Patent Leaderboard
USPTO Patent Rankings Data through Dec 31, 2025
Home › Gas turbine engine flame tube cooling system and integral swirler arrangement

Gas turbine engine flame tube cooling system and integral swirler arrangement

US Patent 5765376 · Granted Jun 16, 1998

Assignee

Inventors

View full patent text on Google Patents →

More Patents by These Inventors

Burner with atomizer nozzle2001
Dual-fuel burner2000
Combustion apparatus for a gas turbine having separate combustion and vaporizati1995
Burner for gas turbine engines with axially adjustable swirler1994
Burner for gas turbine engines1994