F05D 2260/234
Of the generator by compressor inlet air
Official title: of the generator by compressor inlet air
F05D2260/234 (Of the generator by compressor inlet air) appears on 18 US grants and 24 published applications in this corpus.
Search patents in F05D- Granted patents
- 18
- Published applications
- 24
- Assignees
- 15
- Inventors
- 65
- Latest grant
- 29 Sep 2026
Filings by year
| Year | Granted patents | Published applications |
|---|---|---|
| 2006 | 0 | 1 |
| 2007 | 0 | 0 |
| 2008 | 0 | 2 |
| 2009 | 0 | 0 |
| 2010 | 0 | 0 |
| 2011 | 1 | 1 |
| 2012 | 0 | 0 |
| 2013 | 0 | 1 |
| 2014 | 0 | 1 |
| 2015 | 0 | 1 |
| 2016 | 2 | 3 |
| 2017 | 2 | 0 |
| 2018 | 0 | 4 |
| 2019 | 3 | 1 |
| 2020 | 3 | 1 |
| 2021 | 0 | 2 |
| 2022 | 0 | 3 |
| 2023 | 5 | 0 |
| 2024 | 0 | 1 |
| 2025 | 1 | 1 |
| 2026 | 1 | 1 |
By publication year. 2026 runs to 8 Oct.
Recent patents
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- Electric power system and moving object26 Sep 2024US 2024/0318596 A1Honda Motor Co., Ltd.
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- Combined power system13 Oct 2022US 2022/0325664 A1Honda Motor Co., Ltd.
Most cited
By later US patents
- Thermal management of tail cone mounted generator25US 10,801,410 B2Raytheon Technologies Corporation · 2020
- Cooled turbine airfoil structures24US 9,267,381 B2Honeywell International Inc. · 2016
- Turbine engine with integrated generator having shared lubrication system20US 7,908,840 B2United Technologies Corporation · 2011
- Turbine blade tip clearance control9US 9,347,334 B2United Technologies Corporation · 2016
- Turbine blade tip clearance control9US 9,644,490 B2United Technologies Corporation · 2017