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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] => 17571572 [patent_doc_number] => 11319832 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2022-05-03 [patent_title] => Single movement convergent and convergent-divergent nozzle [patent_app_type] => utility [patent_app_number] => 16/803528 [patent_app_country] => US [patent_app_date] => 2020-02-27 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 5 [patent_figures_cnt] => 8 [patent_no_of_words] => 8527 [patent_no_of_claims] => 20 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 171 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 16803528 [rel_patent_id] =>[rel_patent_doc_number] =>)
16/803528
Single movement convergent and convergent-divergent nozzle Feb 26, 2020 Issued
Array ( [id] => 17468158 [patent_doc_number] => 11274630 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2022-03-15 [patent_title] => Exhaust nozzle with vane support structure for a gas turbine engine [patent_app_type] => utility [patent_app_number] => 16/803535 [patent_app_country] => US [patent_app_date] => 2020-02-27 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 4 [patent_figures_cnt] => 8 [patent_no_of_words] => 5162 [patent_no_of_claims] => 20 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 248 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 16803535 [rel_patent_id] =>[rel_patent_doc_number] =>)
16/803535
Exhaust nozzle with vane support structure for a gas turbine engine Feb 26, 2020 Issued
Array ( [id] => 17052952 [patent_doc_number] => 20210262386 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2021-08-26 [patent_title] => FRAME FOR A HEAT ENGINE [patent_app_type] => utility [patent_app_number] => 16/800375 [patent_app_country] => US [patent_app_date] => 2020-02-25 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 0 [patent_figures_cnt] => 0 [patent_no_of_words] => 16880 [patent_no_of_claims] => 0 [patent_no_of_ind_claims] => -18 [patent_words_short_claim] => 109 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 16800375 [rel_patent_id] =>[rel_patent_doc_number] =>)
16/800375
Frame for a heat engine Feb 24, 2020 Issued
Array ( [id] => 17635572 [patent_doc_number] => 11346290 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2022-05-31 [patent_title] => Speed limiting for power turbine governing and protection in a turboshaft engine [patent_app_type] => utility [patent_app_number] => 16/797572 [patent_app_country] => US [patent_app_date] => 2020-02-21 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 4 [patent_figures_cnt] => 4 [patent_no_of_words] => 4703 [patent_no_of_claims] => 11 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 156 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 16797572 [rel_patent_id] =>[rel_patent_doc_number] =>)
16/797572
Speed limiting for power turbine governing and protection in a turboshaft engine Feb 20, 2020 Issued
Array ( [id] => 17052981 [patent_doc_number] => 20210262415 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2021-08-26 [patent_title] => HIGH BYPASS RATIO ENGINE BYPASS DUCT NOZZLE WITH CONTROLLED NOZZLE AREA [patent_app_type] => utility [patent_app_number] => 16/797236 [patent_app_country] => US [patent_app_date] => 2020-02-21 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 0 [patent_figures_cnt] => 0 [patent_no_of_words] => 3985 [patent_no_of_claims] => 0 [patent_no_of_ind_claims] => -16 [patent_words_short_claim] => 117 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 16797236 [rel_patent_id] =>[rel_patent_doc_number] =>)
16/797236
High bypass ratio engine bypass duct nozzle with controlled nozzle area Feb 20, 2020 Issued
Array ( [id] => 19354866 [patent_doc_number] => 12055299 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2024-08-06 [patent_title] => Combustor and gas turbine [patent_app_type] => utility [patent_app_number] => 17/796491 [patent_app_country] => US [patent_app_date] => 2020-02-19 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 19 [patent_figures_cnt] => 29 [patent_no_of_words] => 12251 [patent_no_of_claims] => 21 [patent_no_of_ind_claims] => 4 [patent_words_short_claim] => 120 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 17796491 [rel_patent_id] =>[rel_patent_doc_number] =>)
17/796491
Combustor and gas turbine Feb 18, 2020 Issued
Array ( [id] => 16313155 [patent_doc_number] => 20200291893 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2020-09-17 [patent_title] => THRUST REVERSER CASCADE FOR AN AIRCRAFT NACELLE [patent_app_type] => utility [patent_app_number] => 16/785117 [patent_app_country] => US [patent_app_date] => 2020-02-07 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 0 [patent_figures_cnt] => 0 [patent_no_of_words] => 5547 [patent_no_of_claims] => 0 [patent_no_of_ind_claims] => -15 [patent_words_short_claim] => 110 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 16785117 [rel_patent_id] =>[rel_patent_doc_number] =>)
16/785117
Thrust reverser cascade for an aircraft nacelle Feb 6, 2020 Issued
Array ( [id] => 18261085 [patent_doc_number] => 11608781 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2023-03-21 [patent_title] => Air intake of an aircraft turbojet engine nacelle comprising ventilation orifices for a de-icing flow of hot air [patent_app_type] => utility [patent_app_number] => 17/427563 [patent_app_country] => US [patent_app_date] => 2020-01-22 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 12 [patent_figures_cnt] => 33 [patent_no_of_words] => 6993 [patent_no_of_claims] => 18 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 206 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 17427563 [rel_patent_id] =>[rel_patent_doc_number] =>)
17/427563
Air intake of an aircraft turbojet engine nacelle comprising ventilation orifices for a de-icing flow of hot air Jan 21, 2020 Issued
Array ( [id] => 17407918 [patent_doc_number] => 11248794 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2022-02-15 [patent_title] => Fluid mixing apparatus using liquid fuel and high- and low-pressure fluid streams [patent_app_type] => utility [patent_app_number] => 16/731306 [patent_app_country] => US [patent_app_date] => 2019-12-31 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 18 [patent_figures_cnt] => 22 [patent_no_of_words] => 11131 [patent_no_of_claims] => 16 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 211 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 16731306 [rel_patent_id] =>[rel_patent_doc_number] =>)
16/731306
Fluid mixing apparatus using liquid fuel and high- and low-pressure fluid streams Dec 30, 2019 Issued
Array ( [id] => 15839755 [patent_doc_number] => 20200135160 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2020-04-30 [patent_title] => ACOUSTIC TREATMENT DEVICE FOR AN AIRCRAFT TURBOJET ENGINE NACELLE [patent_app_type] => utility [patent_app_number] => 16/725411 [patent_app_country] => US [patent_app_date] => 2019-12-23 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 0 [patent_figures_cnt] => 0 [patent_no_of_words] => 3044 [patent_no_of_claims] => 0 [patent_no_of_ind_claims] => -3 [patent_words_short_claim] => 148 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 16725411 [rel_patent_id] =>[rel_patent_doc_number] =>)
16/725411
Acoustic treatment device for an aircraft turbojet engine nacelle Dec 22, 2019 Issued
Array ( [id] => 17728557 [patent_doc_number] => 11384938 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2022-07-12 [patent_title] => Burner, burner system, integrated gasification combined cycle, and method for moving burner [patent_app_type] => utility [patent_app_number] => 17/270131 [patent_app_country] => US [patent_app_date] => 2019-12-20 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 6 [patent_figures_cnt] => 7 [patent_no_of_words] => 11418 [patent_no_of_claims] => 7 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 96 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 17270131 [rel_patent_id] =>[rel_patent_doc_number] =>)
17/270131
Burner, burner system, integrated gasification combined cycle, and method for moving burner Dec 19, 2019 Issued
Array ( [id] => 16916907 [patent_doc_number] => 20210189999 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2021-06-24 [patent_title] => EXHAUST NOZZLE OF A GAS TURBINE ENGINE [patent_app_type] => utility [patent_app_number] => 16/719112 [patent_app_country] => US [patent_app_date] => 2019-12-18 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 0 [patent_figures_cnt] => 0 [patent_no_of_words] => 6046 [patent_no_of_claims] => 0 [patent_no_of_ind_claims] => -18 [patent_words_short_claim] => 219 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 16719112 [rel_patent_id] =>[rel_patent_doc_number] =>)
16/719112
Exhaust nozzle of a gas turbine engine Dec 17, 2019 Issued
Array ( [id] => 16916909 [patent_doc_number] => 20210190001 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2021-06-24 [patent_title] => EXHAUST NOZZLE OF A GAS TURBINE ENGINE [patent_app_type] => utility [patent_app_number] => 16/719079 [patent_app_country] => US [patent_app_date] => 2019-12-18 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 0 [patent_figures_cnt] => 0 [patent_no_of_words] => 5376 [patent_no_of_claims] => 0 [patent_no_of_ind_claims] => -19 [patent_words_short_claim] => 233 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 16719079 [rel_patent_id] =>[rel_patent_doc_number] =>)
16/719079
Exhaust nozzle of a gas turbine engine Dec 17, 2019 Issued
Array ( [id] => 15867831 [patent_doc_number] => 20200141319 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2020-05-07 [patent_title] => COOLING SYSTEMS FOR GAS TURBINE ENGINES [patent_app_type] => utility [patent_app_number] => 16/712458 [patent_app_country] => US [patent_app_date] => 2019-12-12 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 0 [patent_figures_cnt] => 0 [patent_no_of_words] => 5883 [patent_no_of_claims] => 0 [patent_no_of_ind_claims] => -14 [patent_words_short_claim] => 202 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 16712458 [rel_patent_id] =>[rel_patent_doc_number] =>)
16/712458
Cooling systems for gas turbine engines Dec 11, 2019 Issued
Array ( [id] => 16886180 [patent_doc_number] => 20210172375 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2021-06-10 [patent_title] => ENGINE THERMAL MANAGEMENT METHODS AND CONTROL SYSTEMS [patent_app_type] => utility [patent_app_number] => 16/708328 [patent_app_country] => US [patent_app_date] => 2019-12-09 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 0 [patent_figures_cnt] => 0 [patent_no_of_words] => 6640 [patent_no_of_claims] => 0 [patent_no_of_ind_claims] => -17 [patent_words_short_claim] => 84 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 16708328 [rel_patent_id] =>[rel_patent_doc_number] =>)
16/708328
Engine thermal management methods and control systems Dec 8, 2019 Issued
Array ( [id] => 16313436 [patent_doc_number] => 20200292174 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2020-09-17 [patent_title] => SINGLE CAVITY TRAPPED VORTEX COMBUSTOR WITH CMC INNER AND OUTER LINERS [patent_app_type] => utility [patent_app_number] => 16/701226 [patent_app_country] => US [patent_app_date] => 2019-12-03 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 0 [patent_figures_cnt] => 0 [patent_no_of_words] => 10356 [patent_no_of_claims] => 0 [patent_no_of_ind_claims] => -17 [patent_words_short_claim] => 2 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 16701226 [rel_patent_id] =>[rel_patent_doc_number] =>)
16/701226
Single cavity trapped vortex combustor with CMC inner and outer liners Dec 2, 2019 Issued
Array ( [id] => 19292151 [patent_doc_number] => 12031501 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2024-07-09 [patent_title] => Cooling system for an engine assembly [patent_app_type] => utility [patent_app_number] => 16/698287 [patent_app_country] => US [patent_app_date] => 2019-11-27 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 10 [patent_figures_cnt] => 15 [patent_no_of_words] => 9305 [patent_no_of_claims] => 20 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 151 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 16698287 [rel_patent_id] =>[rel_patent_doc_number] =>)
16/698287
Cooling system for an engine assembly Nov 26, 2019 Issued
Array ( [id] => 17468129 [patent_doc_number] => 11274601 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2022-03-15 [patent_title] => Internal fuel/air heat exchangers [patent_app_type] => utility [patent_app_number] => 16/696624 [patent_app_country] => US [patent_app_date] => 2019-11-26 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 4 [patent_figures_cnt] => 4 [patent_no_of_words] => 2197 [patent_no_of_claims] => 18 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 155 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 16696624 [rel_patent_id] =>[rel_patent_doc_number] =>)
16/696624
Internal fuel/air heat exchangers Nov 25, 2019 Issued
Array ( [id] => 16840271 [patent_doc_number] => 20210148283 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2021-05-20 [patent_title] => THERMAL MANAGEMENT SYSTEM WITH THERMAL BUS FOR A GAS TURBINE ENGINE OR AIRCRAFT [patent_app_type] => utility [patent_app_number] => 16/685490 [patent_app_country] => US [patent_app_date] => 2019-11-15 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 0 [patent_figures_cnt] => 0 [patent_no_of_words] => 9968 [patent_no_of_claims] => 0 [patent_no_of_ind_claims] => -17 [patent_words_short_claim] => 123 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 16685490 [rel_patent_id] =>[rel_patent_doc_number] =>)
16/685490
Thermal management system with thermal bus for a gas turbine engine or aircraft Nov 14, 2019 Issued
Array ( [id] => 18911019 [patent_doc_number] => 11873994 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2024-01-16 [patent_title] => Electrically heated catalytic combustor [patent_app_type] => utility [patent_app_number] => 17/309248 [patent_app_country] => US [patent_app_date] => 2019-11-13 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 3 [patent_figures_cnt] => 3 [patent_no_of_words] => 10281 [patent_no_of_claims] => 19 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 112 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 17309248 [rel_patent_id] =>[rel_patent_doc_number] =>)
17/309248
Electrically heated catalytic combustor Nov 12, 2019 Issued
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