Patent Leaderboard
USPTO Patent Rankings Data through Dec 31, 2025
Home › Converging flow joint insert system at an intersection between adjacent transitions extending between a combustor and a turbine assembly in a gas turbine engine

Converging flow joint insert system at an intersection between adjacent transitions extending between a combustor and a turbine assembly in a gas turbine engine

US Patent 9771813 · Granted Sep 26, 2017

Assignee

Inventors

View full patent text on Google Patents →

More Patents by These Inventors

Belly band seal with anti-rotation structure2017
Transition support system for combustion transition ducts for turbine engines2016
Exhaust manifold flange connection2014
High temperature packer and method2010
Float collar and method2010
Method for running two tubing strings into a well2002
Telescoping tool2002
Method and apparatus for one-trip insertion and retrieval of a tool and auxiliar2001
Drillable inflatable packer and methods of use2001
Self-locating reentry system for downhole well completions2001
Method and apparatus for deploying a well tool into a lateral wellbore1999
Window assembly for multiple wellbore completions1999