P
USH1111HExpiredUtilityPatentIndex 61

Mold release technique for solid propellant casting tooling

Assignee: US AIR FORCEPriority: Apr 1, 1991Filed: Apr 1, 1991Granted: Nov 3, 1992
Est. expiryApr 1, 2011(expired)· nominal 20-yr term from priority
Inventors:DUNN WILLIAM FPOULTER LARRY W
B29C 33/0033B29C 33/56
61
PatentIndex Score
3
Cited by
13
References
5
Claims

Abstract

Tooling for solid propellant casting consisting essentially of a shaped, filled polymer or copolymer article having an outer layer of cured polyvinyl butyral. The casting tooling is used extensively throughout the solid propellant industry to mold or form the solid propellant grain of rocket motors. The cured polyvinyl butyral layer provides improved mold release properties to the tooling.

Claims

exact text as granted — not AI-modified
We claim: 
     
       1. Tooling for solid propellant casting consisting essentially of a shaped, filled polymer or copolymer article having at least one outer layer of cured polyvinyl butyral. 
     
     
       2. The tooling of claim 1 wherein said shaped, filled article is polytetrafluoroethylene. 
     
     
       3. The tooling of claim 2 wherein said shaped, filled article contains about 25% glass filler. 
     
     
       4. The tooling of claim 2 wherein said polyvinyl butyral layer contains carbon black. 
     
     
       5. The tooling of claim 4 wherein said polyvinyl butyral layer contains about 7% carbon black.

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