Back-to-back performance tests were run on seven airline low pressure turbine (LPT) modules and four new CF6-6D modules. Back-to-back test cell runs, in which an airline LPT module was directly compared to a new production module, were included. The resulting change, measured in fuel burn, equaled the level of LPT module deterioration. Three of the LPT modules were analytically inspected followed by a back-to-back test cell run to evaluate current refurbishment techniques
In the CF6 Jet Engine Diagnostics Program the causes of performance degradation were determined for ...
Results of initial tests of the under the wing experimental engine and boilerplate nacelle are prese...
The effects of high pressure turbine clearance changes on engine and module performance was evaluate...
Studies conducted as part of the NASA-Lewis CF6 jet engine diagnostics program are summarized. An 82...
Cruise cockpit recordings and test cell performance data in conjunction with hardware inspection dat...
Cockpit cruise recordings and test cell data in conjunction with hardware inspection results from ai...
The effects of high pressure compressor clearance changes on engine performance were experimentally ...
As part of the NASA-sponsored Engine Component Improvement (ECI) Program, a feasibility analysis of ...
As part of the NASA sponsored engine component improvement program, and fan package was developed to...
An improved high pressure turbine stator reducing fuel consumption in current CF6-50 turbofan engine...
An engine was specially prepared with extensive instrumentation to monitor performance, case tempera...
The results of the collection and analysis of historical data pertaining to the deterioration of JT9...
The various engine deterioration phenomena that affect JT9D performance retention were studied, and ...
Computer programs written in FORTRAN are given for time response calculations on pneumatic and linea...
The results of a flight loads test of the JT9D-7 engine are presented. The goals of this test progra...
In the CF6 Jet Engine Diagnostics Program the causes of performance degradation were determined for ...
Results of initial tests of the under the wing experimental engine and boilerplate nacelle are prese...
The effects of high pressure turbine clearance changes on engine and module performance was evaluate...
Studies conducted as part of the NASA-Lewis CF6 jet engine diagnostics program are summarized. An 82...
Cruise cockpit recordings and test cell performance data in conjunction with hardware inspection dat...
Cockpit cruise recordings and test cell data in conjunction with hardware inspection results from ai...
The effects of high pressure compressor clearance changes on engine performance were experimentally ...
As part of the NASA-sponsored Engine Component Improvement (ECI) Program, a feasibility analysis of ...
As part of the NASA sponsored engine component improvement program, and fan package was developed to...
An improved high pressure turbine stator reducing fuel consumption in current CF6-50 turbofan engine...
An engine was specially prepared with extensive instrumentation to monitor performance, case tempera...
The results of the collection and analysis of historical data pertaining to the deterioration of JT9...
The various engine deterioration phenomena that affect JT9D performance retention were studied, and ...
Computer programs written in FORTRAN are given for time response calculations on pneumatic and linea...
The results of a flight loads test of the JT9D-7 engine are presented. The goals of this test progra...
In the CF6 Jet Engine Diagnostics Program the causes of performance degradation were determined for ...
Results of initial tests of the under the wing experimental engine and boilerplate nacelle are prese...
The effects of high pressure turbine clearance changes on engine and module performance was evaluate...