Описание: Covering analysis of both internal and external joints and repairs, as well as damage tolerance, non-destructive inspection and self-healing repairs, this book provides essential information on the joints and repairs themselves but, critically, on how they differ from bonds and repairs to metallic aircraft.
Автор: Baker, A.A. Название: Composite Materials for Aircraft Structures ISBN: 1563475405 ISBN-13(EAN): 9781563475405 Издательство: Mare Nostrum (Eurospan) Рейтинг: Цена: 12830.00 р. Наличие на складе: Нет в наличии.
Автор: Cutler John, Gatter Kevin, Liber Jeremy, Natkunam Название: Understanding Aircraft Structures ISBN: 1405120320 ISBN-13(EAN): 9781405120326 Издательство: Wiley Рейтинг: Цена: 8862.00 р. Наличие на складе: Поставка под заказ.
Описание: This book explains aircraft structures so as to provide a basic understanding of the subject and the terminology used, as well as illustrating some of the problems.
Автор: Piet Christof W?lcken; Michael Papadopoulos Название: Smart Intelligent Aircraft Structures (SARISTU) ISBN: 3319224123 ISBN-13(EAN): 9783319224121 Издательство: Springer Рейтинг: Цена: 49631.00 р. Наличие на складе: Есть у поставщика Поставка под заказ.
Описание:
SARISTU: Six years of project management.- Morphing Wing integrated safety approach and results.- Development and validation of a Bird Strike Protection System for an Enhanced Adaptive Droop Nose.- Adaptive Trailing Edge: Specifications, Aerodynamics and Exploitation.- Structural Design of an Adaptive Wing Trailing Edge for Large Aeroplanes.- Design, Optimization, Testing, Verification, and Validation of the Wingtip Active Trailing Edge.- Winglet design, manufacturing and testing.- Ribbon tapes, shape sensors and hardware.- Methodologies for the Damage Detection based on Fiber Optic sensors. Applications to the fuselage panel and lower wing panel.- Methodologies for guided waves based SHM system implementation on composite wing panels: results and perspectives from SARISTU Scenario 5.- An electro-mechanical impedance based mobile system for structural health monitoring and reliability check of bonded piezoelectric sensors.- Damage Identification in Composite Panels - Methodologies and Visualisation.- Manufacturing of CFRP panels with integrated sensor network and contacting of the network.- Flat and curved panel manufacturing.- Compression after multiple impacts: modelling and experimental validation on composite coupon specimens.- Piezochromic compounds able to be used in shock detecting paints.- Brittle coating layers for impact detection in CFRP.- Use of Carbon Nanotubes in Structural Composites.- Enhancement of primary structure robustness by improved damage tolerance.- Improvement of the electrical isotropy of composite structures- Overview.- Fabrication of carbon nanotubes doped veils.- Morphing value assessment on overall aircraft level.- Implementation of Morphing, Structural Health Monitoring and Nanomaterials on an Outer Wing Box.- Fuselage Demonstrators: An overview of the development approach.- Development of a Door Surround Structure with Integrated Structural Health Monitoring System.
Автор: S?rgio M O Tavares; Paulo de Castro Название: Damage Tolerance of Metallic Aircraft Structures ISBN: 3319701894 ISBN-13(EAN): 9783319701899 Издательство: Springer Рейтинг: Цена: 7685.00 р. Наличие на складе: Есть у поставщика Поставка под заказ.
Описание:
This book provides a state-of-the-art review of the fail-safe and damage tolerance approaches, allowing weight savings and increasing aircraft reliability and structural integrity.
The application of the damage tolerance approach requires extensive know-how of the fatigue and fracture properties, corrosion strength, potential failure modes and non-destructive inspection techniques, particularly minimum detectable defect and inspection intervals. In parallel, engineering practice involving damage tolerance requires numerical techniques for stress analysis of cracked structures. These evolved from basic mode I evaluations using rough finite element approaches, to current 3D modeling based on energetic approaches as the VCCT, X-FEM or meshless techniques.
This book provides a concise introduction to this subject.
Автор: Fuh-Gwo Yuan Название: Structural Health Monitoring (SHM) in Aerospace Structures ISBN: 0081001487 ISBN-13(EAN): 9780081001486 Издательство: Elsevier Science Рейтинг: Цена: 33518.00 р. Наличие на складе: Есть у поставщика Поставка под заказ.
Описание: "
Structural Health Monitoring (SHM) in Aerospace Structures "provides readers with the spectacular progress that has taken place over the last twenty years with respect to the area of Structural Health Monitoring (SHM). The widespread adoption of SHM could both significantly improve safety and reduce maintenance and repair expenses that are estimated to be about a quarter of an aircraft fleet s operating costs.
The SHM field encompasses transdisciplinary areas, including smart materials, sensors and actuators, damage diagnosis and prognosis, signal and image processing algorithms, wireless intelligent sensing, data fusion, and energy harvesting. This book focuses on how SHM techniques are applied to aircraft structures with particular emphasis on composite materials, and is divided into four main parts.
Part One provides an overview of SHM technologies for damage detection, diagnosis, and prognosis in aerospace structures. Part Two moves on to analyze smart materials for SHM in aerospace structures, such as piezoelectric materials, optical fibers, and flexoelectricity. In addition, this also includes two vibration-based energy harvesting techniques for powering wireless sensors based on piezoelectric electromechanical coupling and diamagnetic levitation. Part Three explores innovative SHM technologies for damage diagnosis in aerospace structures. Chapters within this section include sparse array imaging techniques and phase array techniques for damage detection. The final section of the volume details innovative SHM technologies for damage prognosis in aerospace structures.
This book serves as a key reference for researchers working within this industry, academic, and government research agencies developing new systems for the SHM of aerospace structures and materials scientists. Provides key information on the potential of SHM in reducing maintenance and repair costsAnalyzes current SHM technologies and sensing systems, highlighting the innovation in each areaEncompasses chapters on smart materials such as electroactive polymers and optical fibers"
Автор: Piet Christof W?lcken; Michael Papadopoulos Название: Smart Intelligent Aircraft Structures (SARISTU) ISBN: 3319370103 ISBN-13(EAN): 9783319370101 Издательство: Springer Рейтинг: Цена: 43100.00 р. Наличие на складе: Есть у поставщика Поставка под заказ.
Описание:
SARISTU: Six years of project management.- Morphing Wing integrated safety approach and results.- Development and validation of a Bird Strike Protection System for an Enhanced Adaptive Droop Nose.- Adaptive Trailing Edge: Specifications, Aerodynamics and Exploitation.- Structural Design of an Adaptive Wing Trailing Edge for Large Aeroplanes.- Design, Optimization, Testing, Verification, and Validation of the Wingtip Active Trailing Edge.- Winglet design, manufacturing and testing.- Ribbon tapes, shape sensors and hardware.- Methodologies for the Damage Detection based on Fiber Optic sensors. Applications to the fuselage panel and lower wing panel.- Methodologies for guided waves based SHM system implementation on composite wing panels: results and perspectives from SARISTU Scenario 5.- An electro-mechanical impedance based mobile system for structural health monitoring and reliability check of bonded piezoelectric sensors.- Damage Identification in Composite Panels - Methodologies and Visualisation.- Manufacturing of CFRP panels with integrated sensor network and contacting of the network.- Flat and curved panel manufacturing.- Compression after multiple impacts: modelling and experimental validation on composite coupon specimens.- Piezochromic compounds able to be used in shock detecting paints.- Brittle coating layers for impact detection in CFRP.- Use of Carbon Nanotubes in Structural Composites.- Enhancement of primary structure robustness by improved damage tolerance.- Improvement of the electrical isotropy of composite structures- Overview.- Fabrication of carbon nanotubes doped veils.- Morphing value assessment on overall aircraft level.- Implementation of Morphing, Structural Health Monitoring and Nanomaterials on an Outer Wing Box.- Fuselage Demonstrators: An overview of the development approach.- Development of a Door Surround Structure with Integrated Structural Health Monitoring System.
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