F02C 3/13
Having variable working fluid interconnections between turbines or compressors or stages of
Official title: having variable working fluid interconnections between turbines or compressors or stages of different rotors {(controlling flow ratio between different flows of multi-flow jet-propulsion plant, e.g. ducted fan F02K3/075)}
F02C3/13 (Having variable working fluid interconnections between turbines or compressors or stages of) appears on 173 US grants and 205 published applications in this corpus.
Search patents in F02C- Granted patents
- 173
- Published applications
- 205
- Assignees
- 59
- Inventors
- 414
- Latest grant
- 8 Sep 2026
Filings by year
| Year | Granted patents | Published applications |
|---|---|---|
| 1989 | 2 | 0 |
| 1990 | 0 | 0 |
| 1991 | 1 | 0 |
| 1992 | 1 | 0 |
| 1993 | 0 | 0 |
| 1994 | 1 | 0 |
| 1995 | 0 | 0 |
| 1996 | 0 | 0 |
| 1997 | 1 | 0 |
| 1998 | 0 | 0 |
| 1999 | 0 | 0 |
| 2000 | 1 | 0 |
| 2001 | 3 | 0 |
| 2002 | 1 | 1 |
| 2003 | 2 | 5 |
| 2004 | 2 | 3 |
| 2005 | 5 | 3 |
| 2006 | 2 | 5 |
| 2007 | 2 | 5 |
| 2008 | 2 | 1 |
| 2009 | 2 | 6 |
| 2010 | 3 | 5 |
| 2011 | 4 | 3 |
| 2012 | 2 | 6 |
| 2013 | 6 | 16 |
| 2014 | 4 | 12 |
| 2015 | 10 | 17 |
| 2016 | 11 | 25 |
| 2017 | 10 | 16 |
| 2018 | 15 | 11 |
| 2019 | 12 | 13 |
| 2020 | 17 | 16 |
| 2021 | 13 | 6 |
| 2022 | 9 | 6 |
| 2023 | 9 | 8 |
| 2024 | 12 | 7 |
| 2025 | 6 | 4 |
| 2026 | 2 | 5 |
By publication year. Applications have been published since 2001. 2026 runs to 8 Oct.
Recent patents
- High temperature anti-ice systems for aircraft engines8 Sep 2026US 12,729,645 B2General Electric Company
- Power generating system for a gas turbine engine comprising a compressor bleed air to exhaust heat exchanger16 Jun 2026US 12,655,793 B1General Electric Company
- Aircraft propulsion system engine with multiple independent rotating structures30 Sep 2025US 12,428,986 B2Rtx Corporation
- High temperature anti-ice systems for aircraft engines30 Sep 2025US 12,428,988 B1General Electric Company
- Powerplant with multiple integrated gas turbine engines19 Aug 2025US 12,392,296 B2Rtx Corporation
- Variable bleed valve assemblies8 Oct 2026US 2026/0309077 A1General Electric Company
- Aircraft propulsion system with auxiliary flowpath system30 Jul 2026US 2026/0218655 A1Rtx Corporation
- High temperature anti-ice systems for aircraft engines19 Feb 2026US 2026/0049571 A1General Electric Company
- Gas turbine system and bleed control method thereof12 Feb 2026US 2026/0043359 A1Mitsubishi Heavy Industries, Ltd.
- Open rotor with aerodynamically isolatable free turbine15 Jan 2026US 2026/0015968 A1Rtx Corporation
Most cited
By later US patents
- Advanced integrated propulsion system with total optimized cycle for gas turbines111US 4,858,428 A1989
- Combination propulsion system for a flying craft92US 5,014,508 AMesserschmitt-Boelkow-Blohm GmbH · 1991
- Compressor system and methods for reducing cooling airflow71US 6,250,061 B1General Electric Company · 2001
- Integrated variable geometry flow restrictor and heat exchanger71US 8,961,114 B2General Electric Company · 2015
- Variable cycle turbine engine65US 8,943,796 B2United Technologies Corporation · 2015