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Initial test results with a single-cylinder rhombic-drive Stirling engineA 6 kW (8 hp), single-cylinder, rhombic-drive Stirling engine was restored to operating condition, and preliminary characterization tests run with hydrogen and helium as the working gases. Initial tests show the engine brake specific fuel consumption (BSFC) with hydrogen working gas to be within the range of BSFC observed by the Army at Fort Belvoir, Virginia, in 1966. The minimum system specific fuel consumption (SFC) observed during the initial tests with hydrogen was 669 g/kW hr (1.1 lb/hpx hr), compared with 620 g/kWx hr (1.02 lb/hpx hr) for the Army tests. However, the engine output power for a given mean compression-space pressure was lower than for the Army tests. The observed output power at a working-space pressure of 5 MPa (725 psig) was 3.27 kW (4.39 hp) for the initial tests and 3.80 kW (5.09 hp) for the Army tests. As expected, the engine power with helium was substantially lower than with hydrogen.
Document ID
19780023590
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Cairelli, J. E.
(NASA Lewis Research Center Cleveland, OH, United States)
Thieme, L. G.
(NASA Lewis Research Center Cleveland, OH, United States)
Walter, R. J.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 3, 2013
Publication Date
July 1, 1978
Subject Category
Energy Production And Conversion
Report/Patent Number
NASA-TM-78919
DOE/NASA/1040-78/1
E-9656
Report Number: NASA-TM-78919
Report Number: DOE/NASA/1040-78/1
Report Number: E-9656
Accession Number
78N31533
Funding Number(s)
CONTRACT_GRANT: EC-77-A-31-1040
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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