Y10T 137/0645
With condition responsive control means
Y10T137/0645 (With condition responsive control means) appears on 63 US grants and 36 published applications in this corpus.
Search patents in Y10T- Granted patents
- 63
- Published applications
- 36
- Assignees
- 35
- Inventors
- 118
- Latest grant
- 25 Apr 2017
Filings by year
| Year | Granted patents | Published applications |
|---|---|---|
| 1976 | 2 | 0 |
| 1977 | 2 | 0 |
| 1978 | 1 | 0 |
| 1979 | 0 | 0 |
| 1980 | 0 | 0 |
| 1981 | 2 | 0 |
| 1982 | 0 | 0 |
| 1983 | 1 | 0 |
| 1984 | 1 | 0 |
| 1985 | 1 | 0 |
| 1986 | 0 | 0 |
| 1987 | 0 | 0 |
| 1988 | 0 | 0 |
| 1989 | 2 | 0 |
| 1990 | 0 | 0 |
| 1991 | 0 | 0 |
| 1992 | 1 | 0 |
| 1993 | 0 | 0 |
| 1994 | 0 | 0 |
| 1995 | 2 | 0 |
| 1996 | 2 | 0 |
| 1997 | 2 | 0 |
| 1998 | 2 | 0 |
| 1999 | 3 | 0 |
| 2000 | 1 | 0 |
| 2001 | 4 | 0 |
| 2002 | 0 | 1 |
| 2003 | 0 | 1 |
| 2004 | 0 | 1 |
| 2005 | 2 | 0 |
| 2006 | 0 | 2 |
| 2007 | 1 | 3 |
| 2008 | 1 | 2 |
| 2009 | 2 | 3 |
| 2010 | 2 | 6 |
| 2011 | 2 | 9 |
| 2012 | 2 | 2 |
| 2013 | 10 | 3 |
| 2014 | 4 | 2 |
| 2015 | 5 | 0 |
| 2016 | 2 | 1 |
| 2017 | 1 | 0 |
By publication year. Applications have been published since 2001.
Recent patents
- Air intake guide25 Apr 2017US 9,631,555 B2ROLLS-ROYCE plc
- Rotating inlet cowl for a turbine engine, comprising an eccentric forward end26 Jan 2016US 9,243,562 B1Snecma
- Variable contour nacelle assembly for a gas turbine engine5 Jan 2016US 9,228,534 B2United Technologies Corporation
- Composite fan case with integral containment zone19 May 2015US 9,032,706 B2Pratt & Whitney Canada Corp.
- Gas turbine engine fan blade airfoil profile7 Apr 2015US 8,997,494 B2United Technologies Corporation
- Rotating inlet cowl for a turbine engine, comprising an eccentric forward end7 Jan 2016US 2016/0003146 A1Snecma
- Gas turbine engine fan blade airfoil profile23 Oct 2014US 2014/0311149 A1United Technologies Corporation
- Air intake and a method of controlling the same23 Oct 2014US 2014/0311580 A1ROLLS-ROYCE plc
- Intake liner for a gas turbine engine10 Oct 2013US 2013/0263601 A1ROLLS-ROYCE plc
- Variable shape inlet section for a nacelle assembly of a gas turbine engine4 Jul 2013US 2013/0170950 A1United Technologies Corporation
Most cited
By later US patents
- Low drag ducted Ram air turbine generator and cooling system76US 6,270,309 B1Ghetzler Aero-Power Corporation · 2001
- Mission adaptive inlet60US 6,089,505 AMcDonnell Douglas Corporation · 2000
- Low observable engine air inlet system48US 5,697,394 AUnited Technologies Corporation · 1997
- Mission adaptive inlet41US 6,260,567 B1The Boeing Company · 2001
- Variable geometry ramjet engine33US 3,974,648 AUnited Technologies Corporation · 1976