F02C 3/365
A part of the compressed air being burned, the other part being
Official title: {a part of the compressed air being burned, the other part being heated indirectly (in a fluidised-bed combustor F02C3/205)}
F02C3/365 (A part of the compressed air being burned, the other part being) appears on 16 US grants and 9 published applications in this corpus.
Search patents in F02C- Granted patents
- 16
- Published applications
- 9
- Assignees
- 13
- Inventors
- 30
- Latest grant
- 17 Jun 2025
Filings by year
| Year | Granted patents | Published applications |
|---|---|---|
| 1979 | 1 | 0 |
| 1980 | 1 | 0 |
| 1981 | 0 | 0 |
| 1982 | 1 | 0 |
| 1983 | 1 | 0 |
| 1984 | 1 | 0 |
| 1985 | 0 | 0 |
| 1986 | 0 | 0 |
| 1987 | 0 | 0 |
| 1988 | 0 | 0 |
| 1989 | 0 | 0 |
| 1990 | 0 | 0 |
| 1991 | 0 | 0 |
| 1992 | 1 | 0 |
| 1993 | 2 | 0 |
| 1994 | 0 | 0 |
| 1995 | 0 | 0 |
| 1996 | 0 | 0 |
| 1997 | 0 | 0 |
| 1998 | 0 | 0 |
| 1999 | 0 | 0 |
| 2000 | 0 | 0 |
| 2001 | 1 | 0 |
| 2002 | 1 | 2 |
| 2003 | 0 | 0 |
| 2004 | 2 | 1 |
| 2005 | 0 | 0 |
| 2006 | 0 | 0 |
| 2007 | 0 | 0 |
| 2008 | 0 | 0 |
| 2009 | 0 | 0 |
| 2010 | 0 | 1 |
| 2011 | 0 | 0 |
| 2012 | 0 | 0 |
| 2013 | 0 | 1 |
| 2014 | 0 | 1 |
| 2015 | 0 | 0 |
| 2016 | 0 | 0 |
| 2017 | 1 | 0 |
| 2018 | 0 | 0 |
| 2019 | 0 | 0 |
| 2020 | 0 | 0 |
| 2021 | 0 | 0 |
| 2022 | 0 | 0 |
| 2023 | 1 | 0 |
| 2024 | 1 | 2 |
| 2025 | 1 | 1 |
By publication year. Applications have been published since 2001.
Recent patents
- Bottoming cycle for waste heat recovery and engine cooling17 Jun 2025US 12,331,678 B2Rtx Corporation
- Air bottoming cycle driven propulsor9 Jul 2024US 12,031,478 B2Rtx Corporation
- Turbine engine bleed waste heat recovery18 Jul 2023US 11,702,981 B1Raytheon Technologies Corporation
- Turbo-engine, particularly internal combustion engine12 Sep 2017US 9,759,067 B2Aella SA
- Re-fired gas turbine engine16 Nov 2004US 6,817,187 B2Alstom (Switzerland) Ltd
- Combustion System with Pollution Abatement by Catalysts and Non-Thermal Plasma for Aircraft and Industrial Gas Turbines31 Jul 2025US 2025/0243801 A1
- Air bottoming cycle driven propulsor11 Apr 2024US 2024/0117764 A1Raytheon Technologies Corporation
- Bottoming cycle for waste heat recovery and engine cooling14 Mar 2024US 2024/0084731 A1Rtx Corporation
- Turbo-engine, particularly internal combustion engine17 Apr 2014US 2014/0102115 A1Aella SA
- Gas turbine engine air cycle system7 Mar 2013US 2013/0055724 A1
Most cited
By later US patents
- Re-fired gas turbine engine98US 6,817,187 B2Alstom (Switzerland) Ltd · 2004
- Radiant energy collection and conversion apparatus and method38US 4,313,304 AThe United States of America as represented by the United States Department of Energy · 1982
- Process and system for producing power22US 5,181,376 AFluor Corporation · 1993
- Combined cycle power plant with pressurized fluidized bed combustor21US 4,223,529 AGeneral Electric Company · 1980
- Radiation receiver19US 4,403,601 A1983