USH2145HExpiredUtility

Mitigating ignition of fluids by hot surfaces

Assignee: US AIR FORCEPriority: Jul 24, 2000Filed: Sep 18, 2000Granted: Feb 7, 2006
Est. expiryJul 24, 2020(expired)· nominal 20-yr term from priority
A62C 3/00
47
PatentIndex Score
2
Cited by
11
References
4
Claims

Abstract

A platform, housing, conduit, exhaust duct or other structural element that encloses or supports a hot operating engine or other machinery is described wherein a pattern of micro-cavities is defined on the outer surface of the structure for mitigating ignition of a flammable liquid that comes into contact with the structure, the micro-cavities being sized to minimize seepage into the cavities of the liquid because of its surface tension, thereby preventing wetting of the interior of the cavities by the liquid.

Claims

exact text as granted — not AI-modified
1. A structural element for enclosing or supporting hot operating machinery, comprising:
 (a) a structural member for enclosing or supporting a hot operating machinery; and  
 (b) means defining a plurality of micro-cavities of preselected width and or preselected depth less than the thickness of said structural member on the outer surface of said structural member for mitigating ignition of a flammable liquid that comes into contact with said structural member, said micro-cavities being about one millimeter in width to minimize seepage of the liquid into said micro-cavities because of the surface tension of the liquid.  
 
   
   
     2. The structural element of  claim 1  wherein said micro-cavities are in the form of holes of selected shape defined in the surface of said structural member. 
   
   
     3. The structural element of  claim 1  wherein said micro-cavities are in the form of grooves defined in the surface of said structural member. 
   
   
     4. The structural element of  claim 2  wherein the centerline of said holes is non-perpendicular to said surface of said structural member.

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