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Development of Multifuel Features of the LD-465 and LDS-465 Military Engines

SAE Technical Papers (1906-current) Available online

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Format:
Conference/Event
Author/Creator:
Isley, W. F., author.
Conference Name:
SAE World Congress & Exhibition (1964-01-01 : Detroit, Michigan, United States)
Language:
English
Physical Description:
1 online resource
Place of Publication:
Warrendale, PA SAE International 1964
Summary:
Continental Aviation, through contract with the U.S. Army Ordnance Corps, has developed the LD-465 and LDS-465 engines at 140 and 210 bhp, respectively, as an outgrowth of the basic LDS-427 multifuel military engine. The engines are of conventional 6-cyl, in-line design except for those features contributing to their multifuel capability. These features include the Hypercycle combustion system, intake swirl port, water-heated intake manifold, a simplified manifold flame heater to aid in cold starting, and a fuel density compensator for maintaining equal power ratings on all fuels
Notes:
Vendor supplied data
Publisher Number:
640371
Access Restriction:
Restricted for use by site license

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