Crashworthy external auxiliary fuel tank for aircraft
This invention relates to aircraft fuel systems. An external auxiliary fuel tank for aircraft including a crashworthy bladder carried within an elongated shell. A center structure is carried by the shell intermediate opposing ends thereof, through which the bladder passes. A mounting assembly is car...
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| Format: | Patent |
| Sprache: | eng |
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| Zusammenfassung: | This invention relates to aircraft fuel systems.
An external auxiliary fuel tank for aircraft including a crashworthy bladder carried within an elongated shell. A center structure is carried by the shell intermediate opposing ends thereof, through which the bladder passes. A mounting assembly is carried by the center structure for attaching the fuel tank to an aircraft. |
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