F05D 2250/74
Given by a set or table of xyz-coordinates
Official title: given by a set or table of xyz-coordinates
F05D2250/74 (Given by a set or table of xyz-coordinates) appears on 436 US grants and 393 published applications in this corpus.
Search patents in F05D- Granted patents
- 436
- Published applications
- 393
- Assignees
- 46
- Inventors
- 718
- Latest grant
- 21 Jul 2026
Filings by year
| Year | Granted patents | Published applications |
|---|---|---|
| 2002 | 1 | 0 |
| 2003 | 0 | 0 |
| 2004 | 3 | 3 |
| 2005 | 4 | 6 |
| 2006 | 3 | 4 |
| 2007 | 2 | 18 |
| 2008 | 12 | 48 |
| 2009 | 46 | 19 |
| 2010 | 10 | 18 |
| 2011 | 20 | 8 |
| 2012 | 18 | 25 |
| 2013 | 17 | 23 |
| 2014 | 26 | 13 |
| 2015 | 16 | 11 |
| 2016 | 6 | 17 |
| 2017 | 15 | 23 |
| 2018 | 25 | 78 |
| 2019 | 71 | 20 |
| 2020 | 46 | 19 |
| 2021 | 14 | 8 |
| 2022 | 35 | 7 |
| 2023 | 20 | 5 |
| 2024 | 9 | 6 |
| 2025 | 10 | 5 |
| 2026 | 7 | 9 |
By publication year. 2026 runs to 8 Oct.
Recent patents
- Turbine rotor blade airfoil profile21 Jul 2026US 12,687,113 B1GE Vernova Infrastructure Technology LLC
- Turbine engine airfoil5 May 2026US 12,618,330 B2Pratt & Whitney Canada Corp.
- Turbine engine airfoil10 Mar 2026US 12,571,323 B2Pratt & Whitney Canada Corp.
- Turbine rotor blade tip shroud surface and edge profiles24 Feb 2026US 12,560,089 B1GE Vernova Infrastructure Technology LLC
- Adaptive component overhaul using structured light scan data17 Feb 2026US 12,551,974 B2Pratt & Whitney Canada Corp.
- Power turbine nozzles in gas turbine engines8 Oct 2026US 2026/0309047 A1GE AEROSPACE POLAND sp. z o. o.
- Adaptive component overhaul using structured light scan data18 Jun 2026US 2026/0166659 A1Pratt & Whitney Canada Corp.
- Turbine Engine Airfoil with Cooling Hole Pattern19 Mar 2026US 2026/0078676 A1Rtx Corporation
- Turbine engine airfoil with cooling hole pattern19 Mar 2026US 2026/0078677 A1Rtx Corporation
- Turbine blade tip shroud with axially offset cutter teeth, and related surface profiles and method26 Feb 2026US 2026/0055709 A1GE Vernova Infrastructure Technology LLC
Most cited
By later US patents
- Airfoil shape for a turbine bucket102US 6,910,868 B2General Electric Company · 2005
- Airfoil shape for a turbine bucket97US 6,854,961 B2General Electric Company · 2005
- Second stage turbine bucket airfoil78US 6,685,434 B1General Electric Company · 2004
- Stator blade airfoil profile for a compressor66US 7,329,092 B2General Electric Company · 2008
- LP turbine vane airfoil profile59US 7,367,779 B2Pratt & Whitney Canada Corp. · 2008