NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
Tests of a 2-Stage, Axial-Flow, 2-Phase TurbineA two phase flow turbine with two stages of axial flow impulse rotors was tested with three different working fluid mixtures at a shaft power of 30 kW. The turbine efficiency was 0.55 with nitrogen and water of 0.02 quality and 94 m/s velocity, 0.57 with Refrigerant 22 of 0.27 quality and 123 m/s velocity, and 0.30 with steam and water of 0.27 quality and 457 m/s velocity. The efficiencies with nitrogen and water and Refrigerant 22 were 86 percent of theoretical. At that fraction of theoretical, the efficiencies of optimized two phase turbines would be in the low 60 percent range with organic working fluids and in the mid 50 percent range with steam and water. The recommended turbine design is a two stage axial flow impulse turbine followed by a rotary separator for discharge of separate liquid and gas streams and recovery of liquid pressure.
Document ID
19830008399
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Elliott, D. G.
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Date Acquired
September 4, 2013
Publication Date
December 15, 1982
Subject Category
Fluid Mechanics And Heat Transfer
Report/Patent Number
DOE/ER-10614/2
NAS 1.26:169789
JPL-PUB-82-98
NASA-CR-169789
Report Number: DOE/ER-10614/2
Report Number: NAS 1.26:169789
Report Number: JPL-PUB-82-98
Report Number: NASA-CR-169789
Accession Number
83N16670
Funding Number(s)
CONTRACT_GRANT: DE-AI01-80ER-10614
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
No Preview Available