Cupped contour for gas turbine engine blade assembly
US-11591914-B2 · Feb 28, 2023 · US
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Snyder Brooks E patents
Snyder Brooks E is listed as an inventor on 43 patents in our database. Major assignees and classification codes are summarized below.
| Metric | Value |
|---|---|
| Inventor | Snyder Brooks E |
| Total patents | 43 |
| First publication | Oct 29, 2015 |
| Latest publication | Feb 28, 2023 |
Notable patents
Publications ranked by popularity score, then publication date.
Additive manufactured combustor heat shield
US-10935240-B2 · Mar 2, 2021 · US
Gas turbine engine component with conformal fillet cooling path
US-10612392-B2 · Apr 7, 2020 · US
Bore-cooled film dispensing pedestals
US-10563583-B2 · Feb 18, 2020 · US
Cooled airfoil structure
US-10494929-B2 · Dec 3, 2019 · US
Airfoil, and method for manufacturing the same
US-10487667-B2 · Nov 26, 2019 · US
Gas turbine engine component cooling cavity with vortex promoting features
US-10465530-B2 · Nov 5, 2019 · US
Cupped contour for gas turbine engine blade assembly
US-2019316474-A1 · Oct 17, 2019 · US
Gas turbine engine turbine blade tip cooling
US-10436039-B2 · Oct 8, 2019 · US
Gas turbine engine component cooling circuit with respirating pedestal
US-10370981-B2 · Aug 6, 2019 · US
Recent patents
Latest publications not already listed above.
Gas turbine engine component cooling passage turbulator
US-10364683-B2 · Jul 30, 2019 · US
Cupped contour for gas turbine engine blade assembly
US-10344597-B2 · Jul 9, 2019 · US
Gas turbine engine airfoil with leading edge trench and impingement cooling
US-10240464-B2 · Mar 26, 2019 · US
Anti-deflection feature for additively manufactured thin metal parts and method of additively manufacturing thin metal parts
US-2019085719-A1 · Mar 21, 2019 · US
Method and system for controlling coating in non-line-of-sight locations
US-10179948-B2 · Jan 15, 2019 · US
Cooling system of a stator assembly for a gas turbine engine having a variable cooling flow mechanism and method of operation
US-10094229-B2 · Oct 9, 2018 · US
Anti-deflection feature for additively manufactured thin metal parts and method of additively manufacturing thin metal parts
US-10094240-B2 · Oct 9, 2018 · US
Variable vane segment
US-10066549-B2 · Sep 4, 2018 · US
Airfoil cooling apparatus
US-10012090-B2 · Jul 3, 2018 · US
Seal for gas turbine engine
US-9988923-B2 · Jun 5, 2018 · US
Airfoil cooling device and method of manufacture
US-9932835-B2 · Apr 3, 2018 · US
Fixture for application of coatings and method of using same
US-9845524-B2 · Dec 19, 2017 · US
Cupped contour for gas turbine engine blade assembly
US-2017051613-A1 · Feb 23, 2017 · US
Blade outer air seal component with varying thermal expansion coefficient
US-2017051625-A1 · Feb 23, 2017 · US
Airfoil, and method for manufacturing the same
US-2016369634-A1 · Dec 22, 2016 · US
Gas turbine engine component cooling circuit with respirating pedestal
US-2016333702-A1 · Nov 17, 2016 · US
Gas turbine engine component cooling cavity with vortex promoting features
US-2016312624-A1 · Oct 27, 2016 · US
Additive manufactured combustor heat shield with cooled attachment stud
US-2016313005-A1 · Oct 27, 2016 · US
Additive manufactured combustor heat shield
US-2016313004-A1 · Oct 27, 2016 · US
Gas turbine engine airfoil with leading edge trench and impingement cooling
US-2016273365-A1 · Sep 22, 2016 · US
Major assignees
Companies most often associated with this inventor's publications.
| Assignee | Patents |
|---|---|
| United Technologies Corp | 43 |
| Raytheon Tech Corp | 2 |
Top CPC classifications
Most common classification codes across this inventor's patents.
| CPC | Patents |
|---|---|
| Y02T50/60 | 29 |
| F05D2220/32 | 28 |
| F01D5/187 | 26 |
| F01D25/12 | 18 |
| F05D2260/201 | 16 |