F05D 2230/61
Using limited numbers of standard modules which can be adapted by machining
Official title: using limited numbers of standard modules which can be adapted by machining
F05D2230/61 (Using limited numbers of standard modules which can be adapted by machining) appears on 79 US grants and 90 published applications in this corpus.
Search patents in F05D- Granted patents
- 79
- Published applications
- 90
- Assignees
- 62
- Inventors
- 258
- Latest grant
- 17 Feb 2026
Filings by year
| Year | Granted patents | Published applications |
|---|---|---|
| 1985 | 1 | 0 |
| 1986 | 0 | 0 |
| 1987 | 0 | 0 |
| 1988 | 0 | 0 |
| 1989 | 0 | 0 |
| 1990 | 0 | 0 |
| 1991 | 0 | 0 |
| 1992 | 1 | 0 |
| 1993 | 0 | 0 |
| 1994 | 1 | 0 |
| 1995 | 1 | 0 |
| 1996 | 1 | 0 |
| 1997 | 2 | 0 |
| 1998 | 0 | 0 |
| 1999 | 0 | 0 |
| 2000 | 0 | 0 |
| 2001 | 3 | 2 |
| 2002 | 2 | 0 |
| 2003 | 0 | 0 |
| 2004 | 1 | 3 |
| 2005 | 1 | 4 |
| 2006 | 2 | 3 |
| 2007 | 3 | 4 |
| 2008 | 2 | 0 |
| 2009 | 2 | 5 |
| 2010 | 0 | 5 |
| 2011 | 3 | 3 |
| 2012 | 4 | 3 |
| 2013 | 4 | 3 |
| 2014 | 2 | 4 |
| 2015 | 1 | 8 |
| 2016 | 3 | 7 |
| 2017 | 7 | 2 |
| 2018 | 7 | 6 |
| 2019 | 1 | 6 |
| 2020 | 8 | 5 |
| 2021 | 2 | 3 |
| 2022 | 2 | 4 |
| 2023 | 1 | 3 |
| 2024 | 9 | 5 |
| 2025 | 1 | 2 |
| 2026 | 1 | 0 |
By publication year. Applications have been published since 2001. 2026 runs to 8 Oct.
Recent patents
- Intercooled combustor nozzle guide vane and secondary air configuration17 Feb 2026US 12,553,609 B2Rtx Corporation
- Extended banana foot stator9 Dec 2025US 12,492,643 B1Pratt & Whitney Canada Corp.
- Electric module for an aircraft turbomachine31 Dec 2024US 12,180,847 B2Safran Aircraft Engines
- Nozzle segment for use with multiple different turbine engines31 Dec 2024US 12,180,859 B2GE Infrastructure Technology LLC
- Multi-zone blade fabrication24 Dec 2024US 12,173,615 B2Rtx Corporation
- Multi-Zone Blade Fabrication24 Apr 2025US 2025/0129721 A1Rtx Corporation
- Method for manufacturing a casing for an aircraft turbine engine17 Apr 2025US 2025/0122813 A1Safran Aircraft Engines
- Intercooled combustor nozzle guide vane and secondary air configuration24 Oct 2024US 2024/0353104 A1Rtx Corporation
- Gas turbine engine configured for decreased diffuser windage and method of assembling the same24 Oct 2024US 2024/0353105 A1Rtx Corporation
- Nozzle segment for use with multiple different turbine engines1 Aug 2024US 2024/0254887 A1General Electric Company
Most cited
By later US patents
- Closed or open circuit cooling of turbine rotor components86US 5,593,274 AGeneral Electric Company · 1997
- Twin spool turbine engine with power take-off means on the low-pressure and high-pressure rotors, and power take-off module for the turbine engine71US 7,552,591 B2Snecma · 2009
- Exhaust-gas-turbine casing25US 7,008,182 B2ABB Turbo Systems AG · 2006
- Turbine unit and VTG mechanism therefor21US 7,322,791 B2BorgWarner Inc. · 2008
- Gas turbines having different frequency applications with hardware commonality20US 5,520,512 AGeneral Electric Company · 1996