High performance, thin metal lined, composite overwrapped pressure vessel

a composite overwrapped and pressure vessel technology, applied in the field of composite overwrapped pressure vessels, can solve the problems of not being able to fabricate a liner with the proper characteristics, not being able to withstand the weight of non-composite overwrapped metal tanks, and several failures, and achieve high ductility and high f.sup.ty/e

a composite overwrapped and pressure vessel technology, applied in the field of composite overwrapped pressure vessels, can solve the problems of not being able to fabricate a liner with the proper characteristics, not being able to withstand the weight of non-composite overwrapped metal tanks, and several failures, and achieve high ductility and high f.sup.ty/e

USRE38433E1Inactive Publication Date: 2004-02-24LOCKHEED MARTIN CORP

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  • High performance, thin metal lined, composite overwrapped pressure vessel
  • High performance, thin metal lined, composite overwrapped pressure vessel
  • High performance, thin metal lined, composite overwrapped pressure vessel

Examples

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Embodiment Construction

The following table lists the part numbers and part descriptions as used herein and drawings attached hereto. The preferred materials, if any, follow in parentheses.

PARTS LIST Part Number Description 10 COPV of the first embodiment of the present invention 20 liner (titanium-alloy) 20M maximum thickness of domes 21, 23 21 spun-formed dome (Ti-6Al-4V) 22 liner cylinder (Ti-6Al-4V) 23 spun-formed dome (Ti-6Al-4V) 24 machined boss (Ti-6Al-4V) 25 machined tube (Ti-6Al-4V) 26 machined boss (Ti-6Al-4V) 27 fitting used to test tank 28 holes in boss 24 29 holes in boss 26 30 EB welds 31 preferred region for boss / dome weld 40 adhesive (AF-191) 50 filament-wound graphite-epoxy overwrap (T-1000 / EPON 862- Curing Agent W) 51 graphite windings of filament-wound graphite-epoxy overwrap 50 60 epoxy coating (EPON 862-Curing Agent W) 120 liner (titanium-alloy) 120M maximum thickness of domes 121, 123 121 spun-formed dome (Ti-6Al-4V) 123 spun-formed dome (Ti-6Al-4V) 124 machined boss (Ti-6Al-4V) 126 m...

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Abstract

An innovative technology for composite overwrapped pressure vessels (COPVs) has been developed which significantly increases cost effectiveness, increases reliability, and reduces weight over state-of-the-art COPVs. This technology combines an innovative thin liner made of a metal having a high modulus of elasticity and a high ductility, a high-performance composite overwrap and a high-performance film adhesive at the overwrap / liner interface. The metal liner can be fabricated from readily available titanium alloy sheet and plate using a combination of spin forming and machining to fabricate components and electron-beam welding for tank assembly. The composite overwrap is filament-wound onto an adhesive-covered titanium liner and the overwrap and adhesive are co-cured in an oven to yield an integrated tank structure.

Description

BACKGROUND OF THE INVENTION1. Field of the InventionThe present invention relates to composite overwrapped pressure vessels (COPV's) and their method of manufacture. More specifically, the present invention relates to high-performance COPV's including liners made of metals which exhibit high moduli of elasticity and high ductility, such as titanium alloys.2. General BackgroundThe basic technology for composite overwrapped pressure vessels with metal liners dates back to the late 60's and early 70's.High-performance fibers offer very high strength-to-weight ratios and are ideal for making lightweight pressure vessels. However, composite laminates fabricated with these fibers have relatively high permeability and cannot contain high pressure liquids or gasses or low pressure gasses for extended periods of time. Therefore, composite pressure vessels must have a liner to prevent leakage. The tank efficiency, as measured by its pressure multiplied by its volume divided by its weight (PV / ...

Claims

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Application Information

Patent Timeline
24 Feb 2004
Publication
USRE38433E1
IPC
B23K15/00; B21D51/24; B21D51/16; F17C1/06; F17C1/00; B29C53/00; B29C53/58
CPC
B21D51/24; B29C70/088; F17C1/06; B23K15/0046; Y10T29/49906; B29C53/58; B29K2105/0097; B29K2705/00
Inventors
SEAL, ELLIS C.; ELFER, NORMAN C.