Common bulkhead for composite propellant tanks
US-8939407-B2 · Jan 27, 2015 · US
US9453293B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-9453293-B2 |
| Application number | US-201213541560-A |
| Country | US |
| Kind code | B2 |
| Filing date | Jul 3, 2012 |
| Priority date | Jul 18, 2008 |
| Publication date | Sep 27, 2016 |
| Grant date | Sep 27, 2016 |
A practical reading order for non-experts. Skip the full description unless you need deep technical detail.
What the patent document calls the invention.
A short plain-language summary of the technical disclosure.
Who owns or filed the patent and who is credited as inventor.
Filing, priority, publication, and grant dates set the timeline.
The legal scope of protection — read this for what is actually claimed.
Technology tags used to group this patent with similar filings.
Prior art links and similar publications in this corpus.
Official abstract text for this publication.
A composite resin tank includes a wall joined to a dome along a joint. A softening strip is located in the joint.
Opening claim text (preview).
What is claimed is: 1. A method of making a tank subjected to cryogenic temperatures, comprising: laying up a composite resin wall and at least one composite resin dome; bonding the wall to the dome along a joint; fabricating a softening strip; and reducing peak stresses in the joint by placing the softening strip in the joint between the wall and the dome. 2. The method of claim 1 , wherein fabricating the softening strip includes: providing a three dimensional fabric having flexible fibers, and coating the flexible fibers with a thermoplastic binder that is flexible at cryogenic temperatures. 3. The method of claim 1 , wherein coating the fibers is performed by: immersing the fabric in an aqueous solution containing a thermoplastic binder, and drying the fabric. 4. The method of claim 3 , wherein coating the fibers further includes removing air bubbles from the aqueous solution. 5. The method of claim 4 , wherein removing the air bubbles is performed by subjecting the immersed fabric to a vacuum. 6. The method of claim 3 , wherein coating the fibers further includes melting the thermoplastic binder. 7. The method of claim 2 , wherein fabricating the softening strip further includes mechanically working the coated fabric to loosen the fibers. 8. The method of claim 7 , wherein mechanically working the coated fabric is performed by a cold working process. 9. The method of claim 1 , wherein placing the softening strip in the joint includes bonding the softening strip to the composite resin wall and to the composite resin dome. 10. The method of claim 1 , further comprising: co-bonding the composite resin wall, the composite resin dome and the softening strip.
characterised by the disposition or nature of their elements · CPC title
Rockets · CPC title
Vessels not under pressure · CPC title
Coatings · CPC title
Arrangements or adaptations of apparatus or instruments, not otherwise provided for · CPC title
Related publications grouped by family.
Answers are generated from the same data shown on this page.