F05D 2240/14
Casings or housings protecting or supporting assemblies within
F05D2240/14 (Casings or housings protecting or supporting assemblies within) appears on 914 US grants and 1,047 published applications in this corpus.
Search patents in F05D- Granted patents
- 914
- Published applications
- 1,047
- Assignees
- 189
- Inventors
- 2,114
- Latest grant
- 6 Oct 2026
Filings by year
| Year | Granted patents | Published applications |
|---|---|---|
| 1984 | 1 | 0 |
| 1985 | 0 | 0 |
| 1986 | 0 | 0 |
| 1987 | 0 | 0 |
| 1988 | 0 | 0 |
| 1989 | 0 | 0 |
| 1990 | 0 | 0 |
| 1991 | 0 | 0 |
| 1992 | 0 | 0 |
| 1993 | 0 | 0 |
| 1994 | 0 | 0 |
| 1995 | 0 | 0 |
| 1996 | 0 | 0 |
| 1997 | 0 | 0 |
| 1998 | 0 | 0 |
| 1999 | 0 | 0 |
| 2000 | 1 | 0 |
| 2001 | 6 | 1 |
| 2002 | 3 | 5 |
| 2003 | 6 | 3 |
| 2004 | 3 | 4 |
| 2005 | 4 | 3 |
| 2006 | 2 | 6 |
| 2007 | 0 | 7 |
| 2008 | 5 | 16 |
| 2009 | 4 | 10 |
| 2010 | 3 | 21 |
| 2011 | 8 | 19 |
| 2012 | 6 | 22 |
| 2013 | 16 | 20 |
| 2014 | 25 | 18 |
| 2015 | 23 | 32 |
| 2016 | 18 | 48 |
| 2017 | 26 | 42 |
| 2018 | 35 | 108 |
| 2019 | 65 | 124 |
| 2020 | 120 | 138 |
| 2021 | 117 | 78 |
| 2022 | 109 | 77 |
| 2023 | 115 | 75 |
| 2024 | 85 | 61 |
| 2025 | 77 | 60 |
| 2026 | 31 | 49 |
By publication year. Applications have been published since 2001. 2026 runs to 8 Oct.
Recent patents
- Stator device for disposition within a given turbine casing of a turbomachine, connection system for a turbmachine, and turbomachine6 Oct 2026US 12,753,702 B2MTU Aero Engines AG
- Turbine exhaust duct for aircraft engine22 Sep 2026US 12,742,401 B2Pratt & Whitney Canada Corp.
- Cooling fluid guide for gas turbine and gas turbine1 Sep 2026US 12,723,522 B2Mitsubishi Heavy Industries, Ltd.
- Connection assembly for a gas turbine engine1 Sep 2026US 12,723,523 B2GE Avio S. r. l.
- Module for an aircraft turbine engine14 Jul 2026US 12,680,458 B2Safran Helicopter Engines
- Casing for an aircraft turbine engine24 Sep 2026US 2026/0286860 A1Safran Aircraft Engines
- Turbine engine for an aircraft having an integral frame24 Sep 2026US 2026/0286863 A1General Electric Company
- Expander and thermodynamic cycle using the expander17 Sep 2026US 2026/0275871 A1Nuovo Pignone Tecnologie Srl
- Rotor stage containment structure for gas turbine engine17 Sep 2026US 2026/0275882 A1Pratt & Whitney Canada Corp.
- Intermediate casing for a turbine engine17 Sep 2026US 2026/0275940 A1Safran Aircraft Engines
Most cited
By later US patents
- System for providing mobile power138US 11,105,266 B2Yantai Jereh Petroleum Equipment & Technologies Co., Ltd. · 2021
- Soundproof cabin of turbine engine97US 11,441,483 B2Yantai Jereh Petroleum Equipment & Technologies Co., Ltd. · 2022
- Method and system for a ceramic matrix composite shroud hanger assembly67US 9,874,104 B2General Electric Company · 2018
- System and method for actively changing an effective flow-through area of an inlet region of an aircraft engine55US 6,655,632 B1General Electric Company · 2003
- Deoiler for a lubrication system55US 7,377,110 B2United Technologies Corporation · 2008