Aircraft Fuel Pump Mechanical and Electrical Safety Design PDF Download
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Author: AE-5B Aircraft and Engine Fuel and Lubricant Sys Components
Publisher:
ISBN:
Category :
Languages : en
Pages : 0
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Book Description
The requirements presented in this document address the key considerations for mechanical and electrical safety in aircraft fuel pump design. Document sections focus on understanding safety relative to an electrically motor driven fuel pump assembly acting as an ignition source for explosive fuel vapors within the airplane tank. This document is a continuation of the safety information presented in ARP594, which covered the thermal aspects of fuel pump safety design. Other failure modes in FAA AC 25.981-1C fall under the umbrellas of mechanical and electrical design. This new document will address these key elements and, when used in combination with ARP594 and ARP5794, will represent a basis for the proper pump design and testing and support certification of an airframe fuel pump installation. ARP6385 has been reaffirmed to comply with the SAE Five-Year Review policy.
Author: AE-5B Aircraft and Engine Fuel and Lubricant Sys Components
Publisher:
ISBN:
Category :
Languages : en
Pages : 0
Get Book Here
Book Description
The requirements presented in this document address the key considerations for mechanical and electrical safety in aircraft fuel pump design. Document sections focus on understanding safety relative to an electrically motor driven fuel pump assembly acting as an ignition source for explosive fuel vapors within the airplane tank. This document is a continuation of the safety information presented in ARP594, which covered the thermal aspects of fuel pump safety design. Other failure modes in FAA AC 25.981-1C fall under the umbrellas of mechanical and electrical design. This new document will address these key elements and, when used in combination with ARP594 and ARP5794, will represent a basis for the proper pump design and testing and support certification of an airframe fuel pump installation. ARP6385 has been reaffirmed to comply with the SAE Five-Year Review policy.
Author: AE-5B Aircraft and Engine Fuel and Lubricant Sys Components
Publisher:
ISBN:
Category :
Languages : en
Pages : 0
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Book Description
This specification covers the general design, testing, and safety requirements for aircraft tank mounted fuel booster pumps used for engine fuel feed, transfer, and jettison. This Aerospace Recommended Practice is intended to provide general guidelines for the design, development, and qualification of aircraft, tank mounted fuel booster pumps. This revision adds references to SAE documents ARP594 and ARP6385 which provide additional details on proper methods for thermal, mechanical, and electrical safety design of pump components.
Author: AE-5B Aircraft and Engine Fuel and Lubricant Sys Components
Publisher:
ISBN:
Category :
Languages : en
Pages : 0
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Book Description
The requirements presented in this document address the key considerations for thermal safety in aircraft fuel pump design. Document sections focus on understanding safety relative to an electrically motor driven fuel pump assembly acting as an ignition source for explosive fuel vapors within the airplane tank. ARP594 and ARP6385 form a basis for proper safety design of electric, motor driven fuel pumps. Revision F of ARP594 upgrades selected topics with additional design details that have already been included in ARP6385. These revisions are necessary to maintain consistency between the two documents. ARP594, when used in combination with ARP6385 and ARP5794, represents a basis for the proper pump design and testing and support certification of an airframe fuel pump installation. ARP594F has been reaffirmed to comply with the SAE Five-Year Review policy.
Author: Roy Langton
Publisher: John Wiley & Sons
ISBN: 047005946X
Category : Science
Languages : en
Pages : 366
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Book Description
All aspects of fuel products and systems including fuel handling, quantity gauging and management functions for both commercial (civil) and military applications. The fuel systems on board modern aircraft are multi-functional, fully integrated complex networks. They are designed to provide a proper and reliable management of fuel resources throughout all phases of operation, notwithstanding changes in altitude or speed, as well as to monitor system functionality and advise the flight crew of any operational anomalies that may develop. Collates together a wealth of information on fuel system design that is currently disseminated throughout the literature. Authored by leading industry experts from Airbus and Parker Aerospace. Includes chapters on basic system functions, features and functions unique to military aircraft, fuel handling, fuel quantity gauging and management, fuel systems safety and fuel systems design and development. Accompanied by a companion website housing a MATLAB/SIMULINK model of a modern aircraft fuel system that allows the user to set up flight conditions, investigate the effects of equipment failures and virtually fly preset missions. Aircraft Fuel Systems provides a timely and invaluable resource for engineers, project and programme managers in the equipment supply and application communities, as well as for graduate and postgraduate students of mechanical and aerospace engineering. It constitutes an invaluable addition to the established Wiley Aerospace Series.
Author: National Research Council
Publisher: National Academies Press
ISBN: 0309058333
Category : Technology & Engineering
Languages : en
Pages : 158
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Book Description
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.
Author:
Publisher:
ISBN:
Category : Administrative law
Languages : en
Pages : 770
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Book Description
Author:
Publisher:
ISBN:
Category : Weights and measures
Languages : en
Pages : 468
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Book Description
Author: Committee on Aviation Fuels with Improved Fire Safety
Publisher: National Academies Press
ISBN: 0309553423
Category : Business & Economics
Languages : en
Pages : 158
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Book Description
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.
Author:
Publisher:
ISBN:
Category : Specialists
Languages : en
Pages : 20
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Book Description
Author: Allan Seabridge
Publisher: John Wiley & Sons
ISBN: 1119611555
Category : Technology & Engineering
Languages : en
Pages : 400
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Book Description
Provides a significant update to the definitive book on aircraft system design This book is written for anyone who wants to understand how industry develops the customer requirement for aircraft into a fully integrated, tested, and qualified product that is safe to fly and fit for purpose. The new edition of Design and Development of Aircraft Systems fully expands its already comprehensive coverage to include both conventional and unmanned systems. It also updates all chapters to bring them in line with current design practice and technologies taught in courses at Cranfield, Bristol, and Loughborough universities in the UK. Design and Development of Aircraft Systems, 3rd Edition begins with an introduction to the subject. It then introduces readers to the aircraft systems (airframe, vehicle, avionic, mission, and ground systems). Following that comes a chapter on the design and development process. Other chapters look at design drivers, systems architectures, systems integration, verification of system requirements, practical considerations, and configuration control. The book finishes with sections that discuss the potential impact of complexity on flight safety, key characteristics of aircraft systems, and more. Provides a holistic view of aircraft system design, describing the interactions among subsystems such as fuel, navigation, flight control, and more Substantially updated coverage of systems engineering, design drivers, systems architectures, systems integration, modelling of systems, practical considerations, and systems examples Incorporates essential new material on the regulatory environment for both manned and unmanned systems Discussion of trends towards complex systems, automation, integration and the potential for an impact on flight safety Design and Development of Aircraft Systems, 3rd Edition is an excellent book for aerospace engineers, researchers, and graduate students involved in the field.
