F01D 5/147
Construction, i.e. structural features
Official title: {Construction, i.e. structural features, e.g. of weight-saving hollow blades (F01D5/148, F01D5/16 and F01D5/20 take precedence; blade shape F01D5/141; blades with cooling or heating channels or cavities F01D5/18; heating, heat-insulating or cooling means on blades F01D5/18)}
F01D5/147 (Construction, i.e. structural features) appears on 2,144 US grants and 2,403 published applications in this corpus.
Search patents in F01D- Granted patents
- 2,144
- Published applications
- 2,403
- Assignees
- 306
- Inventors
- 3,465
- Latest grant
- 6 Oct 2026
Filings by year
| Year | Granted patents | Published applications |
|---|---|---|
| 1976 | 3 | 0 |
| 1977 | 0 | 0 |
| 1978 | 2 | 0 |
| 1979 | 1 | 0 |
| 1980 | 1 | 0 |
| 1981 | 2 | 0 |
| 1982 | 2 | 0 |
| 1983 | 1 | 0 |
| 1984 | 1 | 0 |
| 1985 | 2 | 0 |
| 1986 | 3 | 0 |
| 1987 | 3 | 0 |
| 1988 | 3 | 0 |
| 1989 | 2 | 0 |
| 1990 | 2 | 0 |
| 1991 | 2 | 0 |
| 1992 | 5 | 0 |
| 1993 | 6 | 0 |
| 1994 | 8 | 0 |
| 1995 | 12 | 0 |
| 1996 | 6 | 0 |
| 1997 | 11 | 0 |
| 1998 | 14 | 0 |
| 1999 | 10 | 0 |
| 2000 | 13 | 0 |
| 2001 | 19 | 5 |
| 2002 | 22 | 14 |
| 2003 | 18 | 11 |
| 2004 | 14 | 24 |
| 2005 | 19 | 37 |
| 2006 | 24 | 35 |
| 2007 | 21 | 43 |
| 2008 | 30 | 47 |
| 2009 | 23 | 59 |
| 2010 | 37 | 63 |
| 2011 | 44 | 60 |
| 2012 | 59 | 57 |
| 2013 | 48 | 126 |
| 2014 | 63 | 105 |
| 2015 | 64 | 151 |
| 2016 | 86 | 244 |
| 2017 | 86 | 179 |
| 2018 | 157 | 178 |
| 2019 | 223 | 182 |
| 2020 | 219 | 193 |
| 2021 | 182 | 109 |
| 2022 | 155 | 97 |
| 2023 | 128 | 101 |
| 2024 | 123 | 118 |
| 2025 | 105 | 91 |
| 2026 | 60 | 74 |
By publication year. Applications have been published since 2001. 2026 runs to 8 Oct.
Recent patents
- Turbine engine with a blade assembly having a set of cooling conduits6 Oct 2026US 12,753,696 B2General Electric Company
- Metal coupon with porous stress-relief section and component with same15 Sep 2026US 12,735,986 B2GE Infrastructure Technology LLC
- Polymeric foams for hollow cavities8 Sep 2026US 12,729,627 B2Rtx Corporation
- Engine component1 Sep 2026US 12,723,513 B2General Electric Company
- Localized riblets for a flowpath surface25 Aug 2026US 12,716,358 B1General Electric Company
- Method for attaching a metal reinforcement on a leading edge of a turbomachine blade8 Oct 2026US 2026/0307338 A1Safran Aerospace Composites
- A method of forming an airfoil assembly having a composite spar10 Sep 2026US 2026/0264840 A1General Electric Company
- Airfoil assembly having a composite spar for an engine10 Sep 2026US 2026/0266182 A1General Electric Company
- Cavity consolidation apparatus27 Aug 2026US 2026/0250210 A1General Electric Company
- Localized riblets for a flowpath surface27 Aug 2026US 2026/0251065 A1General Electric Company
Most cited
By later US patents
- Coolable airfoil for a gas turbine engine160US 6,099,251 AUnited Technologies Corporation · 2000
- Double-wall airfoil127US 5,626,462 AGeneral Electric Company · 1997
- Swept fan blade127US 6,071,077 AROLLS-ROYCE plc · 2000
- Method of manufacturing an air cooled vane with film cooling pocket construction92US 5,392,515 AUnited Technologies Corporation · 1995
- Multi-piece turbine vane assembly92US 7,452,182 B2Siemens Energy, Inc. · 2008