F05D 2240/128
Nozzles
F05D2240/128 (Nozzles) appears on 586 US grants and 666 published applications in this corpus.
Search patents in F05D- Granted patents
- 586
- Published applications
- 666
- Assignees
- 148
- Inventors
- 1,378
- Latest grant
- 6 Oct 2026
Filings by year
| Year | Granted patents | Published applications |
|---|---|---|
| 1976 | 2 | 0 |
| 1977 | 0 | 0 |
| 1978 | 0 | 0 |
| 1979 | 1 | 0 |
| 1980 | 0 | 0 |
| 1981 | 0 | 0 |
| 1982 | 0 | 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 | 0 | 0 |
| 1995 | 0 | 0 |
| 1996 | 0 | 0 |
| 1997 | 0 | 0 |
| 1998 | 0 | 0 |
| 1999 | 0 | 0 |
| 2000 | 0 | 0 |
| 2001 | 6 | 0 |
| 2002 | 3 | 6 |
| 2003 | 7 | 1 |
| 2004 | 2 | 6 |
| 2005 | 6 | 2 |
| 2006 | 3 | 4 |
| 2007 | 3 | 4 |
| 2008 | 3 | 1 |
| 2009 | 2 | 1 |
| 2010 | 2 | 12 |
| 2011 | 3 | 11 |
| 2012 | 5 | 5 |
| 2013 | 5 | 14 |
| 2014 | 9 | 9 |
| 2015 | 10 | 9 |
| 2016 | 10 | 63 |
| 2017 | 27 | 78 |
| 2018 | 31 | 75 |
| 2019 | 67 | 61 |
| 2020 | 81 | 62 |
| 2021 | 52 | 54 |
| 2022 | 78 | 55 |
| 2023 | 58 | 46 |
| 2024 | 57 | 40 |
| 2025 | 30 | 29 |
| 2026 | 23 | 18 |
By publication year. Applications have been published since 2001. 2026 runs to 8 Oct.
Subgroups
Granted patents
Recent patents
- Bearing for turbomachine variable pitch stator vane pivot, stator vane comprising such a bearing and turbomachine comprising such stator vanes6 Oct 2026US 12,753,705 B2Safran Aircraft Engines
- Turbocharger29 Sep 2026US 12,747,689 B2
- Sector of a turbine stator for a turbine of an aircraft turbomachine15 Sep 2026US 12,735,988 B2Safran Aircraft Engines
- Jet nozzle effective area control system for gas turbine engine8 Sep 2026US 12,729,658 B2Pratt & Whitney Canada Corp.
- Abrasive flow machining process for a meridionally divided turbine housing, and a masking fixture used in said process11 Aug 2026US 12,703,064 B2Garrett Transportation I Inc.
- Abrasive flow machining process for a meridionally divided turbine housing, and a masking fixture used in said process1 Oct 2026US 2026/0295774 A1Garrett Transportation I Inc.
- Gas turbine for controlling thermal expansion of vane carrier10 Sep 2026US 2026/0266198 A1Doosan Enerbility Co., Ltd.
- Turbine13 Aug 2026US 2026/0235048 A1Cummins Inc.
- Turbocharger23 Jul 2026US 2026/0210287 A1IHI Corporation
- Rocket engine using expander bleed cycle9 Jul 2026US 2026/0194030 A1
Most cited
By later US patents
- First stage turbine nozzle airfoil65US 6,736,599 B1General Electric Company · 2004
- Shroud assembly for gas turbine engine52US 10,301,960 B2General Electric Company · 2019
- Turbine nozzle segment band cooling41US 6,227,798 B1General Electric Company · 2001
- Columnar air moving devices, systems and methods41US 9,151,295 B2Airius IP Holdings, LLC · 2015
- Airfoil shape for a turbine nozzle40US 6,887,041 B2General Electric Company · 2005