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Pump for delivering heated fluidsA thermomechanical pump particularly suited for use in pumping a warming fluid obtained from an RTG (Radioisotope Thermal Generator) through science and flight instrumentation aboard operative spacecraft is described. The invention is characterized by a pair of operatively related cylinders, each including a reciprocating piston head dividing the cylinder into a pressure chamber confining therein a vaporizable fluid, and a pumping chamber for propelling the warming fluid, and a fluid delivery circuit for alternately delivering the warming fluid from the RTG through the pressure chamber of one cylinder to the pumping chamber of the other cylinder, whereby the vaporizable fluid within the pair of pressure chambers alternately is vaporized and condensed for driving the associated pistons in pumping and intake strokes.
Document ID
19730015786
Acquisition Source
Legacy CDMS
Document Type
Other - Patent
Authors
Sabelman, E. E.
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Date Acquired
September 2, 2013
Publication Date
May 8, 1973
Subject Category
Machine Elements And Processes
Report/Patent Number
Patent Number: US-PATENT-3,732,040
Patent Number: NASA-CASE-NPO-11417
Patent Application Number: US-PATENT-APPL-SN-120241
Accession Number
73N24513
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Patent
US-PATENT-3,732,040|NASA-CASE-NPO-11417
Patent Application
US-PATENT-APPL-SN-120241
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