Search

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 numberTitle of the applicationFiling DateStatus
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 [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] => 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 [patent_figures_cnt] => 5 [patent_no_of_words] => 2401 [patent_no_of_claims] => 11 [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] => 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 [patent_figures_cnt] => 21 [patent_no_of_words] => 12380 [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] => 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 [patent_figures_cnt] => 4 [patent_no_of_words] => 4927 [patent_no_of_claims] => 24 [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] => 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 [patent_figures_cnt] => 2 [patent_no_of_words] => 4987 [patent_no_of_claims] => 30 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 165 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [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 [patent_figures_cnt] => 11 [patent_no_of_words] => 4319 [patent_no_of_claims] => 24 [patent_no_of_ind_claims] => 7 [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] => 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 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 4 [patent_figures_cnt] => 4 [patent_no_of_words] => 3338 [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] => 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 [patent_app_date] => 2013-04-09 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 4 [patent_figures_cnt] => 5 [patent_no_of_words] => 2229 [patent_no_of_claims] => 7 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 221 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [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 [patent_app_country] => US [patent_app_date] => 2013-04-01 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 2 [patent_figures_cnt] => 2 [patent_no_of_words] => 4681 [patent_no_of_claims] => 24 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 152 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13854225 [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 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 5 [patent_figures_cnt] => 8 [patent_no_of_words] => 7468 [patent_no_of_claims] => 7 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 94 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [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
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