Y10T 29/49343
Passage contains tubular insert
Y10T29/49343 (Passage contains tubular insert) appears on 49 US grants and 27 published applications in this corpus.
Search patents in Y10T- Granted patents
- 49
- Published applications
- 27
- Assignees
- 24
- Inventors
- 91
- Latest grant
- 14 Jan 2025
Filings by year
| Year | Granted patents | Published applications |
|---|---|---|
| 1979 | 1 | 0 |
| 1980 | 2 | 0 |
| 1981 | 2 | 0 |
| 1982 | 0 | 0 |
| 1983 | 2 | 0 |
| 1984 | 2 | 0 |
| 1985 | 0 | 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 | 0 | 0 |
| 1995 | 1 | 0 |
| 1996 | 1 | 0 |
| 1997 | 0 | 0 |
| 1998 | 1 | 0 |
| 1999 | 0 | 0 |
| 2000 | 1 | 0 |
| 2001 | 3 | 0 |
| 2002 | 2 | 1 |
| 2003 | 2 | 2 |
| 2004 | 2 | 1 |
| 2005 | 0 | 1 |
| 2006 | 3 | 1 |
| 2007 | 0 | 2 |
| 2008 | 1 | 1 |
| 2009 | 1 | 1 |
| 2010 | 2 | 3 |
| 2011 | 1 | 3 |
| 2012 | 2 | 2 |
| 2013 | 5 | 0 |
| 2014 | 1 | 0 |
| 2015 | 1 | 6 |
| 2016 | 0 | 0 |
| 2017 | 2 | 0 |
| 2018 | 3 | 1 |
| 2019 | 0 | 0 |
| 2020 | 2 | 0 |
| 2021 | 0 | 0 |
| 2022 | 0 | 0 |
| 2023 | 1 | 1 |
| 2024 | 0 | 1 |
| 2025 | 1 | 0 |
By publication year. Applications have been published since 2001.
Recent patents
- Cooling jacket of a hollow blade of a distributor14 Jan 2025US 12,196,105 B2Safran Aircraft Engines
- Nozzle blade for a turbine engine, nozzle, turbine engine and method for manufacturing same28 Nov 2023US 11,828,194 B2Safran Aircraft Engines
- Gas turbine engine component having vascular engineered lattice structure26 May 2020US 10,662,781 B2Raytheon Technologies Corporation
- Gas turbine engine component having vascular engineered lattice structure25 Feb 2020US 10,570,746 B2United Technologies Corporation
- Gas turbine engine component having vascular engineered lattice structure18 Dec 2018US 10,156,359 B2United Technologies Corporation
- Cooling jacket of a hollow blade of a distributor15 Aug 2024US 2024/0271535 A1Safran Aircraft Engines
- Nozzle blade for a turbine engine, nozzle, turbine engine and method for manufacturing same23 Mar 2023US 2023/0086163 A1Safran Aircraft Engines
- Gas turbine engine component having vascular engineered lattice structure22 Nov 2018US 2018/0334909 A1United Technologies Corporation
- Bell mouth inlet for turbine blade24 Dec 2015US 2015/0369055 A1United Technologies Corporation
- Tapered thermal barrier coating on convex and concave trailing edge surfaces24 Dec 2015US 2015/0369060 A1United Technologies Corporation
Most cited
By later US patents
- Composite structure formed by CMC-on-insulation process63US 7,093,359 B2Siemens Westinghouse Power Corporation · 2006
- Trapped insert turbine airfoil54US 6,193,465 B1General Electric Company · 2001
- Process of plugging cooling holes of a gas turbine component50US 6,265,022 B1ABB Alstom Power (Schweiz) AG · 2001
- Method of fabricating composite structures for water cooled gas turbine components43US 4,137,619 AGeneral Electric Company · 1979
- Airfoil support36US 7,410,342 B2Florida Turbine Technologies, Inc. · 2008