NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
Resilient Flexible Pressure-Activated SealA resilient, flexible, pressure-activated, high-temperature seal is adapted to be interposed between high and low pressure regions to provide sealing between opposing surfaces of adjacent relatively movable structures. The seal comprises at least one C-shaped sheet element. The C-shaped element design enables the seal to be pressure-activated to provide a radially outward biasing force, responsive to a seal-activating pressure differential acting across the seal thereby increasing resiliency. A centrally-located, resilient core structure provides load bearing and insulating properties. In an exemplary embodiment where at least two seal elements are used, each layer has a cutout slot pattern and the remaining strip material pattern. The slots provide flexibility to the seal, enabling the seal to be manually contoured to seal around corners and curves. The strip material of each layer covers the slots in each adjacent layer to minimize leakage through the slots. Attached barrier strips can block interface leakage between the seal and the opposing surfaces.
Document ID
20090029928
Acquisition Source
Headquarters
Document Type
Other - Patent
Authors
Steinetz, Bruce M.
(NASA Glenn Research Center Cleveland, OH, United States)
Dunlap, Patrick H., Jr.
(NASA Glenn Research Center Cleveland, OH, United States)
Date Acquired
August 24, 2013
Publication Date
March 3, 2009
Subject Category
Mechanical Engineering
Report/Patent Number
Patent Number: US-Patent-7497443
Patent Number: NASA-Case-LEW-17166-1
Patent Application Number: US-Patent-Appl-SN-11/121850
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Patent
US-Patent-7497443|NASA-Case-LEW-17166-1
Patent Application
US-Patent-Appl-SN-11/121850
No Preview Available