Published 1983
by National Aeronautics and Space Administration, National Technical Information Service, distributor in [Washington, DC, Springfield, Va .
Written in
Edition Notes
| Statement | J.W. Bisset and D.C. Howe. |
| Series | NASA contractor report -- NASA CR-168137. |
| Contributions | Howe, David C., United States. National Aeronautics and Space Administration. |
| The Physical Object | |
|---|---|
| Format | Microform |
| Pagination | 1 v. |
| ID Numbers | |
| Open Library | OL15396521M |
The item Energy efficient engine: integrated core/low spool design and performance report, by Aircraft Engine Business Group, Advanced Technology Programs Dept represents a specific, individual, material embodiment of a distinct intellectual or artistic creation found in Indiana State Library. Get this from a library! Energy efficient engine: integrated core/low spool design and performance report. [United States. National Aeronautics and Space Administration.;]. Energy efficient engine. High pressure compressor detail design report Information from these tests is being used to select the configuration for a core engine test scheduled for July and an integrated core/low spool test slated for early The test results will also provide data base for the flight propulsion system. @article{osti_, title = {Energy efficient engine preliminary design and integration study}, author = {Gray, D.E.}, abstractNote = {The technology and configurational requirements of an all new 's energy efficient turbofan engine having a twin spool arrangement with a directly coupled fan and low-pressure turbine, a mixed exhaust nacelle, and a high .
This ACC system is a major improvement in preventing deterioration of the cm ( in.) clearances required to meet the integrated-core/low-spool turbine efficiency goal of . This ACC system is a major improvement in preventing deterioration of the cm ( in.) clearances required to meet the integrated-core/low-spool turbine efficiency goal of % and the light propulsion system efficiency goal of %. The system thus defined is to be demonstrated on the full-scale core and ICLS (integrated core/low spool) test engines which are a part of the E3 program. This report describes the control and fuel system design that has evolved for the E3. Emphasis is placed on the system that is being built for the ICLS engine. The GE design was carried forward into I ntegrated Core/Low Spool (ICLS) testing (Ref. 10). This full-system, integra ted testin g provides a full- engine dataset that was not av ailable.
Intertek is the preferred Energy Efficiency Testing and Certification partner of government authorities, industry associations and manufacturers Intertek has the requisite accreditations, expertise and state-of-the-art testing laboratories around the world to help you meet energy efficiency requirements for global markets. This report summarizes the results of the detail design of the nacelle for the Gei1eral Electric Energy Efficient Engine (E3) Integrated Core Low Spool (ICLS) test vehicle. The results of the detail design effort were presented in a Detail Design Review (DDR) delivered at the NASA-Lewis Research Center on July 9, Stearns, E.M. Energy efficient engine - core design and performance report, NASA-CR, Tiemstra, F.S. Design of a Semi-Empirical Tool for the Evaluation of Turbine Cooling Requirements in a Preliminary Design Stage, Master thesis. The Department of Energy (DOE) establishes energy-efficiency standards for certain appliances and equipment, and currently covers more than 60 different products. Authority to undertake this effort was granted by Congress, and DOE follows a four-phase process when reviewing existing and developing new standards.
