Inventor
OSGA KYLE J
US4 patents
Patents
4 patentsUS7617685B2Nov 17, 2009
Quick change fastener system for attaching liner bracket to convergent flap and seal in turbine nozzle
UNITED TECHNOLOGIES CORP11 citations79
US7555904B1Jul 7, 2009
Thermally compliant rivet connection for connecting turbine engine liner to convergent flap and seal for turbine nozzle
UNITED TECHNOLOGIES CORP11 citations79
US7770399B2Aug 10, 2010
Gas turbine engine nozzle liner with thermally compliant attachment brackets
UNITED TECHNOLOGIES CORP4 citations59
US7685825B2Mar 30, 2010
Axially split nozzle liner for convergent nozzle
UNITED TECHNOLOGIES CORP3 citations59