Patent Leaderboard
USPTO Patent Rankings Data through Dec 31, 2025
Home › Multi-axial pivoting combustor liner in gas turbine engine

Multi-axial pivoting combustor liner in gas turbine engine

US Patent 7007480 · Granted Mar 7, 2006

Estimated economic value: $12,346,000 ⓘ

Assignee

Inventors

View full patent text on Google Patents →

More Patents by These Inventors

Multiaxial thermal dissipation and structurally-compliant device2025
Multidirectional enclosure compression locking mechanism2022
Multi-axial energy damping and displacement control2022
Methane conversion apparatus and process using a supersonic flow reactor2019
Methane conversion apparatus and process using a supersonic flow reactor2019
Methane conversion apparatus and process using a supersonic flow reactor2018
Methane conversion apparatus and process using a supersonic flow reactor2018
Methane conversion apparatus and process using a supersonic flow reactor2017
Methane conversion apparatus and process using a supersonic flow reactor2017
Combustor-turbine seal interface for gas turbine engine2013
Combustor-turbine seal interface for gas turbine engine2013
Turbine nozzle assembly including radially-compliant spring member for gas turbi2013