Skip to Content
Find More Like This
Return to Search

GAS TURBINE ENGINE DUCTING ARRANGEMENT HAVING DISCRETE INSERT

United States Patent Application

20150132117
A1
View the Complete Application at the US Patent & Trademark Office
A ducting arrangement (10), including: a plurality of discrete ducts (18), each defining a flow path and configured to receive a flow of combustion gases from a respective combustor can, where the plurality of discrete ducts merge to form a common duct structure; and a throat insert (50) configured to define at least part of a junction of one of the discrete ducts and the common duct structure.
Marra, John J. (Winter Springs, FL), Morrison, Jay A. (Titusville, FL), Campbell, Ernie B. (Orlando, FL)
14/ 074,776
November 8, 2013
STATEMENT REGARDING FEDERALLY SPONSORED DEVELOPMENT [0001] Development for this invention was supported in part by Contract No. DE-FC26-05NT42644, awarded by the United States Department of Energy. Accordingly, the United States Government may have certain rights in this invention.