F05D 2270/332
Maximum loads or fatigue criteria
F05D2270/332 (Maximum loads or fatigue criteria) appears on 38 US grants and 49 published applications in this corpus.
Search patents in F05D- Granted patents
- 38
- Published applications
- 49
- Assignees
- 25
- Inventors
- 112
- Latest grant
- 16 Dec 2025
Filings by year
| Year | Granted patents | Published applications |
|---|---|---|
| 2010 | 0 | 1 |
| 2011 | 0 | 0 |
| 2012 | 0 | 0 |
| 2013 | 0 | 3 |
| 2014 | 2 | 8 |
| 2015 | 1 | 2 |
| 2016 | 4 | 4 |
| 2017 | 4 | 1 |
| 2018 | 4 | 5 |
| 2019 | 2 | 2 |
| 2020 | 2 | 3 |
| 2021 | 2 | 4 |
| 2022 | 7 | 3 |
| 2023 | 4 | 5 |
| 2024 | 2 | 1 |
| 2025 | 4 | 6 |
| 2026 | 0 | 1 |
By publication year. 2026 runs to 8 Oct.
Recent patents
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- Method for operating a flow producing system als well as a flow producing system12 Jun 2025US 2025/0188942 A1ebm-papst Mulfingen GmbH & Co. KG
- Methods and apparatuses for performing classification of a classification subject1 May 2025US 2025/0139522 A1ROLLS-ROYCE plc
- Transfer of power between the high-pressure shaft and the low-pressure shaft of a turbomachine20 Mar 2025US 2025/0092833 A1Safran Helicopter Engines
- Localized thickening ply reinforcement within ceramic matrix composite airfoil cavity27 Feb 2025US 2025/0067184 A1Rtx Corporation
Most cited
By later US patents
- Electrical power generator for a gas turbine engine19US 9,729,096 B2ROLLS-ROYCE plc · 2017
- Creep life management system for a turbine engine and method of operating the same16US 9,494,490 B2General Electric Company · 2016
- Gas turbine control method and device7US 8,701,420 B2Mitsubishi Heavy Industries, Ltd. · 2014
- Method and a device for performing a health check of a turbine engine of an aircraft having at least one such engine6US 8,666,568 B2Eurocopter · 2014
- Gas turbine engine vane embedded beam interrupt optical tip-timing probe system6US 9,297,720 B2United Technologies Corporation · 2016