Fuel Pump Thermal 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 cover the design factors which might cause any part of an electrically motor driven fuel pump assembly to act as an ignition source for explosive fuel vapors within the airplane tank. Revision E of this document is a complete rewrite of the previous version. It expands the scope to cover requirements contained in 14CFR 25.981 and FAA AC 25.981-1C for fuel pump safety, focusing on auto ignition prevention and the general requirements of MIL-STD-882. Other topics relating to pump safety due to ignition sources will be covered in a separate ARP. Otherwise, the content of the document has been updated to include thermal safety recommendations for pumps at the assembly and component level.
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 cover the design factors which might cause any part of an electrically motor driven fuel pump assembly to act as an ignition source for explosive fuel vapors within the airplane tank. Revision E of this document is a complete rewrite of the previous version. It expands the scope to cover requirements contained in 14CFR 25.981 and FAA AC 25.981-1C for fuel pump safety, focusing on auto ignition prevention and the general requirements of MIL-STD-882. Other topics relating to pump safety due to ignition sources will be covered in a separate ARP. Otherwise, the content of the document has been updated to include thermal safety recommendations for pumps at the assembly and component level.
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
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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: 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 : Nuclear engineering
Languages : en
Pages : 612
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Book Description
Author: Raqué, Manuel
Publisher: KIT Scientific Publishing
ISBN: 3731502771
Category :
Languages : en
Pages : 146
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Book Description
Author: Hildebrand
Publisher: Jones & Bartlett Learning
ISBN: 1284112772
Category : Medical
Languages : en
Pages : 135
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Book Description
Objectives and overview of storage tanks -- Codes, standards, and regulations -- Tank design and construction features -- Fireground operations -- Firefighting foam, water supply and fire protection requirements -- Tactical response guidelines -- Glossary
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: George Cramoisi, Editor
Publisher: Lulu.com
ISBN: 1300646675
Category : History
Languages : en
Pages : 546
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Book Description
On July 17, 1996, about 2031 eastern daylight time, Trans World Airlines, Inc. (TWA) flight 800, a Boeing 747, crashed in the Atlantic Ocean near East Moriches, New York. TWA flight 800 was a scheduled international passenger flight from John F. Kennedy International Airport (JFK), New York, New York, to Charles DeGaulle International Airport, Paris, France. All 230 people on board were killed, and the airplane was destroyed. The weather was good. The National Transportation Safety Board determines that the probable cause of the accident was an explosion of the center wing fuel tank, resulting from ignition of the flammable fuel/air mixture in the tank. Contributing factors to the accident were the design and certification concept that fuel tank explosions could be prevented solely by precluding all ignition sources and the design and certification of the Boeing 747. The safety issues in this report focus on fuel tank flammability.
Author: United States. Air Force. Systems Command
Publisher:
ISBN:
Category : Aerospace industries
Languages : en
Pages : 748
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Book Description
