F05D 2250/43
With three degrees of freedom
Official title: with three degrees of freedom
F05D2250/43 (With three degrees of freedom) appears on 16 US grants and 16 published applications in this corpus.
Search patents in F05D- Granted patents
- 16
- Published applications
- 16
- Assignees
- 8
- Inventors
- 40
- Latest grant
- 25 Nov 2025
Filings by year
| Year | Granted patents | Published applications |
|---|---|---|
| 1996 | 1 | 0 |
| 1997 | 0 | 0 |
| 1998 | 0 | 0 |
| 1999 | 0 | 0 |
| 2000 | 0 | 0 |
| 2001 | 0 | 0 |
| 2002 | 1 | 0 |
| 2003 | 0 | 0 |
| 2004 | 0 | 0 |
| 2005 | 0 | 0 |
| 2006 | 0 | 0 |
| 2007 | 0 | 0 |
| 2008 | 0 | 0 |
| 2009 | 0 | 0 |
| 2010 | 0 | 0 |
| 2011 | 0 | 0 |
| 2012 | 0 | 0 |
| 2013 | 0 | 0 |
| 2014 | 1 | 1 |
| 2015 | 0 | 0 |
| 2016 | 1 | 2 |
| 2017 | 1 | 2 |
| 2018 | 1 | 3 |
| 2019 | 2 | 2 |
| 2020 | 5 | 4 |
| 2021 | 1 | 0 |
| 2022 | 1 | 0 |
| 2023 | 0 | 0 |
| 2024 | 0 | 1 |
| 2025 | 1 | 1 |
By publication year. Applications have been published since 2001.
Recent patents
- Gas turbine engine ducting system having a plurality of spherical joints25 Nov 2025US 12,480,458 B2ROLLS-ROYCE plc
- Multi-directional gearbox deflection limiter for a gas turbine engine18 Jan 2022US 11,225,914 B2General Electric Company
- Seal assembly for a turbo machine14 Sep 2021US 11,118,469 B2General Electric Company
- Thrust vector nozzle17 Nov 2020US 10,837,402 B2
- Turbine engine tie rod systems3 Nov 2020US 10,823,011 B2Raytheon Technologies Corporation
- Articulatable ducting systems10 Jul 2025US 2025/0223934 A1ROLLS-ROYCE plc
- Seal for gas turbine engine9 May 2024US 2024/0151152 A1Raytheon Technologies Corporation
- Turbine Engine Tie Rod Systems13 Aug 2020US 2020/0256216 A1United Technologies Corporation
- Seal Assembly for a Turbo Machine21 May 2020US 2020/0157964 A1General Electric Company
- Thrust Vector Nozzle7 May 2020US 2020/0141354 A1
Most cited
By later US patents
- Three degrees of freedom aft mounting system for gas turbine transition duct42US 6,442,946 B1Power Systems Mfg., LLC · 2002
- Articulated transition duct in turbomachine6US 8,707,673 B1General Electric Company · 2014
- Oil tank mount arrangement on a geared turbofan engine5US 9,951,655 B2United Technologies Corporation · 2018
- Multi-dimensional extending protective arm4US 9,359,063 B2United Technologies Corporation · 2016
- Additively manufactured connection for a turbine nozzle3US 10,184,344 B2General Electric Company · 2019