NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
Interim review of the Energy Efficient Engine /E3/ ProgramThe NASA-sponsored Energy Efficient Engine (E3) Program, which is now in its fourth year, is assessed from the viewpoint of one of its research contractors. Attention is given to the development status of the shroudless fan, segmented combustor and exhaust mixer components which are encompassed by the program. The shroudless fan blades are two-thirds hollow for lightness, and are fabricated by means of plies and cores subjected to hot isostatic pressing diffusion bonding. The combustor's segmented liner is cast from turbine blade materials. Exhaust mixer flow visualization tests are described. Consideration is given to the effects of integrating the technology described with the low and high pressure advanced turbines whose development is also part of the E3 program.
Document ID
19820051912
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Gardner, W. B.
(United Technologies Corp. East Hartford, CT, United States)
Hannah, W.
(United Technologies Corp. East Hartford, CT, United States)
Gray, D. E.
(United Technologies Corp. Commercial Products Div., East Hartford, CT, United States)
Date Acquired
August 10, 2013
Publication Date
April 1, 1982
Subject Category
Aircraft Propulsion And Power
Report/Patent Number
ASME PAPER 82-GT-271
Meeting Information
Meeting: International Gas Turbine Conference and Exhibit
Location: London
Start Date: April 18, 1982
End Date: April 22, 1982
Sponsors: American Society of Mechanical Engineers
Accession Number
82A35447
Distribution Limits
Public
Copyright
Other

Available Downloads

There are no available downloads for this record.
No Preview Available