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Operating Temperatures of a Sodium-Cooled Exhaust Valve as Measured by a ThermocoupleA thermocouple was installed in the crown of a sodium-cooled exhaust valve. The valve was then tested in an air-cooled engine cylinder and valve temperatures under various engine operating conditions were determined. A temperature of 1337 F was observed at a fuel-air ratio of 0.064, a brake mean effective pressure of 179 pounds per square inch, and an engine speed of 2000 rpm. Fuel-air ratio was found to have a large influence on valve temperature, but cooling-air pressure and variation in spark advance had little effect. An increase in engine power by change of speed or mean effective pressure increased the valve temperature. It was found that the temperature of the rear spark-plug bushing was not a satisfactory indication of the temperature of the exhaust valve.
Document ID
19930093181
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)
Wilsted, H. D.
(National Advisory Committee for Aeronautics. Aircraft Engine Research Lab. Cleveland, OH, United States)
Mulcahy, B. A.
(National Advisory Committee for Aeronautics. Aircraft Engine Research Lab. Cleveland, OH, United States)
Date Acquired
September 6, 2013
Publication Date
December 1, 1943
Subject Category
Aircraft Propulsion And Power
Report/Patent Number
NACA-ARR-3L06
NACA-WR-E-140
Report Number: NACA-ARR-3L06
Report Number: NACA-WR-E-140
Accession Number
93R22471
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
FUEL-AIR MIXTURES
STEELS-VALVES
ENGINES-PRESSURE DROP
VALVES, WATER-COOLED
VALVES, OIL-COOLED
VALVES, EXHAUST-TEMPERATURES
VALVES, SODIUM-COOLED
ENGINES, AIR-COOLED
INSTRUMENTS-THERMOCOUPLES
SPARK PLUG BUSHINGS
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