F02K 1/085
By transversely deforming an internal member
Official title: {by transversely deforming an internal member}
F02K1/085 (By transversely deforming an internal member) appears on 32 US grants and 32 published applications in this corpus.
Search patents in F02K- Granted patents
- 32
- Published applications
- 32
- Assignees
- 15
- Inventors
- 69
- Latest grant
- 17 Mar 2026
Filings by year
| Year | Granted patents | Published applications |
|---|---|---|
| 1980 | 1 | 0 |
| 1981 | 1 | 0 |
| 1982 | 0 | 0 |
| 1983 | 0 | 0 |
| 1984 | 0 | 0 |
| 1985 | 0 | 0 |
| 1986 | 0 | 0 |
| 1987 | 0 | 0 |
| 1988 | 0 | 0 |
| 1989 | 1 | 0 |
| 1990 | 0 | 0 |
| 1991 | 0 | 0 |
| 1992 | 0 | 0 |
| 1993 | 0 | 0 |
| 1994 | 0 | 0 |
| 1995 | 0 | 0 |
| 1996 | 0 | 0 |
| 1997 | 0 | 0 |
| 1998 | 1 | 0 |
| 1999 | 1 | 0 |
| 2000 | 0 | 0 |
| 2001 | 0 | 0 |
| 2002 | 0 | 0 |
| 2003 | 0 | 0 |
| 2004 | 0 | 0 |
| 2005 | 0 | 0 |
| 2006 | 1 | 1 |
| 2007 | 0 | 1 |
| 2008 | 0 | 2 |
| 2009 | 0 | 3 |
| 2010 | 1 | 2 |
| 2011 | 2 | 1 |
| 2012 | 2 | 2 |
| 2013 | 1 | 2 |
| 2014 | 2 | 3 |
| 2015 | 2 | 2 |
| 2016 | 3 | 3 |
| 2017 | 3 | 0 |
| 2018 | 0 | 1 |
| 2019 | 2 | 2 |
| 2020 | 3 | 1 |
| 2021 | 0 | 1 |
| 2022 | 2 | 0 |
| 2023 | 0 | 0 |
| 2024 | 0 | 1 |
| 2025 | 1 | 2 |
| 2026 | 2 | 2 |
By publication year. Applications have been published since 2001. 2026 runs to 8 Oct.
Recent patents
- Cooled variable area nozzle for an aircraft engine17 Mar 2026US 12,578,092 B2Rtx Corporation
- Gas turbine engine with third stream24 Feb 2026US 12,560,132 B2General Electric Company
- Seal system using layers of seal segments forced into sealing engagement using tension cable20 May 2025US 12,305,526 B2GE Infrastructure Technology LLC
- Internal structure of a primary exhaust duct having a separator of which the geometry varies depending on the temperature6 Dec 2022US 11,519,302 B2Airbus Operations GmbH
- Ramjet engine with rotating detonation combustion system and method for operation14 Jun 2022US 11,359,578 B2General Electric Company
- Jet nozzle effective area control system for gas turbine engine26 Feb 2026US 2026/0055741 A1Pratt & Whitney Canada Corp.
- Jet nozzle effective area control system for gas turbine engine26 Feb 2026US 2026/0055744 A1Pratt & Whitney Canada Corp.
- Cooled variable area nozzle for an aircraft engine17 Jul 2025US 2025/0230930 A1Rtx Corporation
- Gas turbine engine with third stream10 Apr 2025US 2025/0116243 A1General Electric Company
- Seal system using layers of seal segments forced into sealing engagement using tension cable7 Nov 2024US 2024/0368994 A1GE Infrastructure Technology LLC
Most cited
By later US patents
- Plug-type exhaust nozzle having a variable centerbody and translating shroud47US 4,802,629 AThe Boeing Company · 1989
- Variable area exhaust nozzle22US 4,241,876 AGeneral Motors Corporation · 1980
- Stowable mixer ejection nozzle17US 5,941,065 AThe Boeing Company · 1999
- High flow plug nozzle apparatus and method of using the same14US 10,724,472 B1Aerion Intellectual Property Management Corporation · 2020
- Two-dimensional nozzle10US 4,295,611 AUnited Technologies Corporation · 1981