F05D 2240/40
Use of a multiplicity of similar components
F05D2240/40 (Use of a multiplicity of similar components) appears on 353 US grants and 420 published applications in this corpus.
Search patents in F05D- Granted patents
- 353
- Published applications
- 420
- Assignees
- 156
- Inventors
- 844
- Latest grant
- 6 Oct 2026
Filings by year
| Year | Granted patents | Published applications |
|---|---|---|
| 1994 | 1 | 0 |
| 1995 | 1 | 0 |
| 1996 | 4 | 0 |
| 1997 | 2 | 0 |
| 1998 | 2 | 0 |
| 1999 | 1 | 0 |
| 2000 | 1 | 0 |
| 2001 | 6 | 1 |
| 2002 | 8 | 4 |
| 2003 | 4 | 3 |
| 2004 | 6 | 5 |
| 2005 | 3 | 6 |
| 2006 | 6 | 11 |
| 2007 | 4 | 16 |
| 2008 | 7 | 10 |
| 2009 | 4 | 12 |
| 2010 | 9 | 23 |
| 2011 | 7 | 15 |
| 2012 | 27 | 24 |
| 2013 | 17 | 20 |
| 2014 | 14 | 17 |
| 2015 | 15 | 26 |
| 2016 | 13 | 25 |
| 2017 | 16 | 32 |
| 2018 | 28 | 34 |
| 2019 | 29 | 18 |
| 2020 | 26 | 28 |
| 2021 | 23 | 20 |
| 2022 | 12 | 12 |
| 2023 | 16 | 13 |
| 2024 | 15 | 15 |
| 2025 | 17 | 16 |
| 2026 | 9 | 14 |
By publication year. Applications have been published since 2001. 2026 runs to 8 Oct.
Recent patents
- Methods of modifying existing gas turbine engine design to create a combined storage engine and simple cycle peaker product6 Oct 2026US 12,753,719 B2Powerphase International, LLC
- Multistage pumping system for adaptive offloading of a liquid from a container23 Jun 2026US 12,663,009 B2Flowserve Pte. Ltd.
- Injector with injector elements in circumferential rows that alternate between counter-clockwise and clockwise swirl16 Jun 2026US 12,655,814 B2Aerojet Rocketdyne, Inc.
- Hybrid-electric propulsion system equipped with a coupler for switching between modes of operation5 May 2026US 12,618,385 B2General Electric Company
- Symmetrical two-piece hollow-vane assembly joined via brazing along airfoil centerline21 Apr 2026US 12,607,126 B2Rtx Corporation
- Hybrid-electric propulsion system equipped with a coupler for switching between modes of operation17 Sep 2026US 2026/0275941 A1General Electric Company
- Thrust reverser module of a thrust reverser ring for an aircraft nacelle thrust reverser27 Aug 2026US 2026/0251105 A1Safran Nacelles
- Engine system for an aircraft comprising means for heating dihydrogen before supplying an engine with dihydrogen20 Aug 2026US 2026/0243200 A1Airbus Operations GmbH
- Thrust reverser ring for an aircraft nacelle thrust reverser and aircraft nacelle20 Aug 2026US 2026/0243216 A1Safran Nacelles
- Aircraft air system with boost compressor(s)13 Aug 2026US 2026/0233843 A1Rtx Corporation
Most cited
By later US patents
- Multiple gas turbine forwarding system130US 8,951,019 B2General Electric Company · 2015
- Power conversion systems108US 7,325,401 B1Brayton Energy, LLC · 2008
- Systems and methods utilizing turbine compressor discharge for hydrostatic manifold purge102US 10,968,837 B1BJ Energy Solutions, LLC · 2021
- Power plant and method of use74US 8,266,913 B2General Electric Company · 2012
- Gas turbine engine optimization by electric power transfer74US 9,045,996 B2Honeywell International Inc. · 2015