F05D 2250/35
Rotated
Official title: rotated
F05D2250/35 (Rotated) appears on 20 US grants and 21 published applications in this corpus.
Search patents in F05D- Granted patents
- 20
- Published applications
- 21
- Assignees
- 13
- Inventors
- 48
- Latest grant
- 27 Feb 2024
Filings by year
| Year | Granted patents | Published applications |
|---|---|---|
| 1979 | 1 | 0 |
| 1980 | 0 | 0 |
| 1981 | 0 | 0 |
| 1982 | 0 | 0 |
| 1983 | 0 | 0 |
| 1984 | 1 | 0 |
| 1985 | 1 | 0 |
| 1986 | 0 | 0 |
| 1987 | 0 | 0 |
| 1988 | 0 | 0 |
| 1989 | 0 | 0 |
| 1990 | 0 | 0 |
| 1991 | 0 | 0 |
| 1992 | 0 | 0 |
| 1993 | 0 | 0 |
| 1994 | 0 | 0 |
| 1995 | 0 | 0 |
| 1996 | 0 | 0 |
| 1997 | 0 | 0 |
| 1998 | 0 | 0 |
| 1999 | 0 | 0 |
| 2000 | 0 | 0 |
| 2001 | 1 | 0 |
| 2002 | 1 | 2 |
| 2003 | 1 | 0 |
| 2004 | 1 | 1 |
| 2005 | 0 | 0 |
| 2006 | 0 | 0 |
| 2007 | 1 | 1 |
| 2008 | 0 | 1 |
| 2009 | 0 | 0 |
| 2010 | 0 | 0 |
| 2011 | 1 | 0 |
| 2012 | 0 | 0 |
| 2013 | 0 | 1 |
| 2014 | 0 | 1 |
| 2015 | 0 | 0 |
| 2016 | 0 | 0 |
| 2017 | 1 | 3 |
| 2018 | 2 | 0 |
| 2019 | 0 | 4 |
| 2020 | 2 | 4 |
| 2021 | 3 | 1 |
| 2022 | 1 | 0 |
| 2023 | 0 | 2 |
| 2024 | 2 | 0 |
By publication year. Applications have been published since 2001.
Recent patents
- Nacelle air outlet for aircraft turbojet engine comprising a straightening device for facilitating a reverse thrust phase27 Feb 2024US 11,913,404 B2Safran Aircraft Engines
- Hidden door thrust reverser system for an aircraft propulsion system27 Feb 2024US 11,913,406 B2Rohr, Inc.
- Turbofan comprising a set of rotatable blades for blocking off the bypass flow duct11 Jan 2022US 11,220,978 B2Airbus Operations GmbH
- Aircraft with a jet engine21 Sep 2021US 11,124,305 B2Rolls-Royce Deutschland Ltd & Co KG
- Wind funnel and gas combustion turbine systems with controlled air feed24 Aug 2021US 11,098,645 B2
- Gas turbine engine stationary vane with contoured platform6 Apr 2023US 2023/0107877 A1Siemens Energy Global GmbH & Co. KG
- Nacelle air outlet for aircraft turbojet engine comprising a straightening device for facilitating a reverse thrust phase9 Feb 2023US 2023/0038787 A1Safran Aircraft Engines
- Hidden door thrust reverser system for an aircraft propulsion system7 Oct 2021US 2021/0310441 A1Rohr, Inc.
- Wind funnel, gas combustion turbine and power output generator systems10 Dec 2020US 2020/0386157 A1
- Wind funnel and gas combustion turbine systems including compression sections13 Aug 2020US 2020/0256248 A1
Most cited
By later US patents
- System for attaching two rotating parts made of materials having different expansion coefficients58US 4,452,038 ASnecma · 1984
- System for the precision machining of rotationally symmetrical components14US 6,764,384 B1MTU Aero Engines AG · 2004
- Exhaust turbine for a turbocharger8US 6,374,611 B2DaimlerChrysler AG · 2002
- Exhaust turbocharger for an internal combustion engine8US 6,554,568 B2DaimlerChrysler AG · 2003
- Method and apparatus for manufacturing rotationally symmetrical constructional parts such as nozzles and combination chambers of rocket engines7US 4,148,121 AMesserschmitt-Bolkow-Blohm GmbH · 1979