
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] => 12227972
[patent_doc_number] => 09915207
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2018-03-13
[patent_title] => 'Ignition unit for turbojet engine'
[patent_app_type] => utility
[patent_app_number] => 14/386656
[patent_app_country] => US
[patent_app_date] => 2013-03-22
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
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[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14386656
[rel_patent_id] =>[rel_patent_doc_number] =>) 14/386656 | Ignition unit for turbojet engine | Mar 21, 2013 | Issued |
Array
(
[id] => 11171832
[patent_doc_number] => 09404416
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2016-08-02
[patent_title] => 'Generator compressor combination power system'
[patent_app_type] => utility
[patent_app_number] => 13/847354
[patent_app_country] => US
[patent_app_date] => 2013-03-19
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[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13847354
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/847354 | Generator compressor combination power system | Mar 18, 2013 | Issued |
Array
(
[id] => 10453297
[patent_doc_number] => 20150338312
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2015-11-26
[patent_title] => 'Systems and Methods for Implementing Engine Cycle Count'
[patent_app_type] => utility
[patent_app_number] => 14/761476
[patent_app_country] => US
[patent_app_date] => 2013-03-15
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 6
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[rel_patent_id] =>[rel_patent_doc_number] =>) 14/761476 | Systems and Methods for Implementing Engine Cycle Count | Mar 14, 2013 | Abandoned |
Array
(
[id] => 9725638
[patent_doc_number] => 20140261341
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2014-09-18
[patent_title] => 'MULTI-CYCLE STRATIFIED INTERNAL COMBUSTION SYSTEM'
[patent_app_type] => utility
[patent_app_number] => 13/841988
[patent_app_country] => US
[patent_app_date] => 2013-03-15
[patent_effective_date] => 0000-00-00
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[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13841988
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/841988 | Multi-cycle stratified internal combustion system | Mar 14, 2013 | Issued |
Array
(
[id] => 9177003
[patent_doc_number] => 20130318988
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2013-12-05
[patent_title] => 'AIRCRAFT ENGINE WITH TURBINE HEAT EXCHANGER BYPASS'
[patent_app_type] => utility
[patent_app_number] => 13/800434
[patent_app_country] => US
[patent_app_date] => 2013-03-13
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[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13800434
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/800434 | AIRCRAFT ENGINE WITH TURBINE HEAT EXCHANGER BYPASS | Mar 12, 2013 | |
Array
(
[id] => 12369849
[patent_doc_number] => 09958161
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2018-05-01
[patent_title] => Combustor for gas turbine engine
[patent_app_type] => utility
[patent_app_number] => 13/795082
[patent_app_country] => US
[patent_app_date] => 2013-03-12
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[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13795082
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/795082 | Combustor for gas turbine engine | Mar 11, 2013 | Issued |
Array
(
[id] => 10130009
[patent_doc_number] => 09163837
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2015-10-20
[patent_title] => 'Flow conditioner in a combustor of a gas turbine engine'
[patent_app_type] => utility
[patent_app_number] => 13/778769
[patent_app_country] => US
[patent_app_date] => 2013-02-27
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[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13778769
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/778769 | Flow conditioner in a combustor of a gas turbine engine | Feb 26, 2013 | Issued |
Array
(
[id] => 10523228
[patent_doc_number] => 09249730
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2016-02-02
[patent_title] => 'Integrated inducer heat exchanger for gas turbines'
[patent_app_type] => utility
[patent_app_number] => 13/755500
[patent_app_country] => US
[patent_app_date] => 2013-01-31
[patent_effective_date] => 0000-00-00
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[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13755500
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/755500 | Integrated inducer heat exchanger for gas turbines | Jan 30, 2013 | Issued |
Array
(
[id] => 11219400
[patent_doc_number] => 09447730
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2016-09-20
[patent_title] => 'Purge method and purge unit for gas turbine combustor'
[patent_app_type] => utility
[patent_app_number] => 13/755447
[patent_app_country] => US
[patent_app_date] => 2013-01-31
[patent_effective_date] => 0000-00-00
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[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13755447
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/755447 | Purge method and purge unit for gas turbine combustor | Jan 30, 2013 | Issued |
Array
(
[id] => 9599781
[patent_doc_number] => 20140196462
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2014-07-17
[patent_title] => 'SYSTEMS AND METHODS FOR IMPLEMENTING ENGINE CYCLE COUNT'
[patent_app_type] => utility
[patent_app_number] => 13/743006
[patent_app_country] => US
[patent_app_date] => 2013-01-16
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[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13743006
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/743006 | Systems and methods for implementing engine cycle count | Jan 15, 2013 | Issued |
Array
(
[id] => 9018332
[patent_doc_number] => 08528312
[patent_country] => US
[patent_kind] => B1
[patent_issue_date] => 2013-09-10
[patent_title] => 'Turbojet engine inlet and exhaust covers'
[patent_app_type] => utility
[patent_app_number] => 13/736901
[patent_app_country] => US
[patent_app_date] => 2013-01-08
[patent_effective_date] => 0000-00-00
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[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13736901
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/736901 | Turbojet engine inlet and exhaust covers | Jan 7, 2013 | Issued |
Array
(
[id] => 9975481
[patent_doc_number] => 09021781
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2015-05-05
[patent_title] => 'Fuel injector having an ignitor for igniting a combustor of a gas turbine'
[patent_app_type] => utility
[patent_app_number] => 13/734165
[patent_app_country] => US
[patent_app_date] => 2013-01-04
[patent_effective_date] => 0000-00-00
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[rel_patent_id] =>[rel_patent_doc_number] =>) 13/734165 | Fuel injector having an ignitor for igniting a combustor of a gas turbine | Jan 3, 2013 | Issued |
Array
(
[id] => 9560478
[patent_doc_number] => 20140178191
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2014-06-26
[patent_title] => 'Diffuser Assemblies Having at Least One Adjustable Flow Deflecting Member'
[patent_app_type] => utility
[patent_app_number] => 13/724137
[patent_app_country] => US
[patent_app_date] => 2012-12-21
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[rel_patent_id] =>[rel_patent_doc_number] =>) 13/724137 | Diffuser assemblies having at least one adjustable flow deflecting member | Dec 20, 2012 | Issued |
Array
(
[id] => 9176979
[patent_doc_number] => 20130318965
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2013-12-05
[patent_title] => 'Supercharged Combined Cycle System With Air Flow Bypass To HRSG And Hydraulically Coupled Fan'
[patent_app_type] => utility
[patent_app_number] => 13/721946
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[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13721946
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/721946 | Supercharged Combined Cycle System With Air Flow Bypass To HRSG And Hydraulically Coupled Fan | Dec 19, 2012 | Abandoned |
Array
(
[id] => 9630606
[patent_doc_number] => 20140208714
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2014-07-31
[patent_title] => 'Thermal Management for Gas Turbine Engine'
[patent_app_type] => utility
[patent_app_number] => 13/719706
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[rel_patent_id] =>[rel_patent_doc_number] =>) 13/719706 | Thermal Management for Gas Turbine Engine | Dec 18, 2012 | Abandoned |
Array
(
[id] => 9634173
[patent_doc_number] => 20140212281
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2014-07-31
[patent_title] => 'Flow Feed Diffuser'
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[rel_patent_id] =>[rel_patent_doc_number] =>) 13/719748 | Flow feed diffuser | Dec 18, 2012 | Issued |
Array
(
[id] => 9887127
[patent_doc_number] => 08973369
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2015-03-10
[patent_title] => 'Gas-turbine burner having inflow guide means'
[patent_app_type] => utility
[patent_app_number] => 13/715233
[patent_app_country] => US
[patent_app_date] => 2012-12-14
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[rel_patent_id] =>[rel_patent_doc_number] =>) 13/715233 | Gas-turbine burner having inflow guide means | Dec 13, 2012 | Issued |
Array
(
[id] => 9540943
[patent_doc_number] => 20140165590
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2014-06-19
[patent_title] => 'TURBINE HUB RETAINER'
[patent_app_type] => utility
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[patent_app_country] => US
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[rel_patent_id] =>[rel_patent_doc_number] =>) 13/713513 | Turbine hub retainer | Dec 12, 2012 | Issued |
Array
(
[id] => 12212704
[patent_doc_number] => 09909502
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[patent_kind] => B2
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[patent_title] => 'Battery current regulation'
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Array
(
[id] => 8912951
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[patent_title] => 'TURBOMACHINE COMPONENT ALIGNMENT'
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