Solution of an Engine Inlet Compatibility Problem During C-17 Low Cost N/EAT Nacelle Thrust Reverser Development

2000-01-5579

10/10/2000

Event
World Aviation Congress & Exposition
Authors Abstract
Content
The C-17 transport aircraft is established in military service with unique capabilities to ground maneuver using thrust reversers. Recently, the C-17 has undergone fan thrust reverser re-design to reduce cost. The new Nacelle/Engine Affordability Team (N/EAT) nacelles are now fully qualified but had, during the flight test program, revealed an engine inlet compatibility problem. Flight tests, engineering analyses and practical applications that led to a successful N/EAT fan reverser cascade design modification are discussed. Fabrication methods that enabled timely implementation of the solution and flight test results showing successful resolution of the problem are presented.
Meta TagsDetails
DOI
https://doi.org/10.4271/2000-01-5579
Pages
14
Citation
Johns, C., "Solution of an Engine Inlet Compatibility Problem During C-17 Low Cost N/EAT Nacelle Thrust Reverser Development," SAE Technical Paper 2000-01-5579, 2000, https://doi.org/10.4271/2000-01-5579.
Additional Details
Publisher
Published
Oct 10, 2000
Product Code
2000-01-5579
Content Type
Technical Paper
Language
English