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Stratified charge rotary aircraft engine technology enablement programThe multifuel stratified charge rotary engine is discussed. A single rotor, 0.7L/40 cu in displacement, research rig engine was tested. The research rig engine was designed for operation at high speeds and pressures, combustion chamber peak pressure providing margin for speed and load excursions above the design requirement for a high is advanced aircraft engine. It is indicated that the single rotor research rig engine is capable of meeting the established design requirements of 120 kW, 8,000 RPM, 1,379 KPA BMEP. The research rig engine, when fully developed, will be a valuable tool for investigating, advanced and highly advanced technology components, and provide an understanding of the stratified charge rotary engine combustion process.
Document ID
19850012853
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Badgley, P. R.
(John Deere Technologies International, Inc. Wood-Ridge, NJ, United States)
Irion, C. E.
(John Deere Technologies International, Inc. Wood-Ridge, NJ, United States)
Myers, D. M.
(John Deere Technologies International, Inc. Wood-Ridge, NJ, United States)
Date Acquired
September 5, 2013
Publication Date
January 31, 1985
Subject Category
Aircraft Propulsion And Power
Report/Patent Number
NAS 1.26:174812
JDTI-RED-85-1
NASA-CR-174812
Accession Number
85N21163
Funding Number(s)
CONTRACT_GRANT: NAS3-23056
PROJECT: RTOP 505-40-68
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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