F05D 2250/713
Inflexed
Official title: inflexed
F05D2250/713 (Inflexed) appears on 164 US grants and 181 published applications in this corpus.
Search patents in F05D- Granted patents
- 164
- Published applications
- 181
- Assignees
- 77
- Inventors
- 434
- Latest grant
- 16 Jun 2026
Filings by year
| Year | Granted patents | Published applications |
|---|---|---|
| 1978 | 1 | 0 |
| 1979 | 0 | 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 | 2 | 0 |
| 1995 | 0 | 0 |
| 1996 | 0 | 0 |
| 1997 | 1 | 0 |
| 1998 | 0 | 0 |
| 1999 | 0 | 0 |
| 2000 | 0 | 0 |
| 2001 | 1 | 2 |
| 2002 | 2 | 1 |
| 2003 | 3 | 1 |
| 2004 | 1 | 1 |
| 2005 | 0 | 0 |
| 2006 | 0 | 1 |
| 2007 | 0 | 1 |
| 2008 | 2 | 4 |
| 2009 | 1 | 4 |
| 2010 | 1 | 4 |
| 2011 | 0 | 3 |
| 2012 | 5 | 9 |
| 2013 | 4 | 10 |
| 2014 | 6 | 2 |
| 2015 | 9 | 20 |
| 2016 | 11 | 15 |
| 2017 | 7 | 9 |
| 2018 | 11 | 6 |
| 2019 | 14 | 17 |
| 2020 | 11 | 13 |
| 2021 | 12 | 14 |
| 2022 | 18 | 5 |
| 2023 | 11 | 13 |
| 2024 | 10 | 10 |
| 2025 | 15 | 9 |
| 2026 | 5 | 7 |
By publication year. Applications have been published since 2001. 2026 runs to 8 Oct.
Recent patents
- Turbine component having pin-fin cooling structure, and gas turbine including same16 Jun 2026US 12,655,768 B2Doosan Enerbility Co., Ltd.
- Centrifugal compressor impeller and method of producing the same24 Mar 2026US 12,584,492 B2Pratt & Whitney Canada Corp.
- Gas turbine engine rotor blade geometry and method for selecting same10 Mar 2026US 12,571,313 B2Pratt & Whitney Canada Corp.
- Rocket engine with dual contour nozzle17 Feb 2026US 12,553,404 B2Innovative Rocket Technologies Inc.
- Turbine wheel20 Jan 2026US 12,529,317 B2Kabushiki Kaisha Toyota Jidoshokki
- Centrifugal compressor impeller and method of producing the same6 Aug 2026US 2026/0226911 A1Pratt & Whitney Canada Corp.
- Fixed radial inlet guide vanes configured to direct exhaust to a turbine25 Jun 2026US 2026/0176977 A1Garrett Transportation I Inc.
- Turbine Engine Rotor Blade With Contoured Pocket Surface(S)2 Apr 2026US 2026/0092530 A1Pratt & Whitney Canada Corp.
- Transition duct for gas turbine engine5 Mar 2026US 2026/0063042 A1Siemens Energy Global GmbH & Co. KG
- Aircraft Heat Exchanger15 Jan 2026US 2026/0015972 A1Rtx Corporation
Most cited
By later US patents
- Swept turbomachinery blade99US 5,642,985 AUnited Technologies Corporation · 1997
- Curved blade turbomachinery noise reduction62US 4,131,387 AGeneral Electric Company · 1978
- Rotator member and method53US 6,341,942 B12002
- Method and apparatus for reducing rotor assembly circumferential rim stress44US 6,524,070 B1General Electric Company · 2003
- Light weight steam turbine blade33US 5,352,092 AWestinghouse Electric Corp. · 1994