An Application of Brazed Stainless Steel Honeycomb for Moderately High Temperature Structures

630391

01/01/1963

Event
Pre-1964 SAE Technical Papers
Authors Abstract
Content
The C-141 airplane is powered by four Pratt & Whitney turbofan engines with the fan mounted on the compressor end. High velocity, high pressure air from the fan is ducted to the aft end of the nacelle through kidney shaped ducts. In the tailpipe area, the ducts and tailpipe utilize a common skin. During rapid engine deceleration a condition can occur that subjects the tailpipe to a collapsing pressure. A single skin tailpipe subjected to this pressure at an operating temperature of 1000 F would have been excessively heavy. Brazed stainless steel honeycomb with thin face gages and lightweight core was selected for this application with a substantial saving in weight and no loss in performance.
Meta TagsDetails
DOI
https://doi.org/10.4271/630391
Pages
8
Citation
Gray, W., and Linderman, D., "An Application of Brazed Stainless Steel Honeycomb for Moderately High Temperature Structures," SAE Technical Paper 630391, 1963, https://doi.org/10.4271/630391.
Additional Details
Publisher
Published
Jan 1, 1963
Product Code
630391
Content Type
Technical Paper
Language
English