F05D 2250/192
Bevelled
Official title: bevelled
F05D2250/192 (Bevelled) appears on 67 US grants and 64 published applications in this corpus.
Search patents in F05D- Granted patents
- 67
- Published applications
- 64
- Assignees
- 34
- Inventors
- 172
- Latest grant
- 20 Jan 2026
Filings by year
| Year | Granted patents | Published applications |
|---|---|---|
| 1976 | 1 | 0 |
| 1977 | 0 | 0 |
| 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 | 1 | 0 |
| 1989 | 0 | 0 |
| 1990 | 0 | 0 |
| 1991 | 1 | 0 |
| 1992 | 1 | 0 |
| 1993 | 0 | 0 |
| 1994 | 0 | 0 |
| 1995 | 2 | 0 |
| 1996 | 1 | 0 |
| 1997 | 0 | 0 |
| 1998 | 0 | 0 |
| 1999 | 0 | 0 |
| 2000 | 0 | 0 |
| 2001 | 1 | 0 |
| 2002 | 0 | 0 |
| 2003 | 0 | 2 |
| 2004 | 3 | 2 |
| 2005 | 0 | 3 |
| 2006 | 1 | 3 |
| 2007 | 1 | 1 |
| 2008 | 2 | 1 |
| 2009 | 2 | 3 |
| 2010 | 3 | 4 |
| 2011 | 2 | 2 |
| 2012 | 0 | 1 |
| 2013 | 1 | 2 |
| 2014 | 3 | 2 |
| 2015 | 1 | 7 |
| 2016 | 0 | 4 |
| 2017 | 7 | 5 |
| 2018 | 3 | 2 |
| 2019 | 2 | 2 |
| 2020 | 8 | 7 |
| 2021 | 6 | 6 |
| 2022 | 5 | 2 |
| 2023 | 3 | 1 |
| 2024 | 2 | 1 |
| 2025 | 2 | 1 |
| 2026 | 1 | 0 |
By publication year. Applications have been published since 2001. 2026 runs to 8 Oct.
Recent patents
- High pressure turbine blade double scarf cut20 Jan 2026US 12,529,319 B2Rtx Corporation
- Substrate edge configurations for ceramic coatings4 Nov 2025US 12,460,555 B2Rtx Corporation
- Self-centering seal and method of using same4 Nov 2025US 12,460,727 B2Rtx Corporation
- Undercut groove and chamfer for rim seal6 Aug 2024US 12,055,044 B1Pratt & Whitney Canada Corp.
- Substrate edge configurations for ceramic coatings5 Mar 2024US 11,920,478 B2Rtx Corporation
- High pressure turbine blade double scarf cut21 Aug 2025US 2025/0264024 A1Rtx Corporation
- Substrate Edge Configurations for Ceramic Coatings1 Aug 2024US 2024/0254889 A1Rtx Corporation
- Turbocharger turbine assembly29 Jun 2023US 2023/0203983 A1Garrett Transportation I Inc.
- Technique for cooling squealer tip of a gas turbine blade24 Mar 2022US 2022/0090511 A1Doosan Heavy Industries Construction Co., Ltd
- Rotor and turbo machine including same3 Mar 2022US 2022/0065120 A1Doosan Heavy Industries Construction Co., Ltd
Most cited
By later US patents
- Cooling arrangement for gas-turbine components56US 6,261,053 B1Asea Brown Boveri AG · 2001
- Blade baffle damper37US 3,966,357 AGeneral Electric Company · 1976
- Dynamic control of tip clearance33US 5,456,576 AUnited Technologies Corporation · 1995
- Structures of turbine scroll and blades27US 6,742,989 B2Mitsubishi Heavy Industries, Ltd. · 2004
- Turbine blade27US 6,824,359 B2United Technologies Corporation · 2004