F05D 2260/532
Of the bevelled or angled type
Official title: of the bevelled or angled type
F05D2260/532 (Of the bevelled or angled type) appears on 36 US grants and 45 published applications in this corpus.
Search patents in F05D- Granted patents
- 36
- Published applications
- 45
- Assignees
- 22
- Inventors
- 79
- Latest grant
- 16 Sep 2025
Filings by year
| Year | Granted patents | Published applications |
|---|---|---|
| 2012 | 0 | 1 |
| 2013 | 0 | 2 |
| 2014 | 1 | 2 |
| 2015 | 1 | 3 |
| 2016 | 0 | 5 |
| 2017 | 5 | 3 |
| 2018 | 3 | 7 |
| 2019 | 5 | 7 |
| 2020 | 6 | 7 |
| 2021 | 4 | 4 |
| 2022 | 3 | 1 |
| 2023 | 4 | 0 |
| 2024 | 2 | 2 |
| 2025 | 2 | 0 |
| 2026 | 0 | 1 |
By publication year. 2026 runs to 8 Oct.
Recent patents
- Propeller for a turbine engine of an aircraft with a variable-pitch vane and a geared counterweight device16 Sep 2025US 12,415,597 B2Safran Aircraft Engines
- System for controlling discharge doors of a turbomachine25 Feb 2025US 12,234,737 B2Safran
- Mechanically-distributed propulsion drivetrain and architecture8 Oct 2024US 12,110,846 B2Aurora Flight Sciences Corporation, a subsidiary of The Boeing Company
- Turbojet engine nacelle with a cascade thrust reverser comprising a flap control sector6 Feb 2024US 11,891,965 B2Safran Nacelles
- Aircraft turbomachine arrangement comprising a lubrication pump driven by two oblique gears26 Dec 2023US 11,852,079 B2Safran Aircraft Engines
- Gas Turbine Engine Tower Shaft Assembly2 Apr 2026US 2026/0092565 A1Pratt & Whitney Canada Corp.
- Propeller for a turbine engine of an aircraft with a variable-pitch vane and a geared counterweight device26 Sep 2024US 2024/0317385 A1Safran Aircraft Engines
- System for controlling discharge doors of a turbomachine14 Mar 2024US 2024/0084713 A1Safran
- Aircraft turbomachine arrangement comprising a lubrication pump driven by two oblique gears17 Nov 2022US 2022/0364517 A1Safran Aircraft Engines
- Mechanically-Distributed Propulsion Drivetrain and Architecture16 Sep 2021US 2021/0284352 A1Aurora Flight Sciences Corporation, a subsidiary of The Boeing Company
Most cited
By later US patents
- Bowed rotor prevention system58US 9,664,070 B1United Technologies Corporation · 2017
- Dual input drive AGB for gas turbine engines50US 8,814,502 B2Pratt & Whitney Canada Corp. · 2014
- Intermediate casing for turbomachine and accessory gearbox drive assembly12US 9,689,314 B2Snecma · 2017
- System and method for removing rotor bow in a gas turbine engine using mechanical energy storage device8US 10,760,498 B2General Electric Company · 2020
- Bowed rotor prevention system8US 10,801,371 B2Raytheon Technologies Corporation · 2020