
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] => 10367724
[patent_doc_number] => 20150252729
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2015-09-10
[patent_title] => 'INNER DIFFUSER CASE STRUTS FOR A COMBUSTOR OF A GAS TURBINE ENGINE'
[patent_app_type] => utility
[patent_app_number] => 14/432442
[patent_app_country] => US
[patent_app_date] => 2013-09-27
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 8
[patent_figures_cnt] => 8
[patent_no_of_words] => 3108
[patent_no_of_claims] => 11
[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] => 14432442
[rel_patent_id] =>[rel_patent_doc_number] =>) 14/432442 | Inner diffuser case struts for a combustor of a gas turbine engine | Sep 26, 2013 | Issued |
Array
(
[id] => 11678911
[patent_doc_number] => 09677430
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2017-06-13
[patent_title] => 'Combined cycle power plant'
[patent_app_type] => utility
[patent_app_number] => 14/014797
[patent_app_country] => US
[patent_app_date] => 2013-08-30
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 5
[patent_no_of_words] => 3166
[patent_no_of_claims] => 13
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 333
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14014797
[rel_patent_id] =>[rel_patent_doc_number] =>) 14/014797 | Combined cycle power plant | Aug 29, 2013 | Issued |
Array
(
[id] => 9187732
[patent_doc_number] => 20130327047
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2013-12-12
[patent_title] => 'GAS TURBINE ENGINE VARIABLE AREA EXHAUST NOZZLE'
[patent_app_type] => utility
[patent_app_number] => 13/965362
[patent_app_country] => US
[patent_app_date] => 2013-08-13
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 8
[patent_figures_cnt] => 8
[patent_no_of_words] => 5865
[patent_no_of_claims] => 19
[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] => 13965362
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/965362 | Gas turbine engine variable area exhaust nozzle | Aug 12, 2013 | Issued |
Array
(
[id] => 11613140
[patent_doc_number] => 09650991
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2017-05-16
[patent_title] => 'Pivoting ring petal actuation for variable area fan nozzle'
[patent_app_type] => utility
[patent_app_number] => 13/928407
[patent_app_country] => US
[patent_app_date] => 2013-06-27
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 7
[patent_figures_cnt] => 7
[patent_no_of_words] => 6749
[patent_no_of_claims] => 18
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 236
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13928407
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/928407 | Pivoting ring petal actuation for variable area fan nozzle | Jun 26, 2013 | Issued |
Array
(
[id] => 9187699
[patent_doc_number] => 20130327014
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2013-12-12
[patent_title] => 'Devices and Methods to Optimize Aircraft Power Plant and Aircraft Operations'
[patent_app_type] => utility
[patent_app_number] => 13/914441
[patent_app_country] => US
[patent_app_date] => 2013-06-10
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 4
[patent_no_of_words] => 9630
[patent_no_of_claims] => 10
[patent_no_of_ind_claims] => 1
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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] => 13914441
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/914441 | Devices and Methods to Optimize Aircraft Power Plant and Aircraft Operations | Jun 9, 2013 | Abandoned |
Array
(
[id] => 11635681
[patent_doc_number] => 09657641
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2017-05-23
[patent_title] => 'Fluid flow machine especially gas turbine penetrated axially by a hot gas stream'
[patent_app_type] => utility
[patent_app_number] => 13/912603
[patent_app_country] => US
[patent_app_date] => 2013-06-07
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 4
[patent_no_of_words] => 2490
[patent_no_of_claims] => 7
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 290
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13912603
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/912603 | Fluid flow machine especially gas turbine penetrated axially by a hot gas stream | Jun 6, 2013 | Issued |
Array
(
[id] => 9078073
[patent_doc_number] => 20130263602
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2013-10-10
[patent_title] => 'HIGH TEMPERATURE FUEL MANIFOLD FOR GAS TURBINE ENGINES'
[patent_app_type] => utility
[patent_app_number] => 13/910573
[patent_app_country] => US
[patent_app_date] => 2013-06-05
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 4
[patent_no_of_words] => 3093
[patent_no_of_claims] => 20
[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] => 13910573
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/910573 | High temperature fuel manifold for gas turbine engines | Jun 4, 2013 | Issued |
Array
(
[id] => 9194034
[patent_doc_number] => 20130333349
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2013-12-19
[patent_title] => 'TURBINE EXHAUST DUCT DESIGN FOR AIR COOLED CONDENSERS'
[patent_app_type] => utility
[patent_app_number] => 13/906552
[patent_app_country] => US
[patent_app_date] => 2013-05-31
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 7
[patent_figures_cnt] => 7
[patent_no_of_words] => 2716
[patent_no_of_claims] => 10
[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] => 13906552
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/906552 | Turbine exhaust duct design for air cooled condensers | May 30, 2013 | Issued |
| 13/896083 | Non-Hazardous Coated Rocket Starter | May 15, 2013 | Abandoned |
Array
(
[id] => 11250906
[patent_doc_number] => 09476399
[patent_country] => US
[patent_kind] => B1
[patent_issue_date] => 2016-10-25
[patent_title] => 'Glow plug type acoustic resonance igniter'
[patent_app_type] => utility
[patent_app_number] => 13/894919
[patent_app_country] => US
[patent_app_date] => 2013-05-15
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 2
[patent_figures_cnt] => 7
[patent_no_of_words] => 3960
[patent_no_of_claims] => 20
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 191
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13894919
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/894919 | Glow plug type acoustic resonance igniter | May 14, 2013 | Issued |
Array
(
[id] => 10555142
[patent_doc_number] => 09279340
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2016-03-08
[patent_title] => 'System and method for cooling gas turbine components'
[patent_app_type] => utility
[patent_app_number] => 13/890332
[patent_app_country] => US
[patent_app_date] => 2013-05-09
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 6
[patent_figures_cnt] => 8
[patent_no_of_words] => 4242
[patent_no_of_claims] => 19
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 125
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13890332
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/890332 | System and method for cooling gas turbine components | May 8, 2013 | Issued |
Array
(
[id] => 10942229
[patent_doc_number] => 20140345250
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2014-11-27
[patent_title] => 'IGNITER FOR A GAS TURBINE'
[patent_app_type] => utility
[patent_app_number] => 13/890368
[patent_app_country] => US
[patent_app_date] => 2013-05-09
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
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[patent_no_of_words] => 2401
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[patent_no_of_ind_claims] => 2
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[patent_current_assignee] =>[type] => publication
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13890368
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/890368 | Igniter for a gas turbine | May 8, 2013 | Issued |
Array
(
[id] => 9157453
[patent_doc_number] => 20130305730
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2013-11-21
[patent_title] => 'METHOD FOR PREHEATING FUELS IN A GAS TURBINE ENGINE'
[patent_app_type] => utility
[patent_app_number] => 13/887055
[patent_app_country] => US
[patent_app_date] => 2013-05-03
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 21
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[patent_no_of_words] => 12380
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[patent_current_assignee] =>[type] => publication
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13887055
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/887055 | METHOD FOR PREHEATING FUELS IN A GAS TURBINE ENGINE | May 2, 2013 | Abandoned |
Array
(
[id] => 10915114
[patent_doc_number] => 20140318133
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2014-10-30
[patent_title] => 'THRUST EFFICIENT TURBOFAN ENGINE'
[patent_app_type] => utility
[patent_app_number] => 13/871166
[patent_app_country] => US
[patent_app_date] => 2013-04-26
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
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[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13871166
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/871166 | Thrust efficient turbofan engine | Apr 25, 2013 | Issued |
Array
(
[id] => 11562253
[patent_doc_number] => 09624828
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2017-04-18
[patent_title] => 'Thrust efficient turbofan engine'
[patent_app_type] => utility
[patent_app_number] => 13/871221
[patent_app_country] => US
[patent_app_date] => 2013-04-26
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 2
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[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13871221
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/871221 | Thrust efficient turbofan engine | Apr 25, 2013 | Issued |
Array
(
[id] => 9926984
[patent_doc_number] => 20150075176
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2015-03-19
[patent_title] => 'CONNECTING GAS TURBINE ENGINE ANNULAR MEMBERS'
[patent_app_type] => utility
[patent_app_number] => 14/396206
[patent_app_country] => US
[patent_app_date] => 2013-04-26
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 11
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[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14396206
[rel_patent_id] =>[rel_patent_doc_number] =>) 14/396206 | Connecting gas turbine engine annular members | Apr 25, 2013 | Issued |
Array
(
[id] => 9090001
[patent_doc_number] => 20130269312
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2013-10-17
[patent_title] => 'DEVICE FOR CONTROLLING A VARIABLE SECTION NOZZLE OF AN AIRCRAFT'
[patent_app_type] => utility
[patent_app_number] => 13/864553
[patent_app_country] => US
[patent_app_date] => 2013-04-17
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[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13864553
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/864553 | Device for controlling a variable section nozzle of an aircraft | Apr 16, 2013 | Issued |
Array
(
[id] => 12212635
[patent_doc_number] => 09909433
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2018-03-06
[patent_title] => 'Aircraft gas turbine having a booster bleed duct in a stator vane root element of a bypass duct'
[patent_app_type] => utility
[patent_app_number] => 13/859300
[patent_app_country] => US
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[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13859300
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/859300 | Aircraft gas turbine having a booster bleed duct in a stator vane root element of a bypass duct | Apr 8, 2013 | Issued |
Array
(
[id] => 11562252
[patent_doc_number] => 09624827
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2017-04-18
[patent_title] => 'Thrust efficient turbofan engine'
[patent_app_type] => utility
[patent_app_number] => 13/854225
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[rel_patent_id] =>[rel_patent_doc_number] =>) 13/854225 | Thrust efficient turbofan engine | Mar 31, 2013 | Issued |
Array
(
[id] => 11343342
[patent_doc_number] => 09527736
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2016-12-27
[patent_title] => 'System and method for generating nitrogen from a gas turbine'
[patent_app_type] => utility
[patent_app_number] => 13/851891
[patent_app_country] => US
[patent_app_date] => 2013-03-27
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[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13851891
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/851891 | System and method for generating nitrogen from a gas turbine | Mar 26, 2013 | Issued |