Patent Leaderboard
USPTO Patent Rankings Data through Dec 31, 2025
Home › Monolithic diffuser and deswirl flow structure for gas turbine engine

Monolithic diffuser and deswirl flow structure for gas turbine engine

US Patent 11220922 · Granted Jan 11, 2022

Estimated economic value: $62,156,000 ⓘ

Assignee

Inventors

View full patent text on Google Patents →

More Patents by These Inventors

Acoustic engine casing for gas turbine engine2025
Diffuser and deswirl system with integral tangential onboard injector for engine2023
Multistage axial-centrifugal compressor systems and methods for manufacture2021
Ported shroud system for turboprop inlets2021
Ported shroud system for turboprop inlets2021
Ported shroud system for turboprop inlets2021
Inlet flow structure for turboprop engine2021
Inlet flow structure for turboprop engine2021
Impeller shroud supports having mid-impeller bleed flow passages and gas turbine2019
Systems and methods for axial compressor with secondary flow2019
Forward-swept impellers and gas turbine engines employing the same2018
Methods for manufacturing high temperature bearing components and rolling elemen2017