NASA Technical Reports Server (NTRS) 19930091336: Factors in the Design of Centrifugal Type Injection Valves for Oil Engines
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This edition is associated with NASA Technical Reports Server (NTRS) and a publication year of 1928.
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NASA Technical Reports Server (NTRS) 19930091336: Factors in the Design of Centrifugal Type Injection Valves for Oil Engines
Author: NASA Technical Reports Server (NTRS)
Year: 1928
This research was undertaken in connection with a general study of the application of the fuel injection engine to aircraft. The purpose of the investigation was to determine the effect of four important factors in the design of a centrifugal type automatic injection valve on the penetration, general shape, and distribution of oil sprays. The general method employed was to record the development of single sprays by means of special high-speed photographic apparatus capable of taking 25 consecutive pictures of the moving spray at a rate of 4,000 per second. Investigations were made concerning the effects on spray characteristics, of the helix angle of helical grooves, the ratio of the cross-sectional area of the orifice to that of the grooves, the ratio of orifice length to diameter, and the position of the seat. Maximum spray penetration was obtained with a ratio of orifice length to diameter of about 1.5. Slightly greater penetration was obtained with the seat directly before the orifice.
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