F05D 2270/051
Thrust
F05D2270/051 (Thrust) appears on 188 US grants and 210 published applications in this corpus.
Search patents in F05D- Granted patents
- 188
- Published applications
- 210
- Assignees
- 58
- Inventors
- 389
- Latest grant
- 14 Apr 2026
Filings by year
| Year | Granted patents | Published applications |
|---|---|---|
| 1981 | 3 | 0 |
| 1982 | 2 | 0 |
| 1983 | 1 | 0 |
| 1984 | 1 | 0 |
| 1985 | 1 | 0 |
| 1986 | 0 | 0 |
| 1987 | 1 | 0 |
| 1988 | 1 | 0 |
| 1989 | 0 | 0 |
| 1990 | 3 | 0 |
| 1991 | 0 | 0 |
| 1992 | 2 | 0 |
| 1993 | 2 | 0 |
| 1994 | 2 | 0 |
| 1995 | 1 | 0 |
| 1996 | 2 | 0 |
| 1997 | 0 | 0 |
| 1998 | 0 | 0 |
| 1999 | 1 | 0 |
| 2000 | 0 | 0 |
| 2001 | 2 | 0 |
| 2002 | 1 | 1 |
| 2003 | 4 | 5 |
| 2004 | 1 | 1 |
| 2005 | 2 | 4 |
| 2006 | 1 | 5 |
| 2007 | 4 | 5 |
| 2008 | 1 | 2 |
| 2009 | 2 | 4 |
| 2010 | 3 | 6 |
| 2011 | 2 | 2 |
| 2012 | 2 | 5 |
| 2013 | 4 | 2 |
| 2014 | 3 | 4 |
| 2015 | 4 | 18 |
| 2016 | 7 | 7 |
| 2017 | 9 | 12 |
| 2018 | 10 | 14 |
| 2019 | 15 | 11 |
| 2020 | 8 | 23 |
| 2021 | 18 | 28 |
| 2022 | 12 | 14 |
| 2023 | 15 | 22 |
| 2024 | 20 | 8 |
| 2025 | 13 | 4 |
| 2026 | 2 | 3 |
By publication year. Applications have been published since 2001. 2026 runs to 8 Oct.
Recent patents
- Engine system and method of operating the same14 Apr 2026US 12,601,303 B2ROLLS-ROYCE plc
- Three-stream gas turbine engine with embedded electric machine10 Mar 2026US 12,571,360 B2General Electric Deutschland Holding GmbH
- Aircraft dual-flow turbine engine assembly, the assembly being equipped with incidence-controlled air discharge fins25 Nov 2025US 12,480,452 B2Safran Aircraft Engines
- Limited slip torque-limiter coupling4 Nov 2025US 12,459,660 B1ROLLS-ROYCE plc
- System and method for operating a turboprop engine7 Oct 2025US 12,435,674 B2Pratt & Whitney Canada Corp.
- Gas Turbine Engine with Third Stream12 Feb 2026US 2026/0043376 A1General Electric Company
- Gas Turbine Engine with Third Stream12 Feb 2026US 2026/0043377 A1General Electric Company
- Gas Turbine Engine with Third Stream12 Feb 2026US 2026/0043378 A1General Electric Company
- Hybrid-electric gas turbine engine and method of operating21 Aug 2025US 2025/0264059 A1General Electric Company
- Method and device for optimizing a climb phase of an aircraft, in particular in terms of fuel consumption6 Mar 2025US 2025/0076893 A1Airbus Operations GmbH
Most cited
By later US patents
- Variable specific thrust turbofan engine152US 5,261,227 AGeneral Electric Company · 1993
- Three stream, variable area fixed aperture nozzle with pneumatic actuation69US 9,677,501 B2Rolls-Royce North American Technologies Inc. · 2017
- Three stream, variable area, vectorable nozzle69US 9,845,768 B2Rolls-Royce North American Technologies Inc. · 2017
- Optimal control for a gas turbine engine47US 4,258,545 AGeneral Electric Company · 1981
- Method and apparatus for controlling thrust in a gas turbine engine43US 4,275,557 AGeneral Electric Company · 1981