Quench aperture body for a turbine engine combustor
US-11287132-B2 · Mar 29, 2022 · US
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Bouldin Lee E patents
Bouldin Lee E is listed as an inventor on 16 patents in our database. Major assignees and classification codes are summarized below.
| Metric | Value |
|---|---|
| Inventor | Bouldin Lee E |
| Total patents | 16 |
| First publication | Jul 21, 2016 |
| Latest publication | Mar 29, 2022 |
Notable patents
Publications ranked by popularity score, then publication date.
Quench aperture body for a turbine engine combustor
US-2020292172-A1 · Sep 17, 2020 · US
Controlled variation of pressure drop through effusion cooling in a double walled combustor of a gas turbine engine
US-10731858-B2 · Aug 4, 2020 · US
Turbine engine combustor heat shield with one or more cooling elements
US-10690348-B2 · Jun 23, 2020 · US
Passage geometry for gas turbine engine combustor
US-10684017-B2 · Jun 16, 2020 · US
Dilution passage arrangement for gas turbine engine combustor
US-10655856-B2 · May 19, 2020 · US
Angled combustor liner cooling holes through transverse structure within a gas turbine engine combustor
US-10648666-B2 · May 12, 2020 · US
Quench aperture body for a turbine engine combustor
US-10571125-B2 · Feb 25, 2020 · US
Turbine engine combustor heat shield with multi-angled cooling apertures
US-10215410-B2 · Feb 26, 2019 · US
Controlled variation of pressure drop through effusion cooling in a double walled combustor of a gas turbine engine
US-2016356500-A1 · Dec 8, 2016 · US
Recent patents
Latest publications not already listed above.
Dilution passage arrangement for gas turbine engine combustor
US-2016334103-A1 · Nov 17, 2016 · US
Turbine engine combustor heat shield with multi-angled cooling apertures
US-2016265773-A1 · Sep 15, 2016 · US
Turbine engine combustor heat shield with one or more cooling elements
US-2016258626-A1 · Sep 8, 2016 · US
Quench aperture body for a turbine engine combustor
US-2016238250-A1 · Aug 18, 2016 · US
Passage geometry for gas turbine engine combustor
US-2016238253-A1 · Aug 18, 2016 · US
Angled combustor liner cooling holes through transverse structure within a gas turbine engine combustor
US-2016208704-A1 · Jul 21, 2016 · US
Major assignees
Companies most often associated with this inventor's publications.
| Assignee | Patents |
|---|---|
| United Technologies Corp | 16 |
| Raytheon Tech Corp | 5 |
Top CPC classifications
Most common classification codes across this inventor's patents.
| CPC | Patents |
|---|---|
| F23R3/06 | 16 |
| F23R3/002 | 16 |
| F23R2900/03041 | 14 |
| F23R2900/03044 | 12 |
| F23R3/007 | 10 |