Aircraft Hydraulic Design PDF Download
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Author: George R. Keller
Publisher:
ISBN:
Category : Transportation
Languages : en
Pages : 144
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Book Description
Author: George R. Keller
Publisher:
ISBN:
Category : Transportation
Languages : en
Pages : 144
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Book Description
Author: W. L. Green
Publisher:
ISBN:
Category : Technology & Engineering
Languages : en
Pages : 168
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Book Description
A comprehensive introduction to aircraft hydraulic systems and components and their applications, in which description and analysis are supported by worked examples, exercises, and numerical questions, thus allowing readers to gauge their progress in the subject.
Author: Shaoping Wang
Publisher: Academic Press
ISBN: 0124199925
Category : Technology & Engineering
Languages : en
Pages : 278
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Book Description
Commercial Aircraft Hydraulic Systems: Shanghai Jiao Tong University Press Aerospace Series focuses on the operational principles and design technology of aircraft hydraulic systems, including the hydraulic power supply and actuation system and describing new types of structures and components such as the 2H/2E structure design method and the use of electro hydrostatic actuators (EHAs). Based on the commercial aircraft hydraulic system, this is the first textbook that describes the whole lifecycle of integrated design, analysis, and assessment methods and technologies, enabling readers to tackle challenging high-pressure and high-power hydraulic system problems in university research and industrial contexts. Commercial Aircraft Hydraulic Systems is the latest in a series published by the Shanghai Jiao Tong University Press Aerospace Series that covers the latest advances in research and development in aerospace. Its scope includes theoretical studies, design methods, and real-world implementations and applications. The readership for the series is broad, reflecting the wide range of aerospace interest and application. Titles within the series include Reliability Analysis of Dynamic Systems, Wake Vortex Control, Aeroacoustics: Fundamentals and Applications in Aeropropulsion Systems, Computational Intelligence in Aerospace Engineering, and Unsteady Flow and Aeroelasticity in Turbomachinery. - Presents the first book to describe the interface between the hydraulic system and the flight control system in commercial aircraft - Focuses on the operational principles and design technology of aircraft hydraulic systems, including the hydraulic power supply and actuation system - Includes the most advanced methods and technologies of hydraulic systems - Describes the interaction between hydraulic systems and other disciplines
Author: James E. Ross
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 90
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Book Description
Author: Robert Kyle Schmidt
Publisher: SAE International
ISBN: 0768099420
Category : Technology & Engineering
Languages : en
Pages : 1092
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Book Description
The aircraft landing gear and its associated systems represent a compelling design challenge: simultaneously a system, a structure, and a machine, it supports the aircraft on the ground, absorbs landing and braking energy, permits maneuvering, and retracts to minimize aircraft drag. Yet, as it is not required during flight, it also represents dead weight and significant effort must be made to minimize its total mass. The Design of Aircraft Landing Gear, written by R. Kyle Schmidt, PE (B.A.Sc. - Mechanical Engineering, M.Sc. - Safety and Aircraft Accident Investigation, Chairman of the SAE A-5 Committee on Aircraft Landing Gear), is designed to guide the reader through the key principles of landing system design and to provide additional references when available. Many problems which must be confronted have already been addressed by others in the past, but the information is not known or shared, leading to the observation that there are few new problems, but many new people. The Design of Aircraft Landing Gear is intended to share much of the existing information and provide avenues for further exploration. The design of an aircraft and its associated systems, including the landing system, involves iterative loops as the impact of each modification to a system or component is evaluated against the whole. It is rare to find that the lightest possible landing gear represents the best solution for the aircraft: the lightest landing gear may require attachment structures which don't exist and which would require significant weight and compromise on the part of the airframe structure design. With those requirements and compromises in mind,The Design of Aircraft Landing Gear starts with the study of airfield compatibility, aircraft stability on the ground, the correct choice of tires, followed by discussion of brakes, wheels, and brake control systems. Various landing gear architectures are investigated together with the details of shock absorber designs. Retraction, kinematics, and mechanisms are studied as well as possible actuation approaches. Detailed information on the various hydraulic and electric services commonly found on aircraft, and system elements such as dressings, lighting, and steering are also reviewed. Detail design points, the process of analysis, and a review of the relevant requirements and regulations round out the book content. The Design of Aircraft Landing Gear is a landmark work in the industry, and a must-read for any engineer interested in updating specific skills and students preparing for an exciting career.
Author: Society of Automotive Engineers
Publisher:
ISBN:
Category : Transportation engineering
Languages : en
Pages : 11
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Book Description
Author: Robert H. Davies (Writer on aircraft)
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 16
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Book Description
Author: United States. Navy. Naval Air Technical Training Command
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 306
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Book Description
Author: A-6A1 Commercial Aircraft Committee
Publisher:
ISBN:
Category :
Languages : en
Pages : 0
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Book Description
This SAE Aerospace Recommended Practice (ARP) establishes the factors which should be considered in the design and installation of a hydraulic system that is fitted to a commercial transport aircraft.
Author: A-6A2 Military Aircraft Committee
Publisher:
ISBN:
Category :
Languages : en
Pages : 0
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Book Description
Supply data comparing various aircraft fluid power system design requirements in order to provide a more complete frame of reference for future aircraft fluid power system design.
