
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] => 12227994
[patent_doc_number] => 09915229
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2018-03-13
[patent_title] => 'Bleed duct assembly for a gas turbine engine'
[patent_app_type] => utility
[patent_app_number] => 14/455531
[patent_app_country] => US
[patent_app_date] => 2014-08-08
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 12
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[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14455531
[rel_patent_id] =>[rel_patent_doc_number] =>) 14/455531 | Bleed duct assembly for a gas turbine engine | Aug 7, 2014 | Issued |
Array
(
[id] => 10679061
[patent_doc_number] => 20160025206
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2016-01-28
[patent_title] => 'AIRCRAFT GASEOUS COOLING SYSTEM'
[patent_app_type] => utility
[patent_app_number] => 14/340340
[patent_app_country] => US
[patent_app_date] => 2014-07-24
[patent_effective_date] => 0000-00-00
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[rel_patent_id] =>[rel_patent_doc_number] =>) 14/340340 | Aircraft gaseous cooling system | Jul 23, 2014 | Issued |
Array
(
[id] => 10915117
[patent_doc_number] => 20140318136
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2014-10-30
[patent_title] => 'Gas Turbine Combustor Including a Transition Piece Flow Sleeve Wrapped on an Outside Surface of a Transition Piece'
[patent_app_type] => utility
[patent_app_number] => 14/325597
[patent_app_country] => US
[patent_app_date] => 2014-07-08
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 9
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[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14325597
[rel_patent_id] =>[rel_patent_doc_number] =>) 14/325597 | Gas turbine combustor including a transition piece flow sleeve wrapped on an outside surface of a transition piece | Jul 7, 2014 | Issued |
Array
(
[id] => 10907944
[patent_doc_number] => 20140310959
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2014-10-23
[patent_title] => 'FREQUENCY-TUNABLE BRACKETLESS FLUID MANIFOLD'
[patent_app_type] => utility
[patent_app_number] => 14/324952
[patent_app_country] => US
[patent_app_date] => 2014-07-07
[patent_effective_date] => 0000-00-00
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[rel_patent_id] =>[rel_patent_doc_number] =>) 14/324952 | FREQUENCY-TUNABLE BRACKETLESS FLUID MANIFOLD | Jul 6, 2014 | Abandoned |
Array
(
[id] => 12113292
[patent_doc_number] => 09869277
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2018-01-16
[patent_title] => 'System, method and apparatus for lean combustion with plasma from an electrical arc'
[patent_app_type] => utility
[patent_app_number] => 14/288898
[patent_app_country] => US
[patent_app_date] => 2014-05-28
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 7
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[rel_patent_id] =>[rel_patent_doc_number] =>) 14/288898 | System, method and apparatus for lean combustion with plasma from an electrical arc | May 27, 2014 | Issued |
Array
(
[id] => 10090808
[patent_doc_number] => 09127623
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2015-09-08
[patent_title] => 'Thrust reverser device'
[patent_app_type] => utility
[patent_app_number] => 14/271626
[patent_app_country] => US
[patent_app_date] => 2014-05-07
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[rel_patent_id] =>[rel_patent_doc_number] =>) 14/271626 | Thrust reverser device | May 6, 2014 | Issued |
Array
(
[id] => 10431254
[patent_doc_number] => 20150316266
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2015-11-05
[patent_title] => 'BURNER WITH ADJUSTABLE RADIAL FUEL PROFILE'
[patent_app_type] => utility
[patent_app_number] => 14/265584
[patent_app_country] => US
[patent_app_date] => 2014-04-30
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[rel_patent_id] =>[rel_patent_doc_number] =>) 14/265584 | BURNER WITH ADJUSTABLE RADIAL FUEL PROFILE | Apr 29, 2014 | Abandoned |
Array
(
[id] => 10423367
[patent_doc_number] => 20150308378
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2015-10-29
[patent_title] => 'THRUST REVERSER WITH ONE OR MORE BUTRESSING CORNER CASCADE PORTIONS'
[patent_app_type] => utility
[patent_app_number] => 14/261025
[patent_app_country] => US
[patent_app_date] => 2014-04-24
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 8
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[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14261025
[rel_patent_id] =>[rel_patent_doc_number] =>) 14/261025 | Thrust reverser with one or more butressing corner cascade portions | Apr 23, 2014 | Issued |
Array
(
[id] => 9681280
[patent_doc_number] => 20140238042
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2014-08-28
[patent_title] => 'GAS TURBINE ENGINE BUFFER SYSTEM'
[patent_app_type] => utility
[patent_app_number] => 14/246175
[patent_app_country] => US
[patent_app_date] => 2014-04-07
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[rel_patent_id] =>[rel_patent_doc_number] =>) 14/246175 | Gas turbine engine buffer system | Apr 6, 2014 | Issued |
Array
(
[id] => 9981659
[patent_doc_number] => 09027353
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[patent_issue_date] => 2015-05-12
[patent_title] => 'Gas turbine engine buffer system'
[patent_app_type] => utility
[patent_app_number] => 14/219070
[patent_app_country] => US
[patent_app_date] => 2014-03-19
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[rel_patent_id] =>[rel_patent_doc_number] =>) 14/219070 | Gas turbine engine buffer system | Mar 18, 2014 | Issued |
Array
(
[id] => 11076812
[patent_doc_number] => 20160273776
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2016-09-22
[patent_title] => 'COMBUSTOR AND GAS TURBINE'
[patent_app_type] => utility
[patent_app_number] => 14/777685
[patent_app_country] => US
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[rel_patent_id] =>[rel_patent_doc_number] =>) 14/777685 | Combustor and gas turbine | Mar 18, 2014 | Issued |
Array
(
[id] => 10476870
[patent_doc_number] => 20150361887
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2015-12-17
[patent_title] => 'GAS TURBINE ENGINE WITH GEARED TURBOFAN AND OIL THERMAL MANAGEMENT SYSTEM WITH UNIQUE HEAT EXCHANGER STRUCTURE'
[patent_app_type] => utility
[patent_app_number] => 14/761427
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[rel_patent_id] =>[rel_patent_doc_number] =>) 14/761427 | Gas turbine engine with geared turbofan and oil thermal management system with unique heat exchanger structure | Mar 13, 2014 | Issued |
Array
(
[id] => 10469450
[patent_doc_number] => 20150354467
[patent_country] => US
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[patent_issue_date] => 2015-12-10
[patent_title] => 'GAS TURBINE SYSTEM, GAS TURBINE COMBUSTOR CONTROL DEVICE, AND GAS TURBINE COMBUSTOR CONTROL METHOD'
[patent_app_type] => utility
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[rel_patent_id] =>[rel_patent_doc_number] =>) 14/760519 | GAS TURBINE SYSTEM, GAS TURBINE COMBUSTOR CONTROL DEVICE, AND GAS TURBINE COMBUSTOR CONTROL METHOD | Feb 17, 2014 | Abandoned |
Array
(
[id] => 13765227
[patent_doc_number] => 10174949
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2019-01-08
[patent_title] => Gas turbine engine combustor liner assembly with convergent hyperbolic profile
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[rel_patent_id] =>[rel_patent_doc_number] =>) 14/765227 | Gas turbine engine combustor liner assembly with convergent hyperbolic profile | Feb 4, 2014 | Issued |
Array
(
[id] => 10026855
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[patent_issue_date] => 2015-06-30
[patent_title] => 'Swirler for gas turbine engine fuel injector'
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[rel_patent_id] =>[rel_patent_doc_number] =>) 14/155408 | Swirler for gas turbine engine fuel injector | Jan 14, 2014 | Issued |
Array
(
[id] => 10469486
[patent_doc_number] => 20150354502
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[patent_kind] => A1
[patent_issue_date] => 2015-12-10
[patent_title] => 'ENGINE ARCHITECTURE WITH REVERSE ROTATION INTEGRAL DRIVE AND VANELESS TURBINE'
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[rel_patent_id] =>[rel_patent_doc_number] =>) 14/761698 | Engine architecture with reverse rotation integral drive and vaneless turbine | Jan 13, 2014 | Issued |
Array
(
[id] => 9670226
[patent_doc_number] => 20140234089
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[patent_issue_date] => 2014-08-21
[patent_title] => 'ACTUATING ASSEMBLY FOR A THRUST REVERSER OF AN AIRCRAFT ENGINE'
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[patent_app_number] => 14/133327
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[rel_patent_id] =>[rel_patent_doc_number] =>) 14/133327 | Actuating assembly for a thrust reverser of an aircraft engine | Dec 17, 2013 | Issued |
Array
(
[id] => 9556343
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[patent_title] => 'TURBINE SECTION OF HIGH BYPASS TURBOFAN'
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[rel_patent_id] =>[rel_patent_doc_number] =>) 14/102764 | Turbine section of high bypass turbofan | Dec 10, 2013 | Issued |
Array
(
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[rel_patent_id] =>[rel_patent_doc_number] =>) 14/070698 | Combustion chamber for a turbine engine | Nov 3, 2013 | Issued |
Array
(
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[rel_patent_id] =>[rel_patent_doc_number] =>) 14/044282 | Gas turbine engine buffer system | Oct 1, 2013 | Issued |