Patent Leaderboard
USPTO Patent Rankings Data through Dec 31, 2025
Home › Fuel flow divider and pressurizing valve for gas turbine

Fuel flow divider and pressurizing valve for gas turbine

US Patent 6092546 · Granted Jul 25, 2000

Estimated economic value: $62,774,000 ⓘ

Assignee

Inventors

View full patent text on Google Patents →

More Patents by These Inventors

Electrohydraulic poppet valve device control that maintains the last commanded p2022
Secondary flow lockout valve2022
System that maintains the last commanded position of device controlled by a two-2022
Propeller oil control system for aircraft turboprop engines2021
Combined overspeed and fuel stream selector systems2021
Propeller pitch control system for aircraft turboprop engines2020
Aircraft turboprop engine propeller pitch control system including a controllabl2020
Propeller pitch control actuation system2019
Gas turbine engine mechanical-electrical hybrid fuel delivery system2018
Two-position, two-stage servo valve2017
High efficiency, high pressure gas turbine engine fuel supply system2016
Aircraft fuel filter impending and actual bypass indication system2016