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Gas turbine engine with convertible accessoriesDrive means for connecting a gas turbine engine to its accessories are so constructed as to allow the accessories to be selectively positioned to any one of several predetermined circumferential positions about the perimeter of the engine. This feature permits convenient mounting of the same engine upon vehicles demanding radically different engine mounting arrangements.
Document ID
19780009113
Acquisition Source
Legacy CDMS
Document Type
Other - Patent
Authors
Sargisson, D. F. (GE Cincinnati, Ohio, United States)
Adamson, A. P. (NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 3, 2013
Publication Date
January 17, 1978
Subject Category
Aircraft Propulsion And Power
Report/Patent Number
Patent Number: NASA-CASE-LEW-12390-1
Patent Application Number: US-PATENT-APPL-SN-522109
Patent Number: US-PATENT-4,068,470
Accession Number
78N17056
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Patent
NASA-CASE-LEW-12390-1|US-PATENT-4,068,470
Patent Application
US-PATENT-APPL-SN-522109

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