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Ten-hour endurance test of Lawrance all-aluminum cylinder (power plant section report)


Metadata FieldValueLanguage
dc.creatorUnited States. Army. Air Service. Engineering Division.en_US
dc.date.accessioned2018-08-06T15:13:48Z
dc.date.available2018-08-06T15:13:48Z
dc.date.created1921-03-25en_US
dc.identifier.urihttp://hdl.handle.net/11200/49213
dc.descriptionThe object of this test was to determine the reliability and durability of an all-aluminum alloy cylinder on the Lawrance 3-cylinder engine. The cylinder performed satisfactorily, on the torque stand, for a period of 10 hours, except for the exhaust-valve seat, which was hammered out badly. There appears to be no advantage gained in cooling, due to the all-aluminum construction.en_US
dc.formatPDFen_US
dc.publisherWashington, D.C. : Chief of Air Serviceen_US
dc.relation.ispartofseriesAir Service information circular (Aviation) ; v. 2, no. 192en_US
dc.relation.ispartofseriesMcCook Field report ; Serial no. 1427en_US
dc.subjectAirplanes--Motors--Cylindersen_US
dc.subjectAirplanes--Parts--Testingen_US
dc.subjectAirplanes--Design and constructionen_US
dc.subjectAeronautics--Systems engineeringen_US
dc.subjectAluminum alloysen_US
dc.subjectAirplanes--Motors--Partsen_US
dc.titleTen-hour endurance test of Lawrance all-aluminum cylinder (power plant section report)en_US
dc.typeTexten_US

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