F02C 3/062
The turbine being of the radial-flow type
Official title: {the turbine being of the radial-flow type}
F02C3/062 (The turbine being of the radial-flow type) appears on 8 US grants and 12 published applications in this corpus.
Search patents in F02C- Granted patents
- 8
- Published applications
- 12
- Assignees
- 6
- Inventors
- 24
- Latest grant
- 15 Apr 2025
Filings by year
| Year | Granted patents | Published applications |
|---|---|---|
| 1999 | 1 | 0 |
| 2000 | 0 | 0 |
| 2001 | 0 | 0 |
| 2002 | 0 | 0 |
| 2003 | 0 | 0 |
| 2004 | 0 | 0 |
| 2005 | 0 | 0 |
| 2006 | 0 | 0 |
| 2007 | 0 | 0 |
| 2008 | 0 | 0 |
| 2009 | 0 | 0 |
| 2010 | 0 | 0 |
| 2011 | 0 | 0 |
| 2012 | 0 | 0 |
| 2013 | 0 | 1 |
| 2014 | 0 | 0 |
| 2015 | 0 | 1 |
| 2016 | 1 | 0 |
| 2017 | 1 | 4 |
| 2018 | 0 | 2 |
| 2019 | 0 | 0 |
| 2020 | 1 | 2 |
| 2021 | 0 | 1 |
| 2022 | 2 | 0 |
| 2023 | 1 | 0 |
| 2024 | 0 | 1 |
| 2025 | 1 | 0 |
By publication year. Applications have been published since 2001.
Recent patents
- Cooling structure for radial turbine15 Apr 2025US 12,276,224 B2Honda Motor Co., Ltd.
- Bleed expander cooling with turbine5 Sep 2023US 11,746,701 B2Rolls-Royce North American Technologies Inc.
- Gas turbine engine flow control11 Oct 2022US 11,466,628 B2ROLLS-ROYCE plc
- Control of clearance between aircraft rotor blades and a casing3 May 2022US 11,319,830 B2Safran Aircraft Engines
- Turbine engine with a fire chamber and a helical fan24 Mar 2020US 10,598,019 B1
- Cooling structure for radial turbine26 Sep 2024US 2024/0318591 A1Honda Motor Co., Ltd.
- Gas turbine engine flow control4 Mar 2021US 2021/0062732 A1ROLLS-ROYCE plc
- Control of clearance between aircraft rotor blades and a casing19 Nov 2020US 2020/0362719 A1Safran Aircraft Engines
- Bleed expander cooling with turbine12 Nov 2020US 2020/0355121 A1Rolls-Royce North American Technologies Inc.
- Gear system architecture for gas turbine engine23 Aug 2018US 2018/0238241 A1United Technologies Corporation
Most cited
By later US patents
- Gear system architecture for gas turbine engine13US 9,840,969 B2United Technologies Corporation · 2017
- Jet engine having radial turbine blades and flow-directing turbine manifolds12US 5,996,336 A1999
- Reaction turbine and hybrid impulse reaction turbine9US 9,255,478 B2Hybrid Turbine Group · 2016
- Turbine engine with a fire chamber and a helical fan1US 10,598,019 B12020
- Cooling structure for radial turbine1US 12,276,224 B2Honda Motor Co., Ltd. · 2025