Patent Leaderboard
USPTO Patent Rankings Data through Dec 31, 2025
Home › Multistage gas turbine engine with differential drive of compressor

Multistage gas turbine engine with differential drive of compressor

US Patent 11448125 · Granted Sep 20, 2022

Estimated economic value: $23,808,000 ⓘ

Assignee

Inventors

View full patent text on Google Patents →

More Patents by These Inventors

Tailoring aircraft powerplant split line parameter with inflatable bladder2025
Gas turbine engine with high speed low pressure turbine section and bearing supp2025
Non-uniform and bi-tri stator spacing for swirl recovery vane (SRV) open rotor e2025
Aircraft propulsion system geartrain2025
Aircraft vertical stabilizer with air system2025
Aircraft vertical stabilizer with air system2025
Aircraft vertical stabilizer with moveable propulsion system(s)2025
Aircraft vertical stabilizer with moveable propulsion system(s)2025
Integrated electro-aero-thermal turbine engine2025
Aircraft airframe component with air system2025
Aircraft airframe component with air system2025
Transmission and method for control of boost spool2025