Patent Leaderboard
USPTO Patent Rankings Data through Dec 31, 2025
Home › Gas turbine engine fixed collective takeoff compensation control system and method

Gas turbine engine fixed collective takeoff compensation control system and method

US Patent 8275500 · Granted Sep 25, 2012

Estimated economic value: $12,426,000 ⓘ

Assignee

Inventors

View full patent text on Google Patents →

More Patents by These Inventors

Turbine engine training manual mode fuel flow control system and method2014
Multiple electric fuel metering systems for gas turbine applications2007