A four stage, low pressure turbine component has been designed to power the fan and low pressure compressor system in the Energy Efficient Engine. Designs for a turbine intermediate case and an exit guide vane assembly also have been established. The components incorporate numerous technology features to enhance efficiency, durability, and performance retention. These designs reflect a positive step towards improving engine fuel efficiency on a component level. The aerodynamic and thermal/mechanical designs of the intermediate case and low pressure turbine components are presented and described. An overview of the predicted performance of the various component designs is given
Results obtained from testing five performance builds (three vane cascades and two rotating rigs of ...
A rig test of the cooled high-pressure turbine component for the Energy Efficient Engine was success...
The objective of this study was to demonstrate the capability to analyze the aerodynamic performance...
A subsonic cascade test program was conducted to provide technical data for optimizing the blade and...
The aerodynamic and mechanical design description of the low pressure compressor component of the En...
The energy efficient engine high-pressure turbine is a single stage system based on technology advan...
The objective of the NASA Energy Efficient Engine program is to identify and verify the technology r...
The Low-Pressure Turbine Transition Duct Model Technology Program was directed toward substantiating...
An 8.00-in mean diameter two-stage turbine was investigated over a range of speeds from 0 to 110 per...
The objective of the Energy Efficient Engine Component Development and Integration program is to dev...
Technology for achieving lower installed fuel consumption and lower operating costs in future commer...
The Benefit/Cost Study portion of the NASA-sponsored Energy Efficient Engine Component Development a...
The Energy Efficient Engine (E3) is a NASA program to create fuel saving technology for future trans...
The fan component which was designed for the energy efficient engine is an advanced high performance...
Parametric design and mission evaluations of advanced turbofan configurations were conducted for fut...
Results obtained from testing five performance builds (three vane cascades and two rotating rigs of ...
A rig test of the cooled high-pressure turbine component for the Energy Efficient Engine was success...
The objective of this study was to demonstrate the capability to analyze the aerodynamic performance...
A subsonic cascade test program was conducted to provide technical data for optimizing the blade and...
The aerodynamic and mechanical design description of the low pressure compressor component of the En...
The energy efficient engine high-pressure turbine is a single stage system based on technology advan...
The objective of the NASA Energy Efficient Engine program is to identify and verify the technology r...
The Low-Pressure Turbine Transition Duct Model Technology Program was directed toward substantiating...
An 8.00-in mean diameter two-stage turbine was investigated over a range of speeds from 0 to 110 per...
The objective of the Energy Efficient Engine Component Development and Integration program is to dev...
Technology for achieving lower installed fuel consumption and lower operating costs in future commer...
The Benefit/Cost Study portion of the NASA-sponsored Energy Efficient Engine Component Development a...
The Energy Efficient Engine (E3) is a NASA program to create fuel saving technology for future trans...
The fan component which was designed for the energy efficient engine is an advanced high performance...
Parametric design and mission evaluations of advanced turbofan configurations were conducted for fut...
Results obtained from testing five performance builds (three vane cascades and two rotating rigs of ...
A rig test of the cooled high-pressure turbine component for the Energy Efficient Engine was success...
The objective of this study was to demonstrate the capability to analyze the aerodynamic performance...