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Calculations of the Performance of a Compression-Ignition Engine-Compressor Turbine Combination I : Performance of a Highly Supercharged Compression-Ignition EngineSmall high-speed single-cylinder compression-ignition engines were tested to determine their performance characteristics under high supercharging. Calculations were made on the energy available in the exhaust gas of the compression-ignition engines. The maximum power at any given maximum cylinder pressure was obtained when the compression pressure was equal to the maximum cylinder pressure. Constant-pressure combustion was found possible at an engine speed of 2200 rpm. Exhaust pressures and temperatures were determined from an analysis of indicator cards. The analysis showed that, at rich mixtures with the exhaust back pressure equal to the inlet-air pressure, there is excess energy available for driving a turbine over that required for supercharging. The presence of this excess energy indicates that a highly supercharged compression-ignition engine might be desirable as a compressor and combustion chamber for a turbine.
Document ID
19930093289
Acquisition Source
Legacy CDMS
Document Type
Other - NACA Wartime Report
Authors
Sanders, J. C.
(National Advisory Committee for Aeronautics. Aircraft Engine Research Lab. Cleveland, OH, United States)
Mendelson, Alexander
(National Advisory Committee for Aeronautics. Aircraft Engine Research Lab. Cleveland, OH, United States)
Date Acquired
September 6, 2013
Publication Date
December 1, 1945
Subject Category
Aircraft Propulsion And Power
Report/Patent Number
NACA-ARR-E5K06
NACA-WR-E-234
Report Number: NACA-ARR-E5K06
Report Number: NACA-WR-E-234
Accession Number
93R22579
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
EXHAUST GASES-TEMPERATURE
ENGINES-COMPRESSION PRESSURES
ENGINES-COMBUSTION CHAMBERS, CONSTANT-PRESSURE
ENGINES, COMPRESSION-IGNITION-PERFORMANCE
FUEL CONSUMPTION
EXHAUST GASES-PRESSURE
ENGINES-INDICATOR DIAGRAMS
ENGINES, SUPERCHARGED-PERFORMANCE
ENGINE-COMPRESSOR-TURBINE-COMBINATIONS
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