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Cooled spool piston compressorA hydraulically powered gas compressor receives low pressure gas and outputs a high pressure gas. The housing of the compressor defines a cylinder with a center chamber having a cross-sectional area less than the cross-sectional area of a left end chamber and a right end chamber, and a spool-type piston assembly is movable within the cylinder and includes a left end closure, a right end closure, and a center body that are in sealing engagement with the respective cylinder walls as the piston reciprocates. First and second annual compression chambers are provided between the piston enclosures and center housing portion of the compressor, thereby minimizing the spacing between the core gas and a cooled surface of the compressor. Restricted flow passageways are provided in the piston closure members and a path is provided in the central body of the piston assembly, such that hydraulic fluid flows through the piston assembly to cool the piston assembly during its operation. The compressor of the present invention may be easily adapted for a particular application, and is capable of generating high gas pressures while maintaining both the compressed gas and the compressor components within acceptable temperature limits.
Document ID
19940006219
Acquisition Source
Legacy CDMS
Document Type
Other - Patent
Authors
Morris, Brian G.
(NASA Lyndon B. Johnson Space Center Houston, TX, United States)
Date Acquired
August 16, 2013
Publication Date
August 24, 1993
Subject Category
Mechanical Engineering
Report/Patent Number
Patent Number: US-PATENT-5,238,372
Patent Number: NASA-CASE-MSC-22020-1
Patent Application Number: US-PATENT-APPL-SN-998062
Accession Number
94N10674
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Patent
US-PATENT-5,238,372|NASA-CASE-MSC-22020-1
Patent Application
US-PATENT-APPL-SN-998062
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