F05D 2240/129
Cascades, i.e. assemblies of similar profiles acting in parallel
F05D2240/129 (Cascades, i.e. assemblies of similar profiles acting in parallel) appears on 144 US grants and 175 published applications in this corpus.
Search patents in F05D- Granted patents
- 144
- Published applications
- 175
- Assignees
- 41
- Inventors
- 366
- Latest grant
- 1 Sep 2026
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| Year | Granted patents | Published applications |
|---|---|---|
| 2005 | 0 | 1 |
| 2006 | 1 | 0 |
| 2007 | 0 | 0 |
| 2008 | 0 | 3 |
| 2009 | 0 | 0 |
| 2010 | 0 | 0 |
| 2011 | 1 | 0 |
| 2012 | 1 | 2 |
| 2013 | 0 | 1 |
| 2014 | 0 | 1 |
| 2015 | 3 | 8 |
| 2016 | 1 | 18 |
| 2017 | 4 | 18 |
| 2018 | 12 | 21 |
| 2019 | 16 | 14 |
| 2020 | 26 | 21 |
| 2021 | 18 | 10 |
| 2022 | 14 | 22 |
| 2023 | 20 | 11 |
| 2024 | 12 | 15 |
| 2025 | 12 | 2 |
| 2026 | 3 | 7 |
By publication year. 2026 runs to 8 Oct.
Recent patents
- Splitter assembly for a gas turbine engine of an aircraft propulsion system1 Sep 2026US 12,723,556 B1Rtx Corporation
- Passive flow modulation device28 Apr 2026US 12,612,864 B2General Electric Company
- Aircraft nacelle equipped with at least one thrust reversal device comprising at least one longitudinal deflector, aircraft comprising at least one propulsion unit having such a nacelle27 Jan 2026US 12,535,042 B2Airbus Operations GmbH
- Thrust reverser cascade with offset vane leading edges7 Oct 2025US 12,435,682 B2Rohr, Inc.
- Aircraft nacelle equipped with at least one thrust reversal device comprising at least one longitudinal deflector configured to house a longitudinal actuator2 Sep 2025US 12,404,820 B2Airbus Operations GmbH
- Thrust reverser module of a thrust reverser ring for an aircraft nacelle thrust reverser27 Aug 2026US 2026/0251105 A1Safran Nacelles
- Thrust reverser ring for an aircraft nacelle thrust reverser and aircraft nacelle20 Aug 2026US 2026/0243216 A1Safran Nacelles
- Jet deflection module for a thrust reverser of an aircraft turbine engine30 Jul 2026US 2026/0218666 A1Safran Nacelles
- Cmc component with splash plate16 Jul 2026US 2026/0201812 A1Rtx Corporation
- Cmc component with cover plate16 Jul 2026US 2026/0201815 A1Rtx Corporation
Most cited
By later US patents
- Geared turbofan gas turbine engine architecture75US 10,794,292 B2United Technologies Corporation · 2020
- Methods and apparatus for assembling gas turbine engines17US 7,097,420 B2General Electric Company · 2006
- Integrated inducer heat exchanger for gas turbines17US 9,249,730 B2General Electric Company · 2016
- Method of fabricating a bonded cascade assembly for an aircraft thrust reverser11US 9,587,582 B1Spirit AeroSystems, Inc. · 2017
- Gas turbine engine for aircraft engine11US 9,810,082 B2GE Avio S. r. l. · 2017