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AIR1664A
AIRCRAFT FLEXIBLE TANKS GENERAL DESIGN AND INSTALLATION RECOMMENDATIONS
AIRCRAFT FLEXIBLE TANKS GENERAL DESIGN AND INSTALLATION RECOMMENDATIONS
2007-12-01
有效
【范围】 This SAE Aerospace Information Report (AIR) includes general information about the various types and styles of flexible tanks and the tank-mounted fittings that adapt the tank to the surrounding structure and fluid-system plumbing. Recommendations are given relative to the dimensional layout of the tank when these recommendations serve to avoid tank fabrication problems and tank/structure interface problems. As a part of these recommendations, critical dimensions of plumbing adapter fittings are discussed and recommendations made. Tank manufacturing tolerances are given. Recommendations are made relative to cavity design and preparation to facilitate a reliable installation. The special installation requirements of nonself-sealing, self-sealing, and crash-resistant tanks are discussed. This document is not intended to replace the information or requirements of the military and commercial procurement specifications listed in Section 2. No attempt has been made, except in a very general way, to include physical property data such as weight and thickness of the composite materials available in the industry. Such materials are too numerous and vary too much between manufacturers. Whenever specific data or advice is required, it is necessary that the tank manufacturers be consulted. 1.1 Purpose: The purpose of this document is to supply aircraft fluid-system designers with baseline information pertinent to the application of flexible, removable tanks for power plant fluids without regard to the fluid in the tank.strRefField
【与前一版的变化】

替代标准

引用文件/被引文件

Tanks
Oil
Federal Aviation Agency Standard - Flexible Fuel and Oil Cell Material
Tank
Aircraft
Tank
Crash Resistant Aircraft (Nonself-Sealing and Self-Sealing)
Cord
Chemical Conversion Coatings on Aluminum and Aluminum Alloys
Plastic
Baffle Material and Inerting
Foam Material
Acceptance Standards for Flexible Tanks
Light Fixed and Rotary Wing Aircraft Crashworthiness
Human Engineering Design Criteria for Military Systems
Tank Fitting "O" Ring - Center Bolt
Tank Fitting "O" Ring - Through Hole
Tank Fitting "O" Ring - Threaded Hole
USAF Technical Memorandum - Foam Design
USAAVSCOM Aircraft Crash Survival Design Guide Vol. V - Aircraft Post Crash Survival
Minimization of Electrostatic Hazards in Aircraft Fuel Systems
Reticulated Polyurethane Foam Explosion Suppression Material for Fuel Systems and Dry Bays
Gland Design
Airworthiness Standards: Normal

包含图表

Recommended Proporti
TABLE 1
Typical Crash-Resist
Recommended Dimensio
Installation Procedu
Fitting/Structure -
Installed Tanks Show
Typical Self-Sealing
Ballistic Penetratio
TABLE 2

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