Test Requirements And Means For Commercial Aircraft Hydraulic Systems
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| Author | : A-6A1 Commercial Aircraft Committee |
| Publisher | : |
| Total Pages | : 0 |
| Release | : 2014 |
| Genre | : |
| ISBN | : |
This SAE Aerospace Recommended Practice (ARP) describes the recommended tests and their associated test means for commercial aircraft hydraulic systems at the system level that are required to demonstrate compliance with the 14 CFR Part 25 and EASA CS 25 airworthiness regulations, and to show that the required level of maturity at the aircraft entry into service (EIS) has been achieved. There is a need to provide a document that recommends the tests and their associated test means that are required to demonstrate that a hydraulic system will comply with the applicable regulations of 14CFR Part 25 and EASA CS 25 as well as determining that the hydraulic system has the correct level of maturity at entry into service (EIS). This document addresses this need.
| Author | : A-6A1 Commercial Aircraft Committee |
| Publisher | : |
| Total Pages | : 0 |
| Release | : 1998 |
| Genre | : |
| ISBN | : |
This specification covers the requirements that are common to most components used in commercial aircraft hydraulic systems.This specification shall be used to develop Procurement Specifications for components.
| Author | : Shaoping Wang |
| Publisher | : Academic Press |
| Total Pages | : 278 |
| Release | : 2015-10-09 |
| Genre | : Technology & Engineering |
| ISBN | : 0124199925 |
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 | : A-6C5 Components Committee |
| Publisher | : |
| Total Pages | : 0 |
| Release | : 2005 |
| Genre | : |
| ISBN | : |
This SAE Aerospace Standard (AS) specifies the general requirements for hydraulic system reservoirs that are installed in commercial and military aircraft and helicopters and also in missile hydraulic systems.This document includes design, test (production and qualification) criteria for various types of reservoirs. Appendix A provides information on hydraulic fluid volume requirements and reservoir sizing.This document also provides a basis for the Procurement Specification to completely define individual reservoir requirements.
| Author | : A-6C5 Components Committee |
| Publisher | : |
| Total Pages | : 0 |
| Release | : 2018 |
| Genre | : |
| ISBN | : |
This SAE Aerospace Standard (AS) specifies the general requirements for hydraulic system reservoirs that are installed in commercial and military aircraft and helicopters and also in missile hydraulic systems.This document includes design, test (production and qualification) criteria for various types of reservoirs. Appendix A provides information on hydraulic fluid volume requirements and reservoir sizing.This document also provides a basis for the Procurement Specification to completely define individual reservoir requirements. AS5586 has been updated to Revision A for the following reasons: aMinor technical changes bThe references have been updated.
| Author | : W. L. Green |
| Publisher | : |
| Total Pages | : 168 |
| Release | : 1985 |
| Genre | : Technology & Engineering |
| ISBN | : |
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 | : Scott Jackson |
| Publisher | : Routledge |
| Total Pages | : 315 |
| Release | : 2020-09-10 |
| Genre | : Technology & Engineering |
| ISBN | : 1000109011 |
The key principle of systems engineering is that an aircraft should be considered as a whole and not as a collection of parts. Another principle is that the requirements for the aircraft and its subsystems emanate from a logical set of organized functions and from economic or customer-oriented requirements as well as the regulatory requirements for certification. The resulting process promises to synthesize and validate the design of aircraft which are higher in quality, better meet customer requirements and are most economical to operate. This book is more of a how to and a why to rather than a what to guide. It stresses systems engineering is an integrated technical-managerial process that can be adapted without sacrificing quality in which risk handling and management is a major part. It explains that the systems view applies to both the aircraft and the entire air transport system. The book emphasizes that system engineering is not an added layer of processes on top of the existing design processes; it is the glue that holds all the other processes together. The readership includes the aircraft industry, suppliers and regulatory communities, especially technical, program and procurement managers; systems, design and specialty engineers (human factors, reliability, safety, etc.); students of aeronautical and systems engineering and technical management; and government agencies such as FAA and JAA.
| Author | : Mr Scott Jackson |
| Publisher | : Ashgate Publishing, Ltd. |
| Total Pages | : 315 |
| Release | : 2015-03-28 |
| Genre | : Technology & Engineering |
| ISBN | : 147243921X |
Explains the principles of systems engineering in simple, understandable terms and describes to engineers and managers how these principles would be applied to the development of commercial aircraft.
| Author | : A-6A2 Military Aircraft Committee |
| Publisher | : |
| Total Pages | : 0 |
| Release | : 1994 |
| Genre | : |
| ISBN | : |
The purpose of this document is to outline and publish the criteria applicable to design and installation for types I and II, classes 4000 and 5000 psi aircraft hydraulic systems.
| Author | : National Research Council |
| Publisher | : National Academies Press |
| Total Pages | : 158 |
| Release | : 1997-09-18 |
| Genre | : Technology & Engineering |
| ISBN | : 0309058333 |
The reduction of the fire hazard of fuel is critical to improving survivability in impact-survivable aircraft accidents. Despite current fire prevention and mitigation approaches, fuel flammability can overwhelm post-crash fire scenarios. The Workshop on Aviation Fuels with Improved Fire Safety was held November 19-20, 1996 to review the current state of development, technological needs, and promising technology for the future development of aviation fuels that are most resistant to ignition during a crash. This book contains a summary of workshop discussions and 11 presented papers in the areas of fuel and additive technologies, aircraft fuel system requirements, and the characterization of fuel fires.
