F23R 2900/03342
Arrangement of silo-type combustion chambers
F23R2900/03342 (Arrangement of silo-type combustion chambers) appears on 28 US grants and 22 published applications in this corpus.
Search patents in F23R- Granted patents
- 28
- Published applications
- 22
- Assignees
- 19
- Inventors
- 88
- Latest grant
- 8 Oct 2024
Filings by year
| Year | Granted patents | Published applications |
|---|---|---|
| 1982 | 1 | 0 |
| 1983 | 0 | 0 |
| 1984 | 0 | 0 |
| 1985 | 0 | 0 |
| 1986 | 0 | 0 |
| 1987 | 0 | 0 |
| 1988 | 0 | 0 |
| 1989 | 0 | 0 |
| 1990 | 0 | 0 |
| 1991 | 0 | 0 |
| 1992 | 0 | 0 |
| 1993 | 0 | 0 |
| 1994 | 2 | 0 |
| 1995 | 1 | 0 |
| 1996 | 0 | 0 |
| 1997 | 0 | 0 |
| 1998 | 0 | 0 |
| 1999 | 1 | 0 |
| 2000 | 1 | 0 |
| 2001 | 1 | 0 |
| 2002 | 0 | 0 |
| 2003 | 0 | 1 |
| 2004 | 1 | 1 |
| 2005 | 0 | 0 |
| 2006 | 0 | 0 |
| 2007 | 0 | 0 |
| 2008 | 0 | 0 |
| 2009 | 0 | 0 |
| 2010 | 1 | 2 |
| 2011 | 0 | 1 |
| 2012 | 0 | 3 |
| 2013 | 0 | 0 |
| 2014 | 1 | 1 |
| 2015 | 1 | 3 |
| 2016 | 1 | 3 |
| 2017 | 7 | 2 |
| 2018 | 3 | 2 |
| 2019 | 0 | 0 |
| 2020 | 2 | 1 |
| 2021 | 2 | 0 |
| 2022 | 0 | 1 |
| 2023 | 0 | 1 |
| 2024 | 2 | 0 |
By publication year. Applications have been published since 2001.
Recent patents
- Gas turbine combustor structure8 Oct 2024US 12,111,054 B2Toshiba Energy Systems & Solutions Corporation
- Gas turbine combustor structure6 Feb 2024US 11,892,169 B2Toshiba Energy Systems & Solutions Corporation
- Silo combustion chamber and method for retrofitting same12 Oct 2021US 11,143,403 B2Siemens Energy Global GmbH & Co. KG
- Bent combustion chamber from a turbine engine21 Sep 2021US 11,125,435 B2Safran Aircraft Engines
- Partial-load operation of a gas turbine with an adjustable bypass flow channel15 Sep 2020US 10,774,751 B2Siemens Aktiengesellschaft
- Gas turbine combustor structure28 Dec 2023US 2023/0417413 A1Toshiba Energy Systems & Solutions Corporation
- Gas turbine combustor structure21 Apr 2022US 2022/0120442 A1Toshiba Energy Systems & Solutions Corporation
- Silo combustion chamber and method for retrofitting same7 May 2020US 2020/0141580 A1Siemens Aktiengesellschaft
- Bent combustion chamber from a turbine engine26 Jul 2018US 2018/0209649 A1Safran Aircraft Engines
- System and method for impingement cooling of turbine system components24 May 2018US 2018/0142892 A1General Electric Technology GmbH
Most cited
By later US patents
- Dry low oxides of nitrogen lean premix module for industrial gas turbine engines111US 6,094,916 AAllison Engine Company, Inc. · 2000
- Method and apparatus for cooling hot gas casings54US 4,339,925 ABBC Brown, Boveri & Company, Limited · 1982
- Burner arrangement with interference burners for preventing pressure pulsations27US 5,983,643 AAsea Brown Boveri AG · 1999
- Dry low combustion system with means for eliminating combustion noise19US 6,691,515 B2ROLLS-ROYCE plc · 2004
- Lean premix combustion system having reduced combustion pressure oscillation17US 5,321,947 ASolar Turbines Incorporated · 1994