
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] => 9194073
[patent_doc_number] => 20130333388
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2013-12-19
[patent_title] => 'COMBUSTOR LINER COOLING ASSEMBLY FOR A GAS TURBINE SYSTEM'
[patent_app_type] => utility
[patent_app_number] => 13/495674
[patent_app_country] => US
[patent_app_date] => 2012-06-13
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
[patent_figures_cnt] => 5
[patent_no_of_words] => 2444
[patent_no_of_claims] => 20
[patent_no_of_ind_claims] => 3
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[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13495674
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/495674 | COMBUSTOR LINER COOLING ASSEMBLY FOR A GAS TURBINE SYSTEM | Jun 12, 2012 | Abandoned |
Array
(
[id] => 8518547
[patent_doc_number] => 20120317955
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2012-12-20
[patent_title] => 'SURGE MARGIN CONTROL'
[patent_app_type] => utility
[patent_app_number] => 13/493433
[patent_app_country] => US
[patent_app_date] => 2012-06-11
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 4
[patent_no_of_words] => 3025
[patent_no_of_claims] => 20
[patent_no_of_ind_claims] => 2
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[patent_maintenance] => 1
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[patent_current_assignee] =>[type] => publication
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13493433
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/493433 | Surge margin control | Jun 10, 2012 | Issued |
Array
(
[id] => 9187740
[patent_doc_number] => 20130327055
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2013-12-12
[patent_title] => 'TRANSITION PIECE FOR A GAS TURBOMACHINE'
[patent_app_type] => utility
[patent_app_number] => 13/489776
[patent_app_country] => US
[patent_app_date] => 2012-06-06
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
[patent_figures_cnt] => 5
[patent_no_of_words] => 1945
[patent_no_of_claims] => 20
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[patent_maintenance] => 1
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[patent_current_assignee] =>[type] => publication
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13489776
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/489776 | TRANSITION PIECE FOR A GAS TURBOMACHINE | Jun 5, 2012 | Abandoned |
Array
(
[id] => 8492042
[patent_doc_number] => 20120291449
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2012-11-22
[patent_title] => 'Turbine Section of High Bypass Turbofan'
[patent_app_type] => utility
[patent_app_number] => 13/475252
[patent_app_country] => US
[patent_app_date] => 2012-05-18
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 4
[patent_no_of_words] => 3153
[patent_no_of_claims] => 21
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 0
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13475252
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/475252 | Turbine section of high bypass turbofan | May 17, 2012 | Issued |
Array
(
[id] => 9392976
[patent_doc_number] => 20140090382
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2014-04-03
[patent_title] => 'ANNULAR COMBUSTION CHAMBER FOR A TURBINE ENGINE'
[patent_app_type] => utility
[patent_app_number] => 14/118393
[patent_app_country] => US
[patent_app_date] => 2012-05-11
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 7
[patent_figures_cnt] => 7
[patent_no_of_words] => 5990
[patent_no_of_claims] => 14
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 0
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14118393
[rel_patent_id] =>[rel_patent_doc_number] =>) 14/118393 | Annular combustion chamber for a turbine engine | May 10, 2012 | Issued |
Array
(
[id] => 8473252
[patent_doc_number] => 20120272659
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2012-11-01
[patent_title] => 'REHEAT BURNER INJECTION SYSTEM'
[patent_app_type] => utility
[patent_app_number] => 13/465898
[patent_app_country] => US
[patent_app_date] => 2012-05-07
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 6
[patent_figures_cnt] => 6
[patent_no_of_words] => 6209
[patent_no_of_claims] => 20
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[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13465898
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/465898 | Reheat burner injection system | May 6, 2012 | Issued |
Array
(
[id] => 9116886
[patent_doc_number] => 20130283808
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2013-10-31
[patent_title] => 'SYSTEM AND METHOD FOR COOLING A GAS TURBINE WITH AN EXHAUST GAS PROVIDED BY THE GAS TURBINE'
[patent_app_type] => utility
[patent_app_number] => 13/456575
[patent_app_country] => US
[patent_app_date] => 2012-04-26
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 3
[patent_no_of_words] => 4886
[patent_no_of_claims] => 20
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 0
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13456575
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/456575 | System and method for cooling a gas turbine with an exhaust gas provided by the gas turbine | Apr 25, 2012 | Issued |
Array
(
[id] => 9103326
[patent_doc_number] => 20130276457
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2013-10-24
[patent_title] => 'AIRFOIL INCLUDING LOOSE DAMPER'
[patent_app_type] => utility
[patent_app_number] => 13/454488
[patent_app_country] => US
[patent_app_date] => 2012-04-24
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 7
[patent_figures_cnt] => 7
[patent_no_of_words] => 3663
[patent_no_of_claims] => 20
[patent_no_of_ind_claims] => 3
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[patent_current_assignee] =>[type] => publication
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13454488
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/454488 | Airfoil including loose damper | Apr 23, 2012 | Issued |
Array
(
[id] => 9090048
[patent_doc_number] => 20130269359
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2013-10-17
[patent_title] => 'COMBUSTOR FLOW SLEEVE WITH SUPPLEMENTAL AIR SUPPLY'
[patent_app_type] => utility
[patent_app_number] => 13/447542
[patent_app_country] => US
[patent_app_date] => 2012-04-16
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 6
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[patent_no_of_words] => 2910
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[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13447542
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/447542 | COMBUSTOR FLOW SLEEVE WITH SUPPLEMENTAL AIR SUPPLY | Apr 15, 2012 | Abandoned |
Array
(
[id] => 8346665
[patent_doc_number] => 20120207584
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2012-08-16
[patent_title] => 'SEAL LAND WITH AIR INJECTION FOR CAVITY PURGING'
[patent_app_type] => utility
[patent_app_number] => 13/438871
[patent_app_country] => US
[patent_app_date] => 2012-04-04
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 6
[patent_figures_cnt] => 6
[patent_no_of_words] => 2320
[patent_no_of_claims] => 7
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 0
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13438871
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/438871 | Seal land with air injection for cavity purging | Apr 3, 2012 | Issued |
Array
(
[id] => 8479821
[patent_doc_number] => 20120279228
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2012-11-08
[patent_title] => 'GAS COOLER AND METHOD FOR COOLING GAS'
[patent_app_type] => utility
[patent_app_number] => 13/439459
[patent_app_country] => US
[patent_app_date] => 2012-04-04
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 6
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[patent_no_of_words] => 4046
[patent_no_of_claims] => 16
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[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13439459
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/439459 | Gas cooler and method for cooling gas | Apr 3, 2012 | Issued |
Array
(
[id] => 9063469
[patent_doc_number] => 20130255225
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2013-10-03
[patent_title] => 'GAS TURBINE ENGINE THRUST REVERSER SYSTEM'
[patent_app_type] => utility
[patent_app_number] => 13/431356
[patent_app_country] => US
[patent_app_date] => 2012-03-27
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 6
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[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13431356
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/431356 | Gas turbine engine thrust reverser system | Mar 26, 2012 | Issued |
Array
(
[id] => 8449718
[patent_doc_number] => 20120260664
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2012-10-18
[patent_title] => 'FUEL INJECTOR ARRANGEMENT HAVING AN IGNITER'
[patent_app_type] => utility
[patent_app_number] => 13/427424
[patent_app_country] => US
[patent_app_date] => 2012-03-22
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
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[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13427424
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/427424 | Fuel injector arrangement having an igniter | Mar 21, 2012 | Issued |
Array
(
[id] => 9036943
[patent_doc_number] => 20130239581
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2013-09-19
[patent_title] => 'Systems and Methods for Preventing Flashback in a Combustor Assembly'
[patent_app_type] => utility
[patent_app_number] => 13/423854
[patent_app_country] => US
[patent_app_date] => 2012-03-19
[patent_effective_date] => 0000-00-00
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[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13423854
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/423854 | Systems and methods for preventing flashback in a combustor assembly | Mar 18, 2012 | Issued |
Array
(
[id] => 10084004
[patent_doc_number] => 09121346
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2015-09-01
[patent_title] => 'Pump system for TMS AOC reduction'
[patent_app_type] => utility
[patent_app_number] => 13/419649
[patent_app_country] => US
[patent_app_date] => 2012-03-14
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[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13419649
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/419649 | Pump system for TMS AOC reduction | Mar 13, 2012 | Issued |
Array
(
[id] => 11785456
[patent_doc_number] => 09394831
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2016-07-19
[patent_title] => 'Turbomachine drive arrangement'
[patent_app_type] => utility
[patent_app_number] => 13/411920
[patent_app_country] => US
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[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13411920
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/411920 | Turbomachine drive arrangement | Mar 4, 2012 | Issued |
Array
(
[id] => 8355567
[patent_doc_number] => 20120210723
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2012-08-23
[patent_title] => 'GAS TURBINE GENERATOR SET'
[patent_app_type] => utility
[patent_app_number] => 13/410328
[patent_app_country] => US
[patent_app_date] => 2012-03-02
[patent_effective_date] => 0000-00-00
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[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13410328
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/410328 | Gas turbine generator set | Mar 1, 2012 | Issued |
Array
(
[id] => 9013000
[patent_doc_number] => 20130227964
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2013-09-05
[patent_title] => 'TRANSITION PIECE AFT FRAME ASSEMBLY HAVING A HEAT SHIELD'
[patent_app_type] => utility
[patent_app_number] => 13/410417
[patent_app_country] => US
[patent_app_date] => 2012-03-02
[patent_effective_date] => 0000-00-00
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[rel_patent_id] =>[rel_patent_doc_number] =>) 13/410417 | Transition piece aft frame assembly having a heat shield | Mar 1, 2012 | Issued |
Array
(
[id] => 8998797
[patent_doc_number] => 20130219921
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2013-08-29
[patent_title] => 'MID-SECTION OF A CAN-ANNULAR GAS TURBINE ENGINE WITH A COOLING SYSTEM FOR THE TRANSITION'
[patent_app_type] => utility
[patent_app_number] => 13/408061
[patent_app_country] => US
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[rel_patent_id] =>[rel_patent_doc_number] =>) 13/408061 | Mid-section of a can-annular gas turbine engine with a cooling system for the transition | Feb 28, 2012 | Issued |
Array
(
[id] => 8998793
[patent_doc_number] => 20130219917
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2013-08-29
[patent_title] => 'GAS TURBINE ENGINE BUFFER COOLING SYSTEM'
[patent_app_type] => utility
[patent_app_number] => 13/405466
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[rel_patent_id] =>[rel_patent_doc_number] =>) 13/405466 | Gas turbine engine buffer cooling system | Feb 26, 2012 | Issued |