Patent Leaderboard
USPTO Patent Rankings Data through Dec 31, 2025
Home › Radial fuel shifting and biasing in an axial staged combustor for a gas turbine engine

Radial fuel shifting and biasing in an axial staged combustor for a gas turbine engine

US Patent 10739003 · Granted Aug 11, 2020

Estimated economic value: $27,500,000 ⓘ

Assignee

Inventors

View full patent text on Google Patents →

More Patents by These Inventors

Reducing noise from a combustor of a gas turbine engine2025
Reducing noise from a combustor of a gas turbine engine2023
High shear swirler with recessed fuel filmer for a gas turbine engine2022
Radial fuel shifting and biasing in an axial staged combustor for a gas turbine 2022
Controlled contact surface for a secondary seal in a non-contact seal assembly2022
Pilot/main fuel shifting in an axial staged combustor for a gas turbine engine2020
Circumferential fuel shifting and biasing in an axial staged combustor for a gas2019
Pilot injector fuel shifting in an axial staged combustor for a gas turbine engi2019
Fuel-air mixture distribution for gas turbine engine combustors2017
Low pressure drop, low NOx, induced draft gas heaters2015
Method for control of thermoacoustic instabilities in a combustor2011
Turbine engine tailcone resonator2009