F05D 2250/282
Cubic pattern
Official title: cubic pattern
F05D2250/282 (Cubic pattern) appears on 21 US grants and 29 published applications in this corpus.
Search patents in F05D- Granted patents
- 21
- Published applications
- 29
- Assignees
- 17
- Inventors
- 83
- Latest grant
- 16 Jun 2026
Filings by year
| Year | Granted patents | Published applications |
|---|---|---|
| 2001 | 0 | 1 |
| 2002 | 1 | 2 |
| 2003 | 2 | 1 |
| 2004 | 1 | 0 |
| 2005 | 0 | 0 |
| 2006 | 0 | 0 |
| 2007 | 0 | 0 |
| 2008 | 0 | 0 |
| 2009 | 0 | 0 |
| 2010 | 0 | 1 |
| 2011 | 0 | 0 |
| 2012 | 0 | 0 |
| 2013 | 0 | 1 |
| 2014 | 0 | 0 |
| 2015 | 0 | 2 |
| 2016 | 1 | 1 |
| 2017 | 0 | 2 |
| 2018 | 1 | 2 |
| 2019 | 4 | 2 |
| 2020 | 0 | 4 |
| 2021 | 2 | 0 |
| 2022 | 0 | 2 |
| 2023 | 5 | 3 |
| 2024 | 1 | 2 |
| 2025 | 2 | 2 |
| 2026 | 1 | 1 |
By publication year. 2026 runs to 8 Oct.
Recent patents
- Coating system and method for maintenance thereof16 Jun 2026US 12,655,066 B2ROLLS-ROYCE plc
- System and method for turbomachine with local vortex generator array29 Apr 2025US 12,286,896 B2Honeywell International Inc.
- Auxetic three-dimensional structure utilized in additive manufacturing applications18 Feb 2025US 12,228,046 B2Siemens Energy Global GmbH & Co. KG
- System and method for turbomachine with local vortex generator array30 Jan 2024US 11,885,234 B2Honeywell International Inc.
- Turbomachine hollow blade7 Nov 2023US 11,808,179 B2Safran Helicopter Engines
- Acoustic structure with array of interconnected resonators, and anti-icing system30 Apr 2026US 2026/0117700 A1Rtx Corporation
- Turbine engine with compliant axial retainer20 Nov 2025US 2025/0354494 A1General Electric Company
- Turbine engine with compliant axial retainer3 Apr 2025US 2025/0109690 A1General Electric Company
- Coating system and method for maintenance thereof29 Aug 2024US 2024/0286960 A1ROLLS-ROYCE plc
- System and method for turbomachine with local vortex generator array6 Jun 2024US 2024/0183274 A1Honeywell International Inc.
Most cited
By later US patents
- Profiled surface used as an abradable in flow machines40US 6,457,939 B2Sulzer Metco AG · 2002
- Gas turbine engine blade containment assembly15US 6,543,991 B2ROLLS-ROYCE plc · 2003
- Gas turbine split ring15US 6,602,048 B2Mitsubishi Heavy Industries, Ltd. · 2003
- Turbine abradable layer with zig zag groove pattern15US 9,243,511 B2Siemens Aktiengesellschaft · 2016
- Gas turbine engine blade containment assembly8US 6,739,830 B2ROLLS-ROYCE plc · 2004