Turbine vane including a cooling-air intake portion including a helical element for swirling the cooling air
US-11988108-B2 · May 21, 2024 · US
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Botrel Erwan Daniel patents
Botrel Erwan Daniel is listed as an inventor on 18 patents in our database. Major assignees and classification codes are summarized below.
| Metric | Value |
|---|---|
| Inventor | Botrel Erwan Daniel |
| Total patents | 18 |
| First publication | Aug 27, 2015 |
| Latest publication | May 21, 2024 |
Notable patents
Publications ranked by popularity score, then publication date.
Turbine engine blade with improved cooling
US-11946387-B2 · Apr 2, 2024 · US
Turbine blade comprising ribs between cooling outlets with cooling holes
US-11753945-B2 · Sep 12, 2023 · US
Turbine blade comprising ribs between cooling outlets with cooling holes
US-2023098861-A1 · Mar 30, 2023 · US
Turbine engine blade with improved cooling
US-2022316345-A1 · Oct 6, 2022 · US
Turbine blade comprising an improved trailing-edge
US-10822961-B2 · Nov 3, 2020 · US
Turbine vane comprising a blade with a tub including a curved pressure side in a blade apex region
US-10753215-B2 · Aug 25, 2020 · US
Optimized aerodynamic profile for a turbine vane, in particular for a nozzle of the fifth stage of a turbine
US-10458246-B2 · Oct 29, 2019 · US
Turbine vane including a cooling-air intake portion including a helical element for swirling the cooling air
US-2019292918-A1 · Sep 26, 2019 · US
Optimized aerodynamic profile for a turbine blade, in particular for a rotary wheel of the seventh stage of a turbine
US-10287887-B2 · May 14, 2019 · US
Recent patents
Latest publications not already listed above.
Turbomachine vane including an antivortex fin
US-10260361-B2 · Apr 16, 2019 · US
Turbine vane comprising a blade with a tub including a curved pressure side in a blade apex region
US-2018371925-A1 · Dec 27, 2018 · US
An optimized aerodynamic profile for a turbine vane, in particular for a nozzle of the fifth stage of a turbine
US-2018230807-A1 · Aug 16, 2018 · US
Optimized aerodynamic profile for a turbine blade, in particular for a rotary wheel of the seventh stage of a turbine
US-2018016907-A1 · Jan 18, 2018 · US
Cooled vane of a high-pressure turbine
US-9657579-B2 · May 23, 2017 · US
Gas turbine blade with tip sections offset towards the pressure side and with cooling channels
US-9605545-B2 · Mar 28, 2017 · US
Turbomachine vane including an antivortex fin
US-2015361808-A1 · Dec 17, 2015 · US
Cooled vane of a high-pressure turbine
US-2015240649-A1 · Aug 27, 2015 · US
Major assignees
Companies most often associated with this inventor's publications.
| Assignee | Patents |
|---|---|
| Safran Aircraft Engines | 14 |
| Snecma | 4 |
Top CPC classifications
Most common classification codes across this inventor's patents.
| CPC | Patents |
|---|---|
| Y02T50/60 | 17 |
| F01D5/187 | 8 |
| F05D2220/323 | 7 |
| F01D5/141 | 7 |
| F01D9/041 | 6 |