US 9,814,164 B2
Sealing assembly system and method
Efraim Dabusc, Holon (IL)
Assigned to ISRAEL AEROSPACE INDUSTRIES LTD., Lod (IL)
Appl. No. 14/397,625
Filed by ISRAEL AEROSPACE INDUSTRIES LTD., Lod (IL)
PCT Filed Apr. 23, 2013, PCT No. PCT/IL2013/050347
§ 371(c)(1), (2) Date Oct. 28, 2014,
PCT Pub. No. WO2013/164818, PCT Pub. Date Nov. 7, 2013.
Claims priority of application No. 219476 (IL), filed on Apr. 30, 2012.
Prior Publication US 2015/0101859 A1, Apr. 16, 2015
Int. Cl. H05K 9/00 (2006.01); F16J 15/06 (2006.01); F16J 15/12 (2006.01); F16J 15/02 (2006.01)
CPC H05K 9/0015 (2013.01) [F16J 15/022 (2013.01); F16J 15/061 (2013.01); F16J 15/062 (2013.01); F16J 15/123 (2013.01); H05K 9/0081 (2013.01)] 21 Claims
OG exemplary drawing
 
1. An assembly, comprising:
a first component having a first outer surface defining an opening therein;
a second component having second surface; and
a sealing system including:
a sealing member configured for providing sealing between said first component and said second component with respect to said opening and along a generally non-planar sealing perimeter; and
a support member configured for supporting said sealing member in a generally non-planar configuration corresponding to said generally non-planar sealing perimeter;
wherein the support member is seatable onto the second component in a sealing position to thereby align said sealing member with said second component along said sealing perimeter, and
wherein said support member is configured for being sealingly affixed to and in contact with said first component subsequent to said sealing system being seated onto said second component in said sealing position.