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Due to its speed, low energy requirements, and the fact that it does not require a pre-drilled hole, the technique of self-piercing riveting (SPR) has been increasingly adopted by many industries as a high-speed mechanical fastening technique for the joining of sheet material components. Self-piercing riveting comprehensively reviews the process, equipment, and corrosion behaviour of self-piercing riveting, and also describes the process of evaluation and modelling of strength of self-piercing riveted joints, quality control methods and non-destructive testing.Part one provides an exte
Mechanical Engineering --- Engineering & Applied Sciences --- Mechanical Engineering - General --- Rivets and riveting. --- Automobile industry and trade. --- Automotive industry --- Motor vehicle industry --- Riveting --- Fasteners
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Fatigue of the pressurized fuselages of transport aircraft is a significant problem all builders and users of aircraft have to cope with for reasons associated with assuring a sufficient lifetime and safety, and formulating adequate inspection procedures. These aspects are all addressed in various formal protocols for creating and maintaining airworthiness, including damage tolerance considerations. In most transport aircraft, fatigue occurs in lap joints, sometimes leading to circumstances that threaten safety in critical ways. The problem of fatigue of lap joints has been considerably enlarged by the goal of extending aircraft lifetimes. Fatigue of riveted lap joints between aluminium alloy sheets, typical of the pressurized aircraft fuselage, is the major topic of the present book. The richly illustrated and well-structured chapters treat subjects such as: structural design solutions and loading conditions for fuselage skin joints; relevance of laboratory test results for simple lap joint specimens to riveted joints in a real structure; effect of various production and design related variables on the riveted joint fatigue behaviour; analytical and experimental results on load transmission in mechanically fastened lap joints; theoretical and experimental analysis of secondary bending and its implications for riveted joint fatigue performance; nucleation and shape development of fatigue cracks in riveted longitudinal lap joints; overview of experimental investigations into the multi-site damage for full scale fuselage panels and riveted lap joint specimens; fatigue crack growth and fatigue life prediction methodology for riveted lap joints; residual strength predictions for riveted lap joints in a fuselage structure. The major issues of each chapter are recapitulated in the last section.
Airframes -- Fatigue. --- Airplanes -- Fuselage. --- Riveted joints. --- Strains and stresses. --- Riveted joints --- Airplanes --- Mechanical Engineering --- Chemical & Materials Engineering --- Engineering & Applied Sciences --- Materials Science --- Aeronautics Engineering & Astronautics --- Fuselage --- Fuselage. --- Fuselage (Airplanes) --- Engineering. --- Mechanics. --- Aerospace engineering. --- Astronautics. --- Industrial engineering. --- Production engineering. --- Aerospace Technology and Astronautics. --- Industrial and Production Engineering. --- Joints (Engineering) --- Rivets and riveting --- Airframes --- Classical Mechanics. --- Classical mechanics --- Newtonian mechanics --- Physics --- Dynamics --- Quantum theory --- Management engineering --- Simplification in industry --- Engineering --- Value analysis (Cost control) --- Space sciences --- Aeronautics --- Astrodynamics --- Space flight --- Space vehicles --- Manufacturing engineering --- Process engineering --- Industrial engineering --- Mechanical engineering --- Aeronautical engineering --- Astronautics
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