F05D 2210/43
Radial inlet and axial outlet
F05D2210/43 (Radial inlet and axial outlet) appears on 29 US grants and 36 published applications in this corpus.
Search patents in F05D- Granted patents
- 29
- Published applications
- 36
- Assignees
- 31
- Inventors
- 94
- Latest grant
- 23 Sep 2025
Filings by year
| Year | Granted patents | Published applications |
|---|---|---|
| 1979 | 1 | 0 |
| 1980 | 0 | 0 |
| 1981 | 1 | 0 |
| 1982 | 0 | 0 |
| 1983 | 0 | 0 |
| 1984 | 1 | 0 |
| 1985 | 1 | 0 |
| 1986 | 0 | 0 |
| 1987 | 0 | 0 |
| 1988 | 1 | 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 | 0 | 1 |
| 2002 | 0 | 0 |
| 2003 | 1 | 0 |
| 2004 | 0 | 0 |
| 2005 | 0 | 0 |
| 2006 | 0 | 0 |
| 2007 | 0 | 0 |
| 2008 | 0 | 1 |
| 2009 | 0 | 0 |
| 2010 | 0 | 3 |
| 2011 | 0 | 2 |
| 2012 | 1 | 1 |
| 2013 | 2 | 3 |
| 2014 | 3 | 2 |
| 2015 | 1 | 2 |
| 2016 | 1 | 3 |
| 2017 | 2 | 1 |
| 2018 | 1 | 6 |
| 2019 | 2 | 5 |
| 2020 | 3 | 1 |
| 2021 | 3 | 1 |
| 2022 | 1 | 1 |
| 2023 | 2 | 1 |
| 2024 | 0 | 1 |
| 2025 | 1 | 1 |
By publication year. Applications have been published since 2001.
Recent patents
- Aircraft engine with exhaust having removable deflector23 Sep 2025US 12,420,941 B2Pratt & Whitney Canada Corp.
- Cooling method for a high-temperature radial gas turbine engine19 Dec 2023US 11,846,202 B2TurboGen, LLC
- Variable guide vane control system16 May 2023US 11,649,734 B1Pratt & Whitney Canada Corp.
- Turbine wheel for a turbine11 Jan 2022US 11,220,908 B2BorgWarner Inc.
- Radial inflow turbine, turbocharger, and method for assembling turbocharger1 Jun 2021US 11,021,959 B2Mitsubishi Heavy Industries, Ltd.
- Process assembly with rotor assembly and process device31 Jul 2025US 2025/0242290 A1GE-Hitachi Nuclear Energy Americas LLC
- Aircraft engine with exhaust having removable deflector6 Jun 2024US 2024/0182178 A1Pratt & Whitney Canada Corp.
- Engines28 Dec 2023US 2023/0417184 A1Reaction Engines Limited
- Cooling Method for a High-Temperature Radial Gas Turbine Engine5 May 2022US 2022/0136458 A1TurboGen, LLC
- Radial variable inlet guide vane for axial or axi-centrifugal compressors29 Jul 2021US 2021/0231052 A1General Electric Company
Most cited
By later US patents
- Sealing system for a turboexpander compressor56US 4,477,223 ATexas Turbine, Inc. · 1984
- Rotary device with bypass system38US 4,152,092 A1979
- Impeller shroud of a centrifugal compressor37US 4,264,271 AAvco Corporation · 1981
- Anti-erosion labyrinth seal25US 4,721,313 AAtlas Copco Comptec, LLC · 1988
- Bleed valve of a compressor, in particular a compressor of a bypass aero-engine19US 6,588,195 B2Rolls-Royce Deutschland Ltd & Co KG · 2003