Reliability based airframe maintenance optimization and applications
Reliability Based Aircraft Maintenance Optimization and Applications presents flexible and cost-effective maintenance schedules for aircraft structures, particular in composite airframes. By applying an intelligent rating system, and the back-propagation network (BPN) method and FTA technique, a new...
Otros Autores: | , , |
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Formato: | Libro electrónico |
Idioma: | Inglés |
Publicado: |
London, England :
Academic Press
2017.
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Edición: | 1st edition |
Materias: | |
Ver en Biblioteca Universitat Ramon Llull: | https://discovery.url.edu/permalink/34CSUC_URL/1im36ta/alma991009630343706719 |
Tabla de Contenidos:
- Cover
- Title page
- Copyright page
- Contents
- List of Figures
- List of Tables
- About the Authors
- Preface
- Abbreviations
- Abstract
- Chapter 1 - Introduction
- 1.1 - Challenges of modern developing commercial aircraft
- 1.2 - Evolution of aircraft maintenance process
- 1.3 - Aircraft composite structures
- 1.4 - Reliability-centered maintenance
- 1.4.1 - Reliability Design
- 1.4.2 - Reliability-Centered Maintenance
- 1.5 - MSG-3 structural analysis
- 1.6 - A380 maintenance programs
- 1.7 - Summary
- Chapter 2 - Basic Concepts
- 2.1 - Accident
- 2.1.1 - Accident in Aviation
- 2.1.2 - Accident Category in Aviation
- 2.2 - Near misses
- 2.3 - Risk
- 2.4 - Safety
- 2.5 - Reliability
- 2.6 - Risk management
- 2.7 - Incident
- 2.8 - Airworthiness
- 2.9 - Quality
- 2.10 - Airworthiness
- 2.11 - Availability
- 2.12 - Aircraft maintenance
- 2.13 - Sources and types of failure in aircraft
- 2.13.1 - Mechanisms of Failure
- 2.13.2 - Causes of Failure
- 2.13.3 - Sources of Failure
- 2.14 - Maintenance system and tasks
- 2.14.1 - Servicing
- 2.15 - Component servicing
- 2.16 - Overhaul
- 2.17 - Bay servicing
- 2.17.1 - Repair
- 2.17.2 - Modification
- 2.18 - Replacement/throwaway
- 2.19 - Functional testing
- 2.20 - Calibration
- 2.21 - Nondestructive evaluation
- 2.22 - Avionics maintenance
- 2.23 - Software maintenance
- 2.24 - Interdependence of operations and maintenance
- 2.24.1 - Factors Affecting the Airline's Maintenance System
- 2.24.1.1 - Seasonal Traffic Trends
- 2.24.1.2 - Geography of the Operation
- 2.24.1.3 - Location and Size of Maintenance Establishments
- 2.24.1.4 - Size and Composition of the Airline Fleet
- 2.24.1.5 - Aircraft Utilization
- 2.24.1.6 - Weather
- 2.24.1.7 - Availability of Subcontracting for Servicing and Maintenance
- 2.24.1.8 - Competitors' Operations.
- 2.24.1.9 - Availability of Staff
- 2.24.2 - Factors Affecting the Military Maintenance System
- Chapter 3 - Aircraft Reliability and Maintainability Analysis and Design
- 3.1 - Reliability fundamental mathematics
- 3.1.1 - Density Function
- 3.1.2 - Failure Probability Function
- 3.1.3 - Failure Rate
- 3.1.4 - Reliability Function
- 3.1.5 - Bathtub Curve
- 3.1.6 - MTTF
- 3.2 - Some common failure distributions
- 3.2.1 - Exponential Distribution
- 3.2.2 - Weibull Distribution
- 3.2.3 - Normal Distribution
- 3.2.4 - Lognormal Distribution
- 3.2.5 - Summary of Often Used Distributions
- 3.3 - Binary system reliability models
- 3.3.1 - Series System
- 3.3.2 - Parallel System
- 3.3.3 - Standby Redundancy System
- 3.4 - Mechanical reliability-Stress-strength interference model
- 3.4.1 - Introduction of Theory
- 3.4.2 - Analytical Results
- 3.4.3 - Example
- 3.5 - Fuzzy reliability theory
- 3.5.1 - Irrationality of Conventional Reliability Theory
- 3.5.2 - Fuzzy Reliability Basic Theories
- 3.5.3 - Fuzzy Reliability
- 3.5.4 - Fuzzy Failure Rate
- 3.5.5 - Fuzzy MTBF
- 3.6 - Hardware reliability
- 3.6.1 - Failure Mechanisms and Damage Models
- 3.6.2 - Incorrect Mechanical Performance
- 3.6.3 - Incorrect Thermal Performance
- 3.6.4 - Incorrect Electrical Performance
- 3.6.5 - Electromagnetic Interference
- 3.6.6 - Particle Radiation
- 3.6.7 - Yield
- 3.6.8 - Buckling
- 3.6.9 - Fracture
- 3.6.10 - Interfacial Deadhesion
- 3.6.11 - Fatigue
- 3.6.12 - Creep
- 3.6.13 - Wear
- 3.6.14 - Aging Due to Interdiffusion
- 3.6.15 - Aging Due to Particle Radiation
- 3.6.16 - Other Forms of Aging
- 3.6.17 - Corrosion
- 3.6.18 - Metal Migration
- 3.7 - Maintainability analysis and design
- 3.7.1 - Definitions Used in Maintainability Engineering
- 3.7.2 - Measurements
- 3.7.3 - Maintainability Function.
- 3.7.4 - Often Used Maintainability Distributions
- 3.7.5 - Availability Models
- 3.7.6 - Effectiveness Models
- 3.8 - Specification of Maintainability
- 3.8.1 - Quantitative Maintainability Clauses
- 3.8.2 - Qualitative Maintainability Requirements
- 3.8.3 - Choice of a Maintainability Characteristic
- 3.9 - Assessment and prediction of maintainability
- 3.9.1 - Maintainability Prediction
- 3.9.2 - Prediction Advantages
- 3.9.3 - Techniques
- 3.9.4 - Basic Assumptions and Interpretations
- 3.9.5 - Elements of Maintainability Prediction Techniques
- 3.10 - Maintainability design: The affected factors
- 3.11 - Maintainability design: Criteria
- 3.12 - Maintainability design: Allocation
- 3.13 - Maintainability design-limiting clearance
- 3.14 - Maintainability design-accessibility
- 3.15 - Maintainability design-packaging
- 3.16 - Maintainability design-standardization and interchange ability
- 3.17 - Maintainability design-installation-components arrangement
- 3.18 - Maintainability design-general criteria
- 3.19 - Maintainability demonstration and testing
- 3.19.1 - Maintainability Testing Program
- 3.19.2 - Maintainability Demonstration
- 3.19.3 - Test Conditions
- 3.19.4 - Maintenance Task Selection
- 3.20 - Maintainability and reliability program activities during the phases of a project
- 3.20.1 - Definition Phase
- 3.20.2 - Design and Development (Including Initial Manufacture)
- 3.20.3 - Production
- 3.20.4 - Installation and Commissioning
- 3.20.5 - Operation-Usage and Maintenance
- 3.21 - Maintainability management
- 3.21.1 - Responsibilities Interface of Maintainability and Maintenance
- 3.21.2 - Maintainability Analysis
- 3.21.3 - Maintainability Design
- 3.21.4 - Maintainability Administration
- Chapter 4 - RCM and Integrated Logistic Support
- 4.1 - Introduction.
- 4.2 - Maintenance analysis procedures
- 4.2.1 - The MSG Series Procedures
- 4.2.2 - Reliability-Centered Maintenance
- 4.2.3 - MSG-3 Logic
- 4.2.4 - Structures
- 4.2.5 - Fatigue Damage
- 4.2.6 - Environmental Deterioration
- 4.2.7 - Accidental Damage
- 4.2.8 - Systems and Power Plants
- 4.2.9 - Setting Task Frequencies/Intervals
- 4.3 - Statistical reliability assessment
- 4.4 - Logistic support analysis
- 4.4.1 - LSA Tasks
- 4.4.2 - Failure Mode Effect Analysis
- 4.5 - Fault tree analysis
- 4.5.1 - Qualitative Analysis of a Fault Tree
- 4.5.2 - Quantitative Analysis of a Fault Tree
- 4.6 - Level of repair analysis
- 4.7 - Logistic support analysis record
- 4.8 - LSA models
- 4.9 - Elements of ILS
- 4.10 - Support equipment
- 4.11 - Facilities
- 4.12 - Data
- Chapter 5 - Intelligent Structural Rating System Based on Back-Propagation Network
- 5.1 - Introduction
- 5.2 - Artificial neural network
- 5.2.1 - Basic Theory
- 5.2.2 - Back-Propagation Network
- 5.3 - Design BPN for AD
- 5.3.1 - BPN Configuration
- 5.3.2 - Case Study
- 5.4 - Discussion
- 5.4.1 - Selection of Number of Nodes in Hidden Layers and Parameter Ratio
- 5.4.2 - Selection of Training Algorithms
- 5.5 - Conclusions
- Chapter 6 - Fault Tree Analysis for Composite Structural Damage
- 6.1 - Introduction
- 6.2 - Basic principles of fault tree analysis
- 6.2.1 - Elements of FTA
- 6.2.2 - Boolean Algebra Theorems
- 6.3 - FTA for composite damage
- 6.4 - Qualitative analysis
- 6.4.1 - Minimal Cut Sets
- 6.4.2 - Structure Importance Analysis
- 6.4.3 - Probability Importance Analysis
- 6.4.4 - Relative Probability Importance Analysis
- 6.5 - Quantitative analysis
- 6.6 - Discussion
- 6.7 - Potential solutions
- 6.7.1 - Material Design
- 6.7.2 - Fabrication Process
- 6.7.3 - Personnel Training
- 6.7.4 - Surface Protection.
- 6.7.5 - Damage Evaluation and Life Prediction
- 6.8 - Conclusions
- Chapter 7 - Inspection Interval Optimization for Aircraft Composite Structures Considering Dent Damage
- 7.1 - Introduction
- 7.2 - Damage tolerance philosophy of composite structures
- 7.2.1 - Properties of Aircraft Composite Structures
- 7.2.2 - Maintenance Model of Composite Structures
- 7.3 - Damage characterization
- 7.3.1 - Data Statistics and Category
- 7.3.2 - Damage Size Distribution
- 7.3.3 - Probability of Detection (POD)
- 7.4 - Probabilistic method
- 7.4.1 - Reliability Formulation
- 7.4.2 - Monte Carlo Simulation
- 7.5 - Case study
- 7.5.1 - Average Damages Per Life Cycle (Nd)
- 7.5.2 - Load Cases
- 7.5.3 - Damage Size and Occurrence Time
- 7.5.4 - Inspection Efficiency
- 7.5.5 - Residual Strength Reduction and Recovery
- 7.5.6 - Other Assumptions and Definitions to Facilitate the Simulation
- 7.6 - Simulation results and discussion
- 7.7 - Conclusions
- Chapter 8 - Repair Tolerance for Composite Structures Using Probabilistic Methodologies
- 8.1 - Introduction
- 8.2 - Repair tolerance
- 8.3 - Probabilistic method
- 8.4 - Case study
- 8.4.1 - Load Case
- 8.4.2 - Average Damage Per Life Cycle (Nd)
- 8.4.3 - Damage Size Distribution
- 8.4.4 - Probability of Detection (POD)
- 8.4.5 - Inspection Schedule
- 8.4.6 - Residual Strength Reduction and Recovery
- 8.4.7 - Repair Policy
- 8.4.8 - Factor of Safety
- 8.4.9 - Probability of Failure (POF)
- 8.4.10 - Maintenance Cost
- 8.5 - Results and discussion
- 8.6 - Conclusions
- Chapter 9 - Structural Health Monitoring and Influence on Current Maintenance
- 9.1 - Structural health monitoring technology
- 9.2 - SHM applications in aircraft
- 9.3 - Influence of SHM on current maintenance
- 9.4 - Integration of SHM with MSG-3 analysis
- A - Scheduled Maintenance
- B - Scheduled SHM.
- C - Scheduled CBM.