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] => 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 [patent_figures_cnt] => 13 [patent_no_of_words] => 3154 [patent_no_of_claims] => 12 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 110 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [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 [patent_drawing_sheets_cnt] => 6 [patent_figures_cnt] => 6 [patent_no_of_words] => 3911 [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] => 14340340 [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 [patent_figures_cnt] => 9 [patent_no_of_words] => 4974 [patent_no_of_claims] => 2 [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] => 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 [patent_drawing_sheets_cnt] => 8 [patent_figures_cnt] => 8 [patent_no_of_words] => 2407 [patent_no_of_claims] => 16 [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] => 14324952 [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 [patent_figures_cnt] => 7 [patent_no_of_words] => 6189 [patent_no_of_claims] => 28 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 157 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14288898 [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 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 3 [patent_figures_cnt] => 11 [patent_no_of_words] => 4678 [patent_no_of_claims] => 10 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 223 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14271626 [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 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 5 [patent_figures_cnt] => 5 [patent_no_of_words] => 3416 [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] => 14265584 [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 [patent_figures_cnt] => 8 [patent_no_of_words] => 4847 [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] => 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 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 6 [patent_figures_cnt] => 6 [patent_no_of_words] => 5621 [patent_no_of_claims] => 30 [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] => 14246175 [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 [patent_country] => US [patent_kind] => B2 [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 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 7 [patent_figures_cnt] => 7 [patent_no_of_words] => 6782 [patent_no_of_claims] => 32 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 140 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14219070 [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 [patent_app_date] => 2014-03-19 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 11 [patent_figures_cnt] => 11 [patent_no_of_words] => 7005 [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] => 14777685 [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 [patent_app_country] => US [patent_app_date] => 2014-03-14 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 4 [patent_figures_cnt] => 4 [patent_no_of_words] => 4646 [patent_no_of_claims] => 18 [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] => 14761427 [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 [patent_kind] => A1 [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 [patent_app_number] => 14/760519 [patent_app_country] => US [patent_app_date] => 2014-02-18 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 10 [patent_figures_cnt] => 10 [patent_no_of_words] => 4591 [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] => 14760519 [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 [patent_app_type] => utility [patent_app_number] => 14/765227 [patent_app_country] => US [patent_app_date] => 2014-02-05 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 12 [patent_figures_cnt] => 16 [patent_no_of_words] => 4769 [patent_no_of_claims] => 14 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 87 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14765227 [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 [patent_doc_number] => 09068749 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2015-06-30 [patent_title] => 'Swirler for gas turbine engine fuel injector' [patent_app_type] => utility [patent_app_number] => 14/155408 [patent_app_country] => US [patent_app_date] => 2014-01-15 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 3 [patent_figures_cnt] => 4 [patent_no_of_words] => 1708 [patent_no_of_claims] => 19 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 147 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14155408 [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 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2015-12-10 [patent_title] => 'ENGINE ARCHITECTURE WITH REVERSE ROTATION INTEGRAL DRIVE AND VANELESS TURBINE' [patent_app_type] => utility [patent_app_number] => 14/761698 [patent_app_country] => US [patent_app_date] => 2014-01-14 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 7 [patent_figures_cnt] => 7 [patent_no_of_words] => 5064 [patent_no_of_claims] => 15 [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] => 14761698 [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 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2014-08-21 [patent_title] => 'ACTUATING ASSEMBLY FOR A THRUST REVERSER OF AN AIRCRAFT ENGINE' [patent_app_type] => utility [patent_app_number] => 14/133327 [patent_app_country] => US [patent_app_date] => 2013-12-18 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 3 [patent_figures_cnt] => 3 [patent_no_of_words] => 3151 [patent_no_of_claims] => 6 [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] => 14133327 [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 [patent_doc_number] => 20140174055 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2014-06-26 [patent_title] => 'TURBINE SECTION OF HIGH BYPASS TURBOFAN' [patent_app_type] => utility [patent_app_number] => 14/102764 [patent_app_country] => US [patent_app_date] => 2013-12-11 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 4 [patent_figures_cnt] => 4 [patent_no_of_words] => 3630 [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] => 14102764 [rel_patent_id] =>[rel_patent_doc_number] =>)
14/102764
Turbine section of high bypass turbofan Dec 10, 2013 Issued
Array ( [id] => 10915119 [patent_doc_number] => 20140318138 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2014-10-30 [patent_title] => 'COMBUSTION CHAMBER FOR A TURBINE ENGINE' [patent_app_type] => utility [patent_app_number] => 14/070698 [patent_app_country] => US [patent_app_date] => 2013-11-04 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 5 [patent_figures_cnt] => 5 [patent_no_of_words] => 3317 [patent_no_of_claims] => 8 [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] => 14070698 [rel_patent_id] =>[rel_patent_doc_number] =>)
14/070698
Combustion chamber for a turbine engine Nov 3, 2013 Issued
Array ( [id] => 10057789 [patent_doc_number] => 09097138 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2015-08-04 [patent_title] => 'Gas turbine engine buffer system' [patent_app_type] => utility [patent_app_number] => 14/044282 [patent_app_country] => US [patent_app_date] => 2013-10-02 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 7 [patent_figures_cnt] => 7 [patent_no_of_words] => 5779 [patent_no_of_claims] => 15 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 102 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14044282 [rel_patent_id] =>[rel_patent_doc_number] =>)
14/044282
Gas turbine engine buffer system Oct 1, 2013 Issued
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