US3966147A
Expired / Lapsed
US
⏱️ 0.0 years remaining
Hammock supported fuel tank
Assignee: Boeing Co
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Filing: 1974-11-26
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Granted: 1976-06-29
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Expires: 1994-11-26
Abstract
Abstract An externally located crashworthy self-sealing fuel tank for use in combination with military aircraft is provided. The tank, having a cross-sectional shape with a substantially flat top and a shallow catenary extending below the flat top, is suspended within a hammock which is connected to the underside of the aircraft. This installation eliminates the normal surrounding structure which would tend to tumble incoming projectiles and increase the severity of tank wounds, minimizes the damaging effect of hydraulic ram upon the aircraft structure and minimizes hazards of explosions or fires by eliminating voids or cavities adjacent to the fuel tank.
Inventors
- 👤 Joseph N. Wittko
- 👤 David G. Harding
- 👤 John J. Schneider
- 👤 Joseph E. Gonsalves
Bibliographic Details
Application Number
—
Jurisdiction
US
Data Source
google_patents
Last Synchronized
2026-11-04 14:40
CPC Classifications
B; B64; B64D; B64D37/00; B64D37/02; B64D37/04; Y; Y10; Y10S; Y10S220/00; Y10S220/905
Claims Analysis
Total Claims: 6
Claim 1
Independent Claim
135 words
In an aircraft, a fuel cell fabricated of self-sealing material having: a substantially flat top surface for nesting under and against a substantially flat external bottom surface of the aircraft and having sides and a bottom shaped in the form of a shallow catenary, and means for supporting the fuel cell comprising: a bar member extending the length of the fuel cell on both sides thereof and extending across the front and rear of the fuel cell, hinge means for releasably attaching said bar member to the bottom surface of the aircraft, means provided on said bar member for securing thereto the fuel cell, and a fabric hammock attached to said bar member, said hammock engaging about and conforming to the shape of said fuel cell to confine and support it from said bar member.
Claim 2
Dependent Claim
135 words
In an aircraft, a fuel cell fabricated of self-sealing material having: a substantially flat top surface for nesting under and against a substantially flat external bottom surface of the aircraft and having sides and a bottom shaped in the form of a shallow catenary, and means for supporting the fuel cell comprising: a bar member extending the length of the fuel cell on both sides thereof and extending across the front and rear of the fuel cell, hinge means for releasably attaching said bar member to the bottom surface of the aircraft, means provided on said bar member for securing thereto the fuel cell, and a fabric hammock attached to said bar member, said hammock engaging about and conforming to the shape of said fuel cell to confine and support it from said bar member.
Claim 3
Dependent Claim
88 words
In an aircraft, an external elongate horizontally disposed fuel tank shaped in cross section in the form of a shallow catenary having a flat top surface, the tank being formed of pliable material, and means for supporting said fuel tank comprising: a bar member extending around the periphery of the top surface of the tank, and a fabric cradle attached to said member and depending therefrom, the cradle engaging about and conforming with the sides, bottom and ends of the tank to support the same from the member.
Claim 4
Dependent Claim
88 words
In an aircraft, an external elongate horizontally disposed fuel tank shaped in cross section in the form of a shallow catenary having a flat top surface, the tank being formed of pliable material, and means for supporting said fuel tank comprising: a bar member extending around the periphery of the top surface of the tank, and a fabric cradle attached to said member and depending therefrom, the cradle engaging about and conforming with the sides, bottom and ends of the tank to support the same from the member.
Claim 5
Dependent Claim
100 words
In an aircraft, an external fuel tank fabricated of self-sealing material and being shaped in cross section, originally and throughout its use, in the form of a shallow catenary having a flat top surface, and means for supporting said tank comprising: a bar member extending around the entire periphery of the top surface of the tank, a fabric hammock secured to the bar member and enclosing the tank, the hammock conforming to the side, end and bottom surfaces of the tank to support the tank from the bar member, and means for releasably attaching the bar member to supporting structure.
Claim 6
Dependent Claim
100 words
In an aircraft, an external fuel tank fabricated of self-sealing material and being shaped in cross section, originally and throughout its use, in the form of a shallow catenary having a flat top surface, and means for supporting said tank comprising: a bar member extending around the entire periphery of the top surface of the tank, a fabric hammock secured to the bar member and enclosing the tank, the hammock conforming to the side, end and bottom surfaces of the tank to support the tank from the bar member, and means for releasably attaching the bar member to supporting structure.
References Cited (Backward Citations)
USPTO Annuity & Maintenance Windows
| Annuity Stage | Window Opens | Payment Deadline | Surcharge Period Until | Estimated Fee | Status |
|---|---|---|---|---|---|
| 3.5 Years (Year 4) | 1979-06-29 | 1979-12-29 | 1980-06-29 | $2000.00 | Window Closed / Lapsed |
| 7.5 Years (Year 8) | 1983-06-29 | 1983-12-29 | 1984-06-29 | $3760.00 | Window Closed / Lapsed |
| 11.5 Years (Year 12) | 1987-06-29 | 1987-12-29 | 1988-06-29 | $7700.00 | Window Closed / Lapsed |