
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] => 9030349
[patent_doc_number] => 20130232987
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2013-09-12
[patent_title] => 'GAS TURBINE FUEL INJECTOR WITH INSULATING AIR SHROUD'
[patent_app_type] => utility
[patent_app_number] => 13/672208
[patent_app_country] => US
[patent_app_date] => 2012-11-08
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 6
[patent_figures_cnt] => 6
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[patent_current_assignee] =>[type] => publication
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13672208
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/672208 | GAS TURBINE FUEL INJECTOR WITH INSULATING AIR SHROUD | Nov 7, 2012 | Abandoned |
Array
(
[id] => 10908135
[patent_doc_number] => 20140311149
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2014-10-23
[patent_title] => 'GAS TURBINE ENGINE FAN BLADE AIRFOIL PROFILE'
[patent_app_type] => utility
[patent_app_number] => 13/664647
[patent_app_country] => US
[patent_app_date] => 2012-10-31
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
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[rel_patent_id] =>[rel_patent_doc_number] =>) 13/664647 | Gas turbine engine fan blade airfoil profile | Oct 30, 2012 | Issued |
Array
(
[id] => 10935316
[patent_doc_number] => 20140338337
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2014-11-20
[patent_title] => 'INJECTORS FOR MULTIPOINT INJECTION'
[patent_app_type] => utility
[patent_app_number] => 13/665497
[patent_app_country] => US
[patent_app_date] => 2012-10-31
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
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[rel_patent_id] =>[rel_patent_doc_number] =>) 13/665497 | Injectors for multipoint injection | Oct 30, 2012 | Issued |
Array
(
[id] => 10089877
[patent_doc_number] => 09126690
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2015-09-08
[patent_title] => 'Nacelle for an aircraft engine with cascade-type thrust reverser and variable-geometry nozzle'
[patent_app_type] => utility
[patent_app_number] => 13/662872
[patent_app_country] => US
[patent_app_date] => 2012-10-29
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 2
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[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13662872
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/662872 | Nacelle for an aircraft engine with cascade-type thrust reverser and variable-geometry nozzle | Oct 28, 2012 | Issued |
Array
(
[id] => 8776482
[patent_doc_number] => 20130098457
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2013-04-25
[patent_title] => 'Method and Apparatus for Supplying Heated, Pressurized Air'
[patent_app_type] => utility
[patent_app_number] => 13/656234
[patent_app_country] => US
[patent_app_date] => 2012-10-19
[patent_effective_date] => 0000-00-00
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[rel_patent_id] =>[rel_patent_doc_number] =>) 13/656234 | Method and apparatus for supplying heated, pressurized air | Oct 18, 2012 | Issued |
Array
(
[id] => 10880429
[patent_doc_number] => 08904800
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2014-12-09
[patent_title] => 'Combustor heat shield with integrated louver and method of manufacturing the same'
[patent_app_type] => utility
[patent_app_number] => 13/648530
[patent_app_country] => US
[patent_app_date] => 2012-10-10
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[rel_patent_id] =>[rel_patent_doc_number] =>) 13/648530 | Combustor heat shield with integrated louver and method of manufacturing the same | Oct 9, 2012 | Issued |
Array
(
[id] => 10608896
[patent_doc_number] => 09328923
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2016-05-03
[patent_title] => 'System and method for separating fluids'
[patent_app_type] => utility
[patent_app_number] => 13/649090
[patent_app_country] => US
[patent_app_date] => 2012-10-10
[patent_effective_date] => 0000-00-00
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[rel_patent_id] =>[rel_patent_doc_number] =>) 13/649090 | System and method for separating fluids | Oct 9, 2012 | Issued |
Array
(
[id] => 10104410
[patent_doc_number] => 09140187
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2015-09-22
[patent_title] => 'Magnetic de-icing'
[patent_app_type] => utility
[patent_app_number] => 13/646456
[patent_app_country] => US
[patent_app_date] => 2012-10-05
[patent_effective_date] => 0000-00-00
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[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13646456
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/646456 | Magnetic de-icing | Oct 4, 2012 | Issued |
Array
(
[id] => 8648702
[patent_doc_number] => 20130034432
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2013-02-07
[patent_title] => 'CORRUGATED CORE COWL FOR A GAS TURBINE ENGINE'
[patent_app_type] => utility
[patent_app_number] => 13/617220
[patent_app_country] => US
[patent_app_date] => 2012-09-14
[patent_effective_date] => 0000-00-00
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[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13617220
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/617220 | Corrugated core cowl for a gas turbine engine | Sep 13, 2012 | Issued |
Array
(
[id] => 9962484
[patent_doc_number] => 09010085
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2015-04-21
[patent_title] => 'Turbine section of high bypass turbofan'
[patent_app_type] => utility
[patent_app_number] => 13/599175
[patent_app_country] => US
[patent_app_date] => 2012-08-30
[patent_effective_date] => 0000-00-00
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[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13599175
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/599175 | Turbine section of high bypass turbofan | Aug 29, 2012 | Issued |
Array
(
[id] => 11815741
[patent_doc_number] => 09719685
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2017-08-01
[patent_title] => 'System and method for flame stabilization'
[patent_app_type] => utility
[patent_app_number] => 13/557750
[patent_app_country] => US
[patent_app_date] => 2012-07-25
[patent_effective_date] => 0000-00-00
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[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13557750
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/557750 | System and method for flame stabilization | Jul 24, 2012 | Issued |
Array
(
[id] => 9265485
[patent_doc_number] => 20140020401
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2014-01-23
[patent_title] => 'METHOD FOR CONDITIONING A POWER SUPPLY FOR STARTING A JET ENGINE'
[patent_app_type] => utility
[patent_app_number] => 13/552071
[patent_app_country] => US
[patent_app_date] => 2012-07-18
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[rel_patent_id] =>[rel_patent_doc_number] =>) 13/552071 | Method for conditioning a power supply for starting a jet engine | Jul 17, 2012 | Issued |
Array
(
[id] => 12106803
[patent_doc_number] => 09863279
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2018-01-09
[patent_title] => 'Multipurpose support system for a gas turbine'
[patent_app_type] => utility
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[rel_patent_id] =>[rel_patent_doc_number] =>) 13/546998 | Multipurpose support system for a gas turbine | Jul 10, 2012 | Issued |
Array
(
[id] => 9218988
[patent_doc_number] => 20140013763
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2014-01-16
[patent_title] => 'FUEL-AIR PRE-MIXER WITH PREFILMER'
[patent_app_type] => utility
[patent_app_number] => 13/545418
[patent_app_country] => US
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[rel_patent_id] =>[rel_patent_doc_number] =>) 13/545418 | Fuel-air pre-mixer with prefilmer | Jul 9, 2012 | Issued |
Array
(
[id] => 10581410
[patent_doc_number] => 09303528
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2016-04-05
[patent_title] => 'Mid-turbine frame thermal radiation shield'
[patent_app_type] => utility
[patent_app_number] => 13/543243
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[rel_patent_id] =>[rel_patent_doc_number] =>) 13/543243 | Mid-turbine frame thermal radiation shield | Jul 5, 2012 | Issued |
Array
(
[id] => 10149533
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[patent_issue_date] => 2015-11-10
[patent_title] => 'Air regulation for film cooling and emission control of combustion gas structure'
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[rel_patent_id] =>[rel_patent_doc_number] =>) 13/541841 | Air regulation for film cooling and emission control of combustion gas structure | Jul 4, 2012 | Issued |
Array
(
[id] => 9201089
[patent_doc_number] => 20140000266
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[patent_kind] => A1
[patent_issue_date] => 2014-01-02
[patent_title] => 'Gas Turbine Fuel Nozzle End Cover Using Au-Ni Braze and Method Producing Same'
[patent_app_type] => utility
[patent_app_number] => 13/536577
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[rel_patent_id] =>[rel_patent_doc_number] =>) 13/536577 | Gas turbine fuel nozzle end cover using Au--Ni braze and method producing same | Jun 27, 2012 | Issued |
Array
(
[id] => 8498385
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[patent_title] => 'GAS TURBINE ENGINE'
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Array
(
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[patent_title] => 'Heat exchanger having swirling means'
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[rel_patent_id] =>[rel_patent_doc_number] =>) 13/524460 | Heat exchanger having swirling means | Jun 14, 2012 | Issued |
Array
(
[id] => 8518549
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[patent_title] => 'AIRCRAFT POWERPLANT'
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[rel_patent_id] =>[rel_patent_doc_number] =>) 13/523315 | Aircraft powerplant with moveable nozzle member | Jun 13, 2012 | Issued |