F05D 2210/33
Turbulent flow
F05D2210/33 (Turbulent flow) appears on 24 US grants and 31 published applications in this corpus.
Search patents in F05D- Granted patents
- 24
- Published applications
- 31
- Assignees
- 19
- Inventors
- 61
- Latest grant
- 17 Oct 2023
Filings by year
| Year | Granted patents | Published applications |
|---|---|---|
| 2008 | 0 | 1 |
| 2009 | 0 | 0 |
| 2010 | 0 | 0 |
| 2011 | 0 | 0 |
| 2012 | 3 | 9 |
| 2013 | 0 | 3 |
| 2014 | 3 | 5 |
| 2015 | 2 | 3 |
| 2016 | 5 | 1 |
| 2017 | 1 | 0 |
| 2018 | 2 | 2 |
| 2019 | 0 | 5 |
| 2020 | 3 | 1 |
| 2021 | 2 | 0 |
| 2022 | 2 | 1 |
| 2023 | 1 | 0 |
By publication year.
Recent patents
- Featured bullnose ramp for a thrust reverser system17 Oct 2023US 11,788,488 B2Rohr, Inc.
- Turbine blade including pin-fin array26 Apr 2022US 11,313,238 B2
- Jet engine, flying object, and operation method of jet engine15 Feb 2022US 11,248,562 B2Mitsubishi Heavy Industries, Ltd.
- Spray nozzle23 Nov 2021US 11,181,272 B2ROLLS-ROYCE plc
- Propulsion system using large scale vortex generators for flow redistribution and supersonic aircraft equipped with the propulsion system20 Apr 2021US 10,981,659 B2Gulfstream Aerospace Corporation
- Featured bullnose ramp for a thrust reverser system14 Apr 2022US 2022/0112864 A1Rohr, Inc.
- Turbine blade including pin-fin array26 Mar 2020US 2020/0095870 A1Doosan Heavy Industries Construction Co., Ltd
- Tail cone apparatus and methods for reducing nozzle surface temperatures24 Oct 2019US 2019/0323453 A1The Boeing Company
- Blower with indentations23 May 2019US 2019/0154058 A1Black & Decker Inc.
- Airfoil having internal hybrid cooling cavities4 Apr 2019US 2019/0101010 A1United Technologies Corporation
Most cited
By later US patents
- Dual-vortical-flow hybrid rocket engine10US 9,458,796 B2National Applied Research Laboratories · 2016
- Cooling system having reduced mass pin fins for components in a gas turbine engine9US 8,668,453 B2Siemens Energy, Inc. · 2014
- Serpentine cooling circuit with T-shaped partitions in a turbine airfoil9US 9,017,025 B2Mikro Systems, Inc. · 2015
- Turbine airfoil vane with an impingement insert having a plurality of impingement nozzles7US 9,347,324 B2Siemens Aktiengesellschaft · 2016
- Isentropic compression inlet for supersonic aircraft6US 8,333,076 B2Gulfstream Aerospace Corporation · 2012