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Adiabatic Wankel type rotary engineThis SBIR Phase program accomplished the objective of advancing the technology of the Wankel type rotary engine for aircraft applications through the use of adiabatic engine technology. Based on the results of this program, technology is in place to provide a rotor and side and intermediate housings with thermal barrier coatings. A detailed cycle analysis of the NASA 1007R Direct Injection Stratified Charge (DISC) rotary engine was performed which concluded that applying thermal barrier coatings to the rotor should be successful and that it was unlikely that the rotor housing could be successfully run with thermal barrier coatings as the thermal stresses were extensive.
Document ID
19890008228
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Kamo, R.
(Adiabatics, Inc. Columbus, IN, United States)
Badgley, P.
(Adiabatics, Inc. Columbus, IN, United States)
Doup, D.
(Adiabatics, Inc. Columbus, IN, United States)
Date Acquired
September 5, 2013
Publication Date
September 1, 1988
Subject Category
Aircraft Propulsion And Power
Report/Patent Number
NASA-CR-182233
AI-120
NAS 1.26:182233
Accession Number
89N17599
Funding Number(s)
CONTRACT_GRANT: NAS3-24880
CONTRACT_GRANT: SBIR-01.03-5052
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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