F23M 2900/05002
Means for accommodate thermal expansion of the wall liner
F23M2900/05002 (Means for accommodate thermal expansion of the wall liner) appears on 42 US grants and 47 published applications in this corpus.
Search patents in F23M- Granted patents
- 42
- Published applications
- 47
- Assignees
- 31
- Inventors
- 117
- Latest grant
- 9 Dec 2025
Filings by year
| Year | Granted patents | Published applications |
|---|---|---|
| 1998 | 1 | 0 |
| 1999 | 1 | 0 |
| 2000 | 1 | 0 |
| 2001 | 0 | 1 |
| 2002 | 3 | 2 |
| 2003 | 0 | 2 |
| 2004 | 3 | 1 |
| 2005 | 1 | 0 |
| 2006 | 0 | 2 |
| 2007 | 0 | 3 |
| 2008 | 1 | 2 |
| 2009 | 0 | 4 |
| 2010 | 2 | 4 |
| 2011 | 1 | 0 |
| 2012 | 4 | 1 |
| 2013 | 2 | 1 |
| 2014 | 3 | 5 |
| 2015 | 0 | 6 |
| 2016 | 1 | 0 |
| 2017 | 6 | 3 |
| 2018 | 3 | 1 |
| 2019 | 2 | 3 |
| 2020 | 1 | 1 |
| 2021 | 1 | 2 |
| 2022 | 3 | 1 |
| 2023 | 1 | 1 |
| 2024 | 0 | 0 |
| 2025 | 1 | 1 |
By publication year. Applications have been published since 2001.
Recent patents
- Combustor for a gas turbine engine9 Dec 2025US 12,492,821 B2General Electric Company
- Combustor for a gas turbine engine3 Oct 2023US 11,774,098 B2General Electric Company
- Gas turbine engine combustor with ceramic matrix composite liner11 Oct 2022US 11,466,855 B2Rolls-Royce North American Technologies Inc.
- Combustor liner attachment assembly for gas turbine engine5 Apr 2022US 11,293,637 B2Raytheon Technologies Corporation
- Combustion chamber having a double chamber bottom15 Feb 2022US 11,248,793 B2Safran Aircraft Engines
- Probe Motion Compensation22 May 2025US 2025/0163824 A1General Electric Company
- Combustor for a gas turbine engine28 Dec 2023US 2023/0417415 A1General Electric Company
- Combustor for a gas turbine engine8 Dec 2022US 2022/0390110 A1General Electric Company
- Gas turbine engine combustor with ceramic matrix composite liner21 Oct 2021US 2021/0325043 A1Rolls-Royce North American Technologies Inc.
- Combustion chamber having a double chamber bottom13 May 2021US 2021/0140639 A1Safran Aircraft Engines
Most cited
By later US patents
- Ceramic matrix composite combustor vane ring assembly28US 9,335,051 B2United Technologies Corporation · 2016
- Architecture for a combustion chamber made of ceramic matrix material24US 6,679,062 B2Snecma Moteurs · 2004
- Ceramic liner23US 5,957,067 AABB Research Ltd. · 1999
- Combustor apparatus for a gas turbine engine22US 6,401,447 B1Allison Advanced Development Company · 2002
- Combustion apparatus17US 8,256,224 B2ROLLS-ROYCE plc · 2012