F05D 2250/00
Geometry
F05D2250/00 (Geometry) appears on 9,271 US grants and 10,056 published applications in this corpus.
Search patents in F05D- Granted patents
- 9,271
- Published applications
- 10,056
- Assignees
- 1,371
- Inventors
- 14,555
- Latest grant
- 6 Oct 2026
Filings by year
| Year | Granted patents | Published applications |
|---|---|---|
| 1976 | 17 | 0 |
| 1977 | 15 | 0 |
| 1978 | 14 | 0 |
| 1979 | 18 | 0 |
| 1980 | 20 | 0 |
| 1981 | 18 | 0 |
| 1982 | 12 | 0 |
| 1983 | 28 | 0 |
| 1984 | 27 | 0 |
| 1985 | 28 | 0 |
| 1986 | 17 | 0 |
| 1987 | 28 | 0 |
| 1988 | 23 | 0 |
| 1989 | 36 | 0 |
| 1990 | 25 | 0 |
| 1991 | 28 | 0 |
| 1992 | 37 | 0 |
| 1993 | 31 | 0 |
| 1994 | 31 | 0 |
| 1995 | 21 | 0 |
| 1996 | 42 | 0 |
| 1997 | 30 | 0 |
| 1998 | 30 | 0 |
| 1999 | 37 | 0 |
| 2000 | 44 | 0 |
| 2001 | 68 | 19 |
| 2002 | 90 | 69 |
| 2003 | 83 | 59 |
| 2004 | 81 | 122 |
| 2005 | 70 | 153 |
| 2006 | 103 | 174 |
| 2007 | 108 | 234 |
| 2008 | 106 | 283 |
| 2009 | 185 | 250 |
| 2010 | 194 | 329 |
| 2011 | 208 | 275 |
| 2012 | 291 | 326 |
| 2013 | 258 | 445 |
| 2014 | 291 | 391 |
| 2015 | 334 | 514 |
| 2016 | 283 | 775 |
| 2017 | 417 | 696 |
| 2018 | 556 | 783 |
| 2019 | 812 | 722 |
| 2020 | 863 | 774 |
| 2021 | 668 | 613 |
| 2022 | 749 | 506 |
| 2023 | 597 | 544 |
| 2024 | 608 | 464 |
| 2025 | 411 | 298 |
| 2026 | 180 | 238 |
By publication year. Applications have been published since 2001. 2026 runs to 8 Oct.
Subgroups
Granted patents
- F05D 2250/70ShapeIndexing code2,572
- F05D 2250/10Two-dimensionalIndexing code2,339
- F05D 2250/20Three-dimensionalIndexing code2,204
- F05D 2250/50Inlet or outletIndexing code1,605
- F05D 2250/30Arrangement of componentsIndexing code1,601
- F05D 2250/60StructureIndexing code401
- F05D 2250/40Movement of componentsIndexing code368
- F05D 2250/90Variable geometryIndexing code184
All 9 subgroupsShow fewer
Recent patents
- Cooling features for a component of a gas turbine engine6 Oct 2026US 12,753,697 B2Rtx Corporation
- Turbine engine vane baffle6 Oct 2026US 12,753,698 B1Rtx Corporation
- Noise reducing device having an obliquely pierced honeycomb structure6 Oct 2026US 12,753,720 B2Safran Aircraft Engines
- Turbocharger29 Sep 2026US 12,747,674 B2IHI Corporation
- Thrust reverser with blocker door opening control device(s)29 Sep 2026US 12,747,714 B2Rohr, Inc.
- Power turbine nozzles in gas turbine engines8 Oct 2026US 2026/0309047 A1GE AEROSPACE POLAND sp. z o. o.
- Method for manufacturing a vane made from composite material comprising a serration element and an anti-erosion coating1 Oct 2026US 2026/0295949 A1Safran Aerospace Composites
- Flow deflector having channels with double ejection angles1 Oct 2026US 2026/0298265 A1Safran Aircraft Engines
- Airfoils for gas turbine engines24 Sep 2026US 2026/0286849 A1General Electric Company
- Gas turbine structural component24 Sep 2026US 2026/0286861 A1
Most cited
By later US patents
- Expandable impeller pump391US 7,393,181 B2Datascope Investment Corp. · 2008
- Low solidity turbofan352US 7,374,403 B2General Electric Company · 2008
- Film cooling hole for turbine airfoil313US 7,997,868 B1Florida Turbine Technologies, Inc. · 2011
- Expandable impeller pump296US 7,927,068 B2The Penn State Research Foundation · 2011
- System for reducing noise in a hydraulic fracturing fleet263US 9,587,649 B2U.S. Well Services, LLC · 2017