Aircraft Hydraulic Design
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Author |
: George R. Keller |
Publisher |
: |
Total Pages |
: 144 |
Release |
: 1957 |
ISBN-10 |
: UOM:39015013844603 |
ISBN-13 |
: |
Rating |
: 4/5 (03 Downloads) |
Synopsis Aircraft Hydraulic Design by : George R. Keller
Author |
: W. L. Green |
Publisher |
: |
Total Pages |
: 168 |
Release |
: 1985 |
ISBN-10 |
: UOM:39015009832364 |
ISBN-13 |
: |
Rating |
: 4/5 (64 Downloads) |
Synopsis Aircraft Hydraulic Systems by : W. L. Green
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 |
Total Pages |
: 278 |
Release |
: 2015-10-09 |
ISBN-10 |
: 9780124199927 |
ISBN-13 |
: 0124199925 |
Rating |
: 4/5 (27 Downloads) |
Synopsis Commercial Aircraft Hydraulic Systems by : Shaoping Wang
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 |
: |
Total Pages |
: 90 |
Release |
: 1957 |
ISBN-10 |
: OCLC:228410561 |
ISBN-13 |
: |
Rating |
: 4/5 (61 Downloads) |
Synopsis Study of the Design of an Aircraft Hydraulic System by : James E. Ross
Author |
: Robert Kyle Schmidt |
Publisher |
: SAE International |
Total Pages |
: 1092 |
Release |
: 2021-02-18 |
ISBN-10 |
: 9780768099423 |
ISBN-13 |
: 0768099420 |
Rating |
: 4/5 (23 Downloads) |
Synopsis The Design of Aircraft Landing Gear by : Robert Kyle Schmidt
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 |
: |
Total Pages |
: 11 |
Release |
: 1990 |
ISBN-10 |
: OCLC:61806858 |
ISBN-13 |
: |
Rating |
: 4/5 (58 Downloads) |
Synopsis A Concurrent Design-analysis Tool for Aircraft Hydraulic Systems by : Society of Automotive Engineers
Author |
: Wayne Stout, Phd |
Publisher |
: DesignAerospace LLC |
Total Pages |
: 395 |
Release |
: 2013-04-25 |
ISBN-10 |
: |
ISBN-13 |
: |
Rating |
: 4/5 ( Downloads) |
Synopsis Aerospace Hydraulic Systems by : Wayne Stout, Phd
The book addresses hydraulic system operation and design from an aerospace perspective. The book covers issues of fluids and fluid flow, component operation and system design. Component sizing methods, mathematical relationships and modeling equations are presented for each component. A methodology for system level modeling and simulation is also presented. Numerous examples and worked sample problems are included.
Author |
: Robert H. Davies (Writer on aircraft) |
Publisher |
: |
Total Pages |
: 16 |
Release |
: 1945 |
ISBN-10 |
: OSU:32435014034979 |
ISBN-13 |
: |
Rating |
: 4/5 (79 Downloads) |
Synopsis Report on the Design of German Aircraft Hydraulic Systems, Fuel Systems, Fuel System Components and Accessories, and Miscellaneous Related Units by : Robert H. Davies (Writer on aircraft)
Author |
: United States. Navy. Naval Air Technical Training Command |
Publisher |
: |
Total Pages |
: 304 |
Release |
: 1951 |
ISBN-10 |
: UIUC:30112008596014 |
ISBN-13 |
: |
Rating |
: 4/5 (14 Downloads) |
Synopsis Aircraft Hydraulics by : United States. Navy. Naval Air Technical Training Command
Author |
: A-6A1 Commercial Aircraft Committee |
Publisher |
: |
Total Pages |
: 0 |
Release |
: 1994 |
ISBN-10 |
: OCLC:1374660886 |
ISBN-13 |
: |
Rating |
: 4/5 (86 Downloads) |
Synopsis AEROSPACE - DESIGN AND INSTALLATION OF COMMERCIAL TRANSPORT AIRCRAFT HYDRAULIC SYSTEMS by : A-6A1 Commercial Aircraft Committee
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.