix
1 Introduction
1(1)
1.1 General
1(2)
1.2 Systems Development
3(2)
1.3 Skills
5(4)
1.4 Human Aspects
9(1)
1.4.1 Introduction
9(1)
1.4.2 Design Considerations
10(2)
1.4.3 Legislation
12(1)
1.4.4 Summary of Legal Threats
12(1)
1.4.5 Conclusions
13(1)
1.5 Overview
14(3)
Exercises
17(1)
References
17(1)
Further Reading
17(2)
2 The Aircraft Systems
19(1)
2.1 Introduction
19(1)
2.2 Definitions
19(2)
2.3 Everyday Examples of Systems
21(3)
2.4 Aircraft Systems of Interest
24(9)
2.4.1 Airframe Systems
28(1)
2.4.2 Vehicle Systems
28(2)
2.4.3 Interface Characteristics of Vehicle Systems
30(1)
2.4.4 Avionics Systems
31(1)
2.4.5 Interface Characteristics of Vehicle and Avionics Systems
31(1)
2.4.5.1 Vehicle Systems
32(1)
2.4.5.2 Avionics Systems
32(1)
2.4.6 Mission Systems
32(1)
2.4.7 Interface Characteristics of Mission Systems
33(1)
2.5 Ground Systems
33(1)
2.6 Generic System Definition
34(5)
Exercises
37(1)
References
37(1)
Further Reading
37(2)
3 The Design and Development Process
39(34)
3.1 Introduction
39(1)
3.2 Definitions
39(2)
3.3 The Product Lifecycle
41(5)
3.4 Concept Phase
46(4)
3.4.1 Engineering Process
48(1)
3.4.2 Engineering Skills
48(2)
3.5 Definition Phase
50(6)
3.5.1 Engineering Process
52(1)
3.5.2 Engineering Skills
53(3)
3.6 Design Phase
56(2)
3.6.1 Engineering Process
56(1)
3.6.2 Engineering Skills
57(1)
3.7 Build Phase
58(2)
3.7.1 Engineering Process
59(1)
3.7.2 Engineering Skills
59(1)
3.8 Test Phase
60(1)
3.8.1 Engineering Process
60(1)
3.8.2 Engineering Skills
60(1)
3.9 Operate Phase
61(2)
3.9.1 Engineering Process
62(1)
3.9.2 Engineering Skills
63(1)
3.10 Disposal or Retirement Phase
63(2)
3.10.1 Engineering Process
65(1)
3.10.2 Engineering Skills
65(1)
3.11 Refurbishment Phase
65(1)
3.11.1 Engineering Process
66(1)
3.11.2 Engineering Skills
66(1)
3.12 Whole Lifecycle Tasks
66(1)
3.13 Summary
67(6)
Exercises
69(1)
References
70(1)
Further Reading
70(3)
4 Design Drivers
73(40)
4.1 Introduction
73(2)
4.2 Design Drivers in the Business Environment
75(5)
4.2.1 Customer
76(1)
4.2.2 Market and Competition
76(1)
4.2.3 Capacity
77(1)
4.2.4 Financial Issues
77(1)
4.2.5 Defence Policy
78(1)
4.2.6 Leisure and Business Interests
78(1)
4.2.7 Politics
79(1)
4.2.8 Technology
79(1)
4.2.9 Global Economy
80(1)
4.3 Design Drivers in the Project Environment
80(4)
4.3.1 Standards and Regulations
80(1)
4.3.2 Availability
81(1)
4.3.3 Cost
81(1)
4.3.4 Programme
82(1)
4.3.5 Performance
82(1)
4.3.6 Skills and Resources
82(1)
4.3.7 Health, Safety, and Environmental Issues
83(1)
4.3.8 Risk
84(1)
4.4 Design Drivers in the Product Environment
84(4)
4.4.1 Functional Performance
84(1)
4.4.2 Human-Machine Interface
85(1)
4.4.3 Crew and Passengers
86(1)
4.4.4 Stores and Cargo
86(1)
4.4.5 Structure
87(1)
4.4.6 Safety
87(1)
4.4.7 Quality
87(1)
4.4.8 Environmental Conditions
87(1)
4.5 Design Drivers in the Product Operating Environment
88(5)
4.5.1 Heat
88(1)
4.5.2 Noise
89(1)
4.5.3 RF Radiation
89(1)
4.5.4 Solar Energy
90(1)
4.5.5 Altitude
91(1)
4.5.6 Temperature
91(1)
4.5.7 Contaminants, and Destructive and Hazardous Substances
92(1)
4.5.8 Lightning
92(1)
4.5.9 Nuclear, Biological, and Chemical Contamination
92(1)
4.5.10 Vibration
93(1)
4.5.11 Shock
93(1)
4.6 Interfaces with the Sub-system Environment
93(3)
4.6.1 Physical Interfaces
94(1)
4.6.2 Power Interfaces
94(1)
4.6.3 Data Communication Interfaces
95(1)
4.6.4 Input/Output Interfaces
95(1)
4.6.5 Status/Discrete Data
95(1)
4.7 Obsolescence
96(10)
4.7.1 Introduction
96(1)
4.7.2 The Threat of Obsolescence in the Product Lifecycle
97(1)
4.7.2.1 Requirements Specification
98(1)
4.7.2.2 People
99(2)
4.7.2.3 Regulations
101(1)
4.7.2.4 Design, Development, and Manufacture
101(2)
4.7.2.5 The Supply Chain
103(1)
4.7.3 Managing Obsolescence
103(3)
4.8 Ageing Aircraft
106(7)
4.8.1 Introduction
106(1)
4.8.2 Some Examples
107(1)
4.8.3 Systems Issues
108(1)
4.8.4 Certification Issues
109(1)
Exercises
109(1)
References
110(1)
Further Reading
110(3)
5 System Architectures
113(38)
5.1 Introduction
113(1)
5.2 Definitions
114(1)
5.3 System Architectures
115(5)
5.3.1 Vehicle Systems
117(1)
5.3.2 Avionic Systems
118(1)
5.3.3 Mission Systems
118(1)
5.3.4 Cabin Systems
119(1)
5.3.5 Data Bus
119(1)
5.4 Architecture Modelling and Trade-off
120(3)
5.5 Example of a Developing Architecture
123(3)
5.6 Evolution of Avionics Architectures
126(9)
5.6.1 Distributed Analogue Architecture
127(1)
5.6.2 Distributed Digital Architecture
128(2)
5.6.3 Federated Digital Architecture
130(2)
5.6.4 Integrated Modular Architecture
132(3)
5.7 Example Architectures
135(16)
5.7.1 Example 1: System Architecture
135(1)
5.7.2 Example 2: Flight Control System
136(2)
5.7.3 Example 3: Radar System
138(1)
5.7.4 Example 4: Vehicle Systems Management
139(10)
Exercises
149(1)
References
149(1)
Further Reading
149(2)
6 System Integration
151(36)
6.1 Introduction
151(2)
6.2 Definitions
153(1)
6.3 Examples of System Integration
153(19)
6.3.1 Integration at the Component Level
153(1)
6.3.2 Integration at the System Level
154(6)
6.3.3 Integration at the Process Level
160(3)
6.3.4 Integration at the Functional Level
163(3)
6.3.5 Integration at the Information Level
166(1)
6.3.6 Integration at the Prime Contractor Level
166(1)
6.3.7 Integration Arising from Emergent Properties
167(2)
6.3.8 Further Examples of Integrated Systems
169(1)
6.3.8.1 The Airframe
169(2)
6.3.8.2 Propulsion
171(1)
6.3.8.3 Air Systems
171(1)
6.4 System Integration Skills
172(3)
6.5 Management of System Integration
175(3)
6.5.1 Major Activities
175(1)
6.5.2 Major Milestones
175(3)
6.5.3 Decomposition and Definition Process
178(1)
6.5.4 Integration and Verification Process
178(1)
6.5.5 Component Engineering
178(1)
6.6 Highly Integrated Systems
178(4)
6.6.1 Integration of Primary Flight Control Systems
179(3)
6.7 Discussion
182(5)
Exercises
184(2)
References
186(1)
Further Reading
186(1)
7 Verification of System Requirements
187(30)
7.1 Introduction
187(2)
7.2 Gathering Qualification Evidence in the Lifecycle
189(2)
7.3 Test Methods
191(21)
7.3.1 Inspection of Design
192(1)
7.3.2 Calculation
192(1)
7.3.3 Analogy
193(1)
7.3.4 Modelling and Simulation
193(4)
7.3.4.1 Modelling Techniques
197(9)
7.3.5 Test Rigs
206(1)
7.3.6 Environmental Testing
207(1)
7.3.7 Integration Test Rigs
207(2)
7.3.8 Aircraft Ground Testing
209(1)
7.3.9 Flight Test
210(1)
7.3.10 Trials
211(1)
7.3.11 Operational Test
212(1)
7.3.12 Demonstrations
212(1)
7.4 An Example Using a Radar System
212(2)
7.5 Summary
214(3)
Exercises
215(1)
References
215(1)
Further Reading
216(1)
8 Practical Considerations
217(32)
8.1 Introduction
217(1)
8.2 Stakeholders
218(2)
8.2.1 Identification of Stakeholders
218(1)
8.2.2 Classification of Stakeholders
219(1)
8.3 Communications
220(10)
8.3.1 The Nature of Communication
222(1)
8.3.2 Examples of Organisation Communication Media
223(2)
8.3.2.1 Mechanisms for Generating Information
225(1)
8.3.2.2 Unauthorised Access
225(1)
8.3.2.3 Data Storage and Access
226(1)
8.3.2.4 Data Discipline
227(1)
8.3.3 The Cost of Poor Communication
227(1)
8.3.4 A Lesson Learned
228(2)
8.4 Giving and Receiving Criticism
230(2)
8.4.1 The Need for Criticism in the Design Process
230(1)
8.4.2 The Nature of Criticism
230(1)
8.4.3 Behaviours Associated with Criticism
231(1)
8.4.4 Conclusions
232(1)
8.5 Supplier Relationships
232(2)
8.6 Engineering Judgement
234(1)
8.7 Complexity
234(1)
8.8 Emergent Properties
235(1)
8.9 Aircraft Wiring and Connectors
236(10)
8.9.1 Aircraft Wiring
236(1)
8.9.2 Aircraft Breaks
237(1)
8.9.3 Wiring Bundle Definition
238(1)
8.9.4 Wiring Routing
239(1)
8.9.5 Wiring Sizing
239(2)
8.9.6 Aircraft Electrical Signal Types
241(1)
8.9.7 Electrical Segregation
242(1)
8.9.8 The Nature of Aircraft Wiring and Connectors
242(2)
8.9.9 Use of Twisted Pairs and Quads
244(2)
8.10 Bonding and Grounding
246(3)
Exercise
248(1)
References
248(1)
Further Reading
248(1)
9 Configuration Control
249(20)
9.1 Introduction
249(1)
9.2 Configuration Control Process
249(1)
9.3 A Simple Portrayal of a System
250(2)
9.4 Varying System Configurations
252(3)
9.4.1 System Configuration A
252(1)
9.4.2 System Configuration B
253(1)
9.4.3 System Configuration C
254(1)
9.5 Forwards and Backwards Compatibility
255(1)
9.5.1 Forwards Compatibility
255(1)
9.5.2 Backwards Compatibility
256(1)
9.6 Factors Affecting Compatibility
256(2)
9.6.1 Hardware
257(1)
9.6.2 Software
257(1)
9.6.3 Wiring
258(1)
9.7 System Evolution
258(1)
9.8 Configuration Control
259(5)
9.8.1 Airbus A380 Example
261(3)
9.9 Interface Control
264(3)
9.9.1 Interface Control Document
264(2)
9.9.2 Aircraft-level Data Bus Data
266(1)
9.9.3 System Internal Data Bus Data
266(1)
9.9.4 Internal System Input/Output Data
267(1)
9.9.5 Fuel Component Interfaces
267(1)
9.10 Control of Day-to-Day Documents
267(2)
Exercise
268(1)
10 Aircraft System Examples
269(22)
10.1 Introduction
269(1)
10.2 Design Considerations
269(2)
10.3 Safety and Economic Considerations
271(1)
10.4 Failure Severity Categorisation
272(1)
10.5 Design Assurance Levels
272(1)
10.6 Redundancy
273(7)
10.6.1 Architecture Options
274(1)
10.6.1.1 Simplex Architecture
274(2)
10.6.1.2 Duplex Architecture
276(1)
10.6.1.3 Dual/Dual Architecture
276(1)
10.6.1.4 Triplex Architecture
276(1)
10.6.1.5 Quadruplex Architecture
276(1)
10.6.2 System Examples
277(1)
10.6.2.1 Major Systems Event
277(1)
10.6.2.2 Flight Critical Event
278(2)
10.7 Integration of Aircraft Systems
280(7)
10.7.1 Engine Control System
282(1)
10.7.2 Flight Control System
283(1)
10.7.3 Attitude Measurement System
284(1)
10.7.4 Air Data System
284(1)
10.7.5 Electrical Power System
285(1)
10.7.6 Hydraulic Power System
286(1)
10.8 Integration of Avionics Systems
287(4)
References
290(1)
11 Integration and Complexity: The Potential Impact on Flight Safety
291(18)
11.1 Introduction
291(1)
11.2 Integration
291(3)
11.3 Complexity
294(4)
11.4 Automation
298(1)
11.5 Impact on Flight Safety Discussion
299(3)
11.6 Single-pilot Operations
302(1)
11.7 Postscript: Chaos Discussion
303(6)
Exercises
307(1)
References
307(1)
Further Reading
308(1)
12 Key Characteristics of Aircraft Systems
309(48)
12.1 Introduction
309(2)
12.2 Aircraft Systems
311(15)
12.3 Avionics Systems
326(10)
12.4 Mission Systems
336(7)
12.5 Sizing and Scoping Systems
343(2)
12.6 Analysis of the Fuel Penalties of Aircraft Systems
345(12)
12.6.1 Introduction
345(1)
12.6.2 Basic Formulation of Fuel Weight Penalties of Systems
346(3)
12.6.3 Application of Fuel Weight Penalties Formulation for Multi-phase Flight
349(1)
12.6.4 Analysis of Fuel Weight Penalties Formulation for Multi-phase Flight
350(1)
12.6.5 Use of Fuel Weight Penalties to Compare Systems
350(1)
12.6.6 Determining Input Data for Systems Weight Penalties Analysis
351(1)
12.6.6.1 Lift/Drag Ratio
351(1)
12.6.6.2 Specific Fuel Consumption
352(1)
12.6.6.3 System Mass
352(1)
12.6.6.4 System Drag Increase
352(1)
12.6.6.5 Increase in sfc Due to Systems Power Off-takes
352(2)
Nomenclature
354(1)
References
354(3)
13 Conclusions
357(6)
13.1 What's Next?
359(2)
13.2 A Historical Footnote
361(2)
References
362(1)
Index 363
Allan Seabridge has over 50 years of experience in aerospace systems engineering, business development, and research & development, and has developed systems and engineering courses at UK universities. He has retired from full time engineering and enjoys spending time at an aircraft company heritage group.

Ian Moir spent 20 years as an Engineering Officer in the Royal Air Force and has broad and detailed experience working in aircraft avionics systems at a major UK avionics company. Ian has now retired from aerospace activities and is enjoying a life of leisure in the Cotswolds, whilst retaining an interest in aerospace.