
Eugene Lee
Examiner (ID: 15333)
| Most Active Art Unit | 2815 |
| Art Unit(s) | 2815 |
| Total Applications | 1427 |
| Issued Applications | 1095 |
| Pending Applications | 109 |
| Abandoned Applications | 246 |
Applications
| Application number | Title of the application | Filing Date | Status |
|---|---|---|---|
Array
(
[id] => 18764625
[patent_doc_number] => 11815014
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2023-11-14
[patent_title] => Combined cooling heating and power micro gas turbine device
[patent_app_type] => utility
[patent_app_number] => 17/625346
[patent_app_country] => US
[patent_app_date] => 2020-12-11
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[rel_patent_id] =>[rel_patent_doc_number] =>) 17/625346 | Combined cooling heating and power micro gas turbine device | Dec 10, 2020 | Issued |
Array
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[patent_doc_number] => 20220178302
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[patent_kind] => A1
[patent_issue_date] => 2022-06-09
[patent_title] => GAS TURBINE APPARATUS WITH COUNTER-ROTATING BLADES
[patent_app_type] => utility
[patent_app_number] => 17/113995
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Array
(
[id] => 17998350
[patent_doc_number] => 11499449
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[patent_issue_date] => 2022-11-15
[patent_title] => Gas turbine module, gas turbine plant including the same, method of unloading gas turbine module, and method of exchanging gas turbine module
[patent_app_type] => utility
[patent_app_number] => 17/105862
[patent_app_country] => US
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Array
(
[id] => 18413718
[patent_doc_number] => 11668253
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2023-06-06
[patent_title] => System and method for providing in-flight reverse thrust for an aircraft
[patent_app_type] => utility
[patent_app_number] => 17/072477
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Array
(
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[patent_issue_date] => 2021-05-06
[patent_title] => EXHAUST NOZZLE
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Array
(
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[patent_title] => EXHAUST NOZZLE
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Array
(
[id] => 17324120
[patent_doc_number] => 11215123
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[patent_issue_date] => 2022-01-04
[patent_title] => Turbine section of high bypass turbofan
[patent_app_type] => utility
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[patent_app_country] => US
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[rel_patent_id] =>[rel_patent_doc_number] =>) 17/062756 | Turbine section of high bypass turbofan | Oct 4, 2020 | Issued |
Array
(
[id] => 17801028
[patent_doc_number] => 11415321
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[patent_kind] => B2
[patent_issue_date] => 2022-08-16
[patent_title] => Combustor liner for a gas turbine engine and an associated method thereof
[patent_app_type] => utility
[patent_app_number] => 17/029587
[patent_app_country] => US
[patent_app_date] => 2020-09-23
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[rel_patent_id] =>[rel_patent_doc_number] =>) 17/029587 | Combustor liner for a gas turbine engine and an associated method thereof | Sep 22, 2020 | Issued |
Array
(
[id] => 17474525
[patent_doc_number] => 20220082029
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2022-03-17
[patent_title] => ROTATING HEAT EXCHANGER
[patent_app_type] => utility
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[patent_app_country] => US
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[rel_patent_id] =>[rel_patent_doc_number] =>) 17/021547 | Rotating heat exchanger | Sep 14, 2020 | Issued |
Array
(
[id] => 18566807
[patent_doc_number] => 20230257135
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[patent_kind] => A1
[patent_issue_date] => 2023-08-17
[patent_title] => MICRO-CATHODE ARC PROPULSION SYSTEM
[patent_app_type] => utility
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[rel_patent_id] =>[rel_patent_doc_number] =>) 17/918901 | MICRO-CATHODE ARC PROPULSION SYSTEM | Sep 13, 2020 | Abandoned |
Array
(
[id] => 17461121
[patent_doc_number] => 20220074426
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[patent_kind] => A1
[patent_issue_date] => 2022-03-10
[patent_title] => SYSTEMS FOR INTERSTAGE PARTICLE SEPARATION IN MULTISTAGE RADIAL COMPRESSORS OF TURBINE ENGINES
[patent_app_type] => utility
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[rel_patent_id] =>[rel_patent_doc_number] =>) 17/014701 | Systems for interstage particle separation in multistage radial compressors of turbine engines | Sep 7, 2020 | Issued |
Array
(
[id] => 17838454
[patent_doc_number] => 20220275759
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[patent_kind] => A1
[patent_issue_date] => 2022-09-01
[patent_title] => FLAME CONTROL IN AN OXYFUEL COMBUSTION PROCESS
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[rel_patent_id] =>[rel_patent_doc_number] =>) 17/638061 | Flame control in an oxyfuel combustion process | Aug 25, 2020 | Issued |
Array
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[patent_title] => Anterior part of a nacelle of an aircraft propulsion system having a shield in front of its rigidifying frame
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Array
(
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Array
(
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[patent_title] => Gas turbine engine flow control
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Array
(
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[patent_title] => GAS TURBINE HEATER AND DUAL FUEL GAS TURBINE ENGINE
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Array
(
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[patent_title] => ACOUSTIC ATTENUATOR, TUBE ASSEMBLY, COMBUSTOR, GAS TURBINE, AND METHOD FOR MANUFACTURING TUBE ASSEMBLY
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Array
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Array
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[rel_patent_id] =>[rel_patent_doc_number] =>) 17/620455 | Radio-frequency plasma generating system and method for adjusting the same | Jun 16, 2020 | Issued |