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Pressure wall patchA rigid patch body for placing over a damaged portion (hole) of an external wall of a pressurized vessel, such as a space vehicle or a habitat, is discussed. The rigid patch body allows an astronaut to make temporary repairs to the pressurized vessel from the exterior of the vessel, which enables more permanent repairs to be made from the interior of the vessel. The pressure wall patch of the present invention includes a floor surrounded by four side members. Each side member includes a threaded screw for anchoring the patch body to the external wall of the pressurized vessel and a recess in its lower surface for supporting an inflatable bladder for surrounding the damaged portion (hole) of the external wall to seal the area surrounding the damaged portion. This allows the vessel to be repressurized. The floor of the rigid patch body supports a source of gas that is connected to the gas supply valve and a gas supply gauge in communication with the gas supply valve and the inflatable bladder.
Document ID
19940019351
Acquisition Source
Legacy CDMS
Document Type
Other - Patent
Authors
Williamsen, Joel E.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Weddendorf, Bruce C.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Date Acquired
August 16, 2013
Publication Date
January 18, 1994
Subject Category
Spacecraft Design, Testing And Performance
Report/Patent Number
Patent Application Number: US-PATENT-APPL-SN-961293
Patent Number: US-PATENT-5,279,092
Patent Number: NASA-CASE-MFS-28724-1
Accession Number
94N23824
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Patent
US-PATENT-5,279,092|NASA-CASE-MFS-28724-1
Patent Application
US-PATENT-APPL-SN-961293
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