Actions for The CF6 jet engine performance improvement : New front mount

Email RIS file
Bookmark
Report an Issue

The CF6 jet engine performance improvement : New front mount

Author
Fasching, W. A.
Published
Dec 1, 1979.
Physical Description
1 electronic document
Online Version

Availability

I Want It
I Want It

Finding items...

Restrictions on Access
Unclassified, Unlimited, Publicly available.
Free-to-read Unrestricted online access
Summary
The New Front Mount was evaluated in component tests including stress, deflection/distortion and fatigue tests. The test results demonstrated a performance improvement of 0.1% in cruise sfc, 16% in compressor stall margin and 10% in compressor stator angle margin. The New Front Mount hardware successfully completed 35,000 simulated flight cycles endurance testing.
Other Subject(s)
Collection
NASA Technical Reports Server (NTRS) Collection.
Note
Document ID: 19800005870.
Accession ID: 80N14127.
NASA-CR-159639.
R79AEG366.
Terms of Use and Reproduction
No Copyright.
View MARC record | catkey: 15723896