Patent Leaderboard
USPTO Patent Rankings Data through Dec 31, 2025
Home › Descent operation for an aircraft parallel hybrid gas turbine engine propulsion system

Descent operation for an aircraft parallel hybrid gas turbine engine propulsion system

US Patent 11939925 · Granted Mar 26, 2024

Estimated economic value: $66,108,000 ⓘ

Assignee

Inventors

View full patent text on Google Patents →

More Patents by These Inventors

Multi-stage partial admission axial turbine2025
Turbine engine with inverse Brayton cycle2025
Hydrogen steam injected turbine engine with turboexpander heat recovery2025
Gas turbine engine mounted above wing and with camber2025
Reverse flow hydrogen steam injected turbine engine2025
Aircraft heat exchanger2025
Cryogenic cooling system for an aircraft2025
Cryogenic cooling system for an aircraft2025
Hybrid electric hydrogen engine for aircraft2025
Gas turbine engine compressor arrangement2025
Increased water heat absorption capacity for steam injected turbine engine2025
Hydrogen-oxygen fueled powerplant with water and heat recovery2025