F02K 1/165
With air intake control
Official title: {with air intake control}
F02K1/165 (With air intake control) appears on 12 US grants and 10 published applications in this corpus.
Search patents in F02K- Granted patents
- 12
- Published applications
- 10
- Assignees
- 11
- Inventors
- 33
- Latest grant
- 27 Jun 2023
Filings by year
| Year | Granted patents | Published applications |
|---|---|---|
| 2000 | 1 | 0 |
| 2001 | 0 | 0 |
| 2002 | 0 | 0 |
| 2003 | 0 | 0 |
| 2004 | 0 | 0 |
| 2005 | 0 | 0 |
| 2006 | 0 | 0 |
| 2007 | 0 | 0 |
| 2008 | 0 | 1 |
| 2009 | 0 | 0 |
| 2010 | 2 | 2 |
| 2011 | 0 | 0 |
| 2012 | 1 | 0 |
| 2013 | 2 | 1 |
| 2014 | 2 | 1 |
| 2015 | 0 | 0 |
| 2016 | 0 | 0 |
| 2017 | 0 | 1 |
| 2018 | 0 | 0 |
| 2019 | 0 | 0 |
| 2020 | 0 | 1 |
| 2021 | 1 | 0 |
| 2022 | 1 | 0 |
| 2023 | 2 | 1 |
| 2024 | 0 | 0 |
| 2025 | 0 | 0 |
| 2026 | 0 | 2 |
By publication year. Applications have been published since 2001. 2026 runs to 8 Oct.
Recent patents
- Propulsion system for an aircraft27 Jun 2023US 11,686,246 B2Gulfstream Aerospace Corporation
- Supersonic air intake passage capable of achieving synchronous adjustment of capturing area and throat area3 Jan 2023US 11,542,867 B2Nanjing University of Aeronautics and Astronautics
- Fiber optic exit area sensing for gas turbine engine nozzles23 Aug 2022US 11,421,607 B1Raytheon Technologies Corporation
- Jet engine13 Apr 2021US 10,975,775 B2IHI Corporation
- Gas turbine engine having slim-line nacelle30 Sep 2014US 8,844,294 B2United Technologies Corporation
- Gas turbine engine with variable airflow inlet23 Jul 2026US 2026/0210288 A1Rtx Corporation
- Turboprop engine with closable core8 Jan 2026US 2026/0009356 A1Pratt & Whitney Canada Corp.
- Propulsion system for an aircraft20 Apr 2023US 2023/0120249 A1Gulfstream Aerospace Corporation
- Supersonic air intake passage capable of achieving synchronous adjustment of capturing area and throat area1 Oct 2020US 2020/0309030 A1Nanjing University of Aeronautics and Astronautics
- Jet engine28 Dec 2017US 2017/0370295 A1IHI Corporation
Most cited
By later US patents
- Method and apparatus for an aerodynamic stability management system29US 7,827,803 B1General Electric Company · 2010
- Gas turbine engine having slim-line nacelle23US 7,797,944 B2United Technologies Corporation · 2010
- Rocket and ramjet powered hypersonic stealth missile having alterable radar cross section11US 6,058,846 ALockhead Martin Corporation · 2000
- Gas turbine engine having slim-line nacelle9US 8,726,632 B2United Technologies Corporation · 2014
- Gas turbine engine having slim-line nacelle4US 8,353,164 B2United Technologies Corporation · 2013