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Compound cycle engine programThe Compound Cycle Engine (CCE) is a highly turbocharged, power compounded power plant which combines the lightweight pressure rise capability of a gas turbine with the high efficiency of a diesel. When optimized for a rotorcraft, the CCE will reduce fuel burned for a typical 2 hr (plus 30 min reserve) mission by 30 to 40 percent when compared to a conventional advanced technology gas turbine. The CCE can provide a 50 percent increase in range-payload product on this mission. A program to establish the technology base for a Compound Cycle Engine is presented. The goal of this program is to research and develop those technologies which are barriers to demonstrating a multicylinder diesel core in the early 1990's. The major activity underway is a three-phased contract with the Garrett Turbine Engine Company to perform: (1) a light helicopter feasibility study, (2) component technology development, and (3) lubricant and material research and development. Other related activities are also presented.
Document ID
19870002357
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Bobula, G. A.
(NASA Lewis Research Center Cleveland, OH, United States)
Wintucky, W. T.
(NASA Lewis Research Center Cleveland, OH, United States)
Castor, J. G.
(Garrett Turbine Engine Co. Phoenix, Ariz., United States)
Date Acquired
September 5, 2013
Publication Date
January 1, 1986
Subject Category
Aircraft Propulsion And Power
Report/Patent Number
AD-A174144
NASA-TM-88879
NAS 1.26:88879
USAAVSCOM-TR-86-C-37
E-3286
Accession Number
87N11790
Funding Number(s)
PROJECT: DA PROJ. 1L1-62209-AH-76
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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