Y10S 60/909
Reaction motor or component composed of specific material
Y10S60/909 (Reaction motor or component composed of specific material) appears on 53 US grants and 3 published applications in this corpus.
Search patents in Y10S- Granted patents
- 53
- Published applications
- 3
- Assignees
- 31
- Inventors
- 114
- Latest grant
- 15 Jun 2010
Filings by year
| Year | Granted patents | Published applications |
|---|---|---|
| 1976 | 3 | 0 |
| 1977 | 2 | 0 |
| 1978 | 4 | 0 |
| 1979 | 5 | 0 |
| 1980 | 0 | 0 |
| 1981 | 2 | 0 |
| 1982 | 0 | 0 |
| 1983 | 3 | 0 |
| 1984 | 1 | 0 |
| 1985 | 1 | 0 |
| 1986 | 0 | 0 |
| 1987 | 1 | 0 |
| 1988 | 1 | 0 |
| 1989 | 2 | 0 |
| 1990 | 2 | 0 |
| 1991 | 1 | 0 |
| 1992 | 0 | 0 |
| 1993 | 0 | 0 |
| 1994 | 2 | 0 |
| 1995 | 4 | 0 |
| 1996 | 2 | 0 |
| 1997 | 0 | 0 |
| 1998 | 7 | 0 |
| 1999 | 3 | 0 |
| 2000 | 2 | 0 |
| 2001 | 2 | 1 |
| 2002 | 0 | 0 |
| 2003 | 1 | 1 |
| 2004 | 1 | 0 |
| 2005 | 0 | 0 |
| 2006 | 0 | 1 |
| 2007 | 0 | 0 |
| 2008 | 0 | 0 |
| 2009 | 0 | 0 |
| 2010 | 1 | 0 |
By publication year. Applications have been published since 2001.
Recent patents
- Pulsed detonation engines manufactured from materials having low thermal stability15 Jun 2010US 7,735,311 B2Science Applications International Corporation
- Net molded tantalum carbide rocket nozzle throat and method of making6 Jan 2004US 6,673,449 B2Lockheed Corporation
- Net molded tantalum carbide rocket nozzle throat28 Jan 2003US 6,510,694 B2Lockhead Martin Corporation
- Rocket engine thrust chamber assembly18 Dec 2001US 6,330,792 B2The United States of America as represented by the Administrator of the National Aeronautics and Space Administration
- Rocket engine thrust chamber assembly6 Mar 2001US 6,195,984 B1The United States of America as represented by the Administrator of the National Aeronautics and Space Administration
- Pulsed detonation engines manufactured from materials having low thermal stability14 Sep 2006US 2006/0201133 A1Science Applications International Corporation
- Net molded tantalum carbide rocket nozzle throat10 Jul 2003US 2003/0126855 A1Lockheed Corporation
- Rocket engine thrust chamber assembly30 Aug 2001US 2001/0017183 A1The United States of America as represented by the Administrator of the National Aeronautics and Space Administration
Most cited
By later US patents
- Wear reduction kit for gas turbine combustors62US 5,749,218 AGeneral Electric Company · 1998
- Compressor protection means41US 4,155,680 AGeneral Electric Company · 1979
- Gas turbine engine having an automatic ice shedding spinner38US 4,393,650 AROLLS-ROYCE plc · 1983
- Longitudinal load carrying method for fiber reinforced filament wound structures35US 4,118,262 ABrunswick Corporation · 1978
- Turbine engine shroud35US 4,247,249 AGeneral Electric Company · 1981