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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] => 17998402 [patent_doc_number] => 11499502 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2022-11-15 [patent_title] => Dual function cascade integrated variable area fan nozzle and thrust reverser [patent_app_type] => utility [patent_app_number] => 16/895037 [patent_app_country] => US [patent_app_date] => 2020-06-08 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 4 [patent_figures_cnt] => 7 [patent_no_of_words] => 3510 [patent_no_of_claims] => 24 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 304 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 16895037 [rel_patent_id] =>[rel_patent_doc_number] =>)
16/895037
Dual function cascade integrated variable area fan nozzle and thrust reverser Jun 7, 2020 Issued
Array ( [id] => 17793177 [patent_doc_number] => 20220252268 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2022-08-11 [patent_title] => METHOD FOR MANUFACTURING A FLAME TUBE FOR A TURBOMACHINE [patent_app_type] => utility [patent_app_number] => 17/616280 [patent_app_country] => US [patent_app_date] => 2020-06-03 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 0 [patent_figures_cnt] => 0 [patent_no_of_words] => 3789 [patent_no_of_claims] => 0 [patent_no_of_ind_claims] => -9 [patent_words_short_claim] => 150 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 17616280 [rel_patent_id] =>[rel_patent_doc_number] =>)
17/616280
Method for manufacturing a flame tube for a turbomachine Jun 2, 2020 Issued
Array ( [id] => 17259345 [patent_doc_number] => 20210372330 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2021-12-02 [patent_title] => LEAN BLOWOUT PRECURSOR DETECTION FOR GAS TURBINES [patent_app_type] => utility [patent_app_number] => 16/885541 [patent_app_country] => US [patent_app_date] => 2020-05-28 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 0 [patent_figures_cnt] => 0 [patent_no_of_words] => 5562 [patent_no_of_claims] => 0 [patent_no_of_ind_claims] => -15 [patent_words_short_claim] => 65 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 16885541 [rel_patent_id] =>[rel_patent_doc_number] =>)
16/885541
Lean blowout precursor detection for gas turbines May 27, 2020 Issued
Array ( [id] => 17762091 [patent_doc_number] => 20220235703 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2022-07-28 [patent_title] => GAS TURBINE AND CONTROL METHOD THEREOF, AND COMBINED CYCLE PLANT [patent_app_type] => utility [patent_app_number] => 17/614873 [patent_app_country] => US [patent_app_date] => 2020-05-25 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 0 [patent_figures_cnt] => 0 [patent_no_of_words] => 13032 [patent_no_of_claims] => 0 [patent_no_of_ind_claims] => -12 [patent_words_short_claim] => 99 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 17614873 [rel_patent_id] =>[rel_patent_doc_number] =>)
17/614873
Gas turbine and control method thereof, and combined cycle plant May 24, 2020 Issued
Array ( [id] => 16622245 [patent_doc_number] => 20210040898 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2021-02-11 [patent_title] => TURBINE SECTION OF HIGH BYPASS TURBOFAN [patent_app_type] => utility [patent_app_number] => 16/881567 [patent_app_country] => US [patent_app_date] => 2020-05-22 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 0 [patent_figures_cnt] => 0 [patent_no_of_words] => 3142 [patent_no_of_claims] => 0 [patent_no_of_ind_claims] => -23 [patent_words_short_claim] => 67 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 16881567 [rel_patent_id] =>[rel_patent_doc_number] =>)
16/881567
Turbine section of high bypass turbofan May 21, 2020 Issued
Array ( [id] => 17588259 [patent_doc_number] => 11326520 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2022-05-10 [patent_title] => Heat exchange apparatus and gas turbine having the same [patent_app_type] => utility [patent_app_number] => 16/876051 [patent_app_country] => US [patent_app_date] => 2020-05-16 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 15 [patent_figures_cnt] => 15 [patent_no_of_words] => 6964 [patent_no_of_claims] => 19 [patent_no_of_ind_claims] => 3 [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] => 16876051 [rel_patent_id] =>[rel_patent_doc_number] =>)
16/876051
Heat exchange apparatus and gas turbine having the same May 15, 2020 Issued
Array ( [id] => 17762092 [patent_doc_number] => 20220235704 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2022-07-28 [patent_title] => OPTIMIZED HEAT EXCHANGE SYSTEM FOR A TURBOMACHINE [patent_app_type] => utility [patent_app_number] => 17/612129 [patent_app_country] => US [patent_app_date] => 2020-05-11 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 0 [patent_figures_cnt] => 0 [patent_no_of_words] => 7225 [patent_no_of_claims] => 0 [patent_no_of_ind_claims] => -15 [patent_words_short_claim] => 131 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 17612129 [rel_patent_id] =>[rel_patent_doc_number] =>)
17/612129
Optimized heat exchange system for a turbomachine May 10, 2020 Issued
Array ( [id] => 17635526 [patent_doc_number] => 11346244 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2022-05-31 [patent_title] => Heat transfer augmentation feature [patent_app_type] => utility [patent_app_number] => 16/860481 [patent_app_country] => US [patent_app_date] => 2020-04-28 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 8 [patent_figures_cnt] => 13 [patent_no_of_words] => 4969 [patent_no_of_claims] => 16 [patent_no_of_ind_claims] => 6 [patent_words_short_claim] => 78 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 16860481 [rel_patent_id] =>[rel_patent_doc_number] =>)
16/860481
Heat transfer augmentation feature Apr 27, 2020 Issued
Array ( [id] => 19044154 [patent_doc_number] => 11933246 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2024-03-19 [patent_title] => Turbojet engine comprising a nacelle with an air intake to promote a reversed thrust phase [patent_app_type] => utility [patent_app_number] => 17/600071 [patent_app_country] => US [patent_app_date] => 2020-04-08 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 9 [patent_figures_cnt] => 18 [patent_no_of_words] => 6134 [patent_no_of_claims] => 11 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 283 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 17600071 [rel_patent_id] =>[rel_patent_doc_number] =>)
17/600071
Turbojet engine comprising a nacelle with an air intake to promote a reversed thrust phase Apr 7, 2020 Issued
Array ( [id] => 16391774 [patent_doc_number] => 20200332715 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2020-10-22 [patent_title] => MULTIPLE STREAM HEAT EXCHANGER [patent_app_type] => utility [patent_app_number] => 16/843313 [patent_app_country] => US [patent_app_date] => 2020-04-08 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 0 [patent_figures_cnt] => 0 [patent_no_of_words] => 5235 [patent_no_of_claims] => 0 [patent_no_of_ind_claims] => -17 [patent_words_short_claim] => 146 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 16843313 [rel_patent_id] =>[rel_patent_doc_number] =>)
16/843313
Multiple stream heat exchanger Apr 7, 2020 Issued
Array ( [id] => 17363955 [patent_doc_number] => 11230973 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2022-01-25 [patent_title] => Heat-transfer fluid for a cooling system of an aircraft turbojet engine [patent_app_type] => utility [patent_app_number] => 16/839118 [patent_app_country] => US [patent_app_date] => 2020-04-03 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 2 [patent_figures_cnt] => 4 [patent_no_of_words] => 3264 [patent_no_of_claims] => 13 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 81 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 16839118 [rel_patent_id] =>[rel_patent_doc_number] =>)
16/839118
Heat-transfer fluid for a cooling system of an aircraft turbojet engine Apr 2, 2020 Issued
Array ( [id] => 18029461 [patent_doc_number] => 11512638 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2022-11-29 [patent_title] => Surface heat-exchanger for a cooling system of an aircraft turbojet engine [patent_app_type] => utility [patent_app_number] => 16/839123 [patent_app_country] => US [patent_app_date] => 2020-04-03 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 2 [patent_figures_cnt] => 5 [patent_no_of_words] => 3861 [patent_no_of_claims] => 13 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 167 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 16839123 [rel_patent_id] =>[rel_patent_doc_number] =>)
16/839123
Surface heat-exchanger for a cooling system of an aircraft turbojet engine Apr 2, 2020 Issued
Array ( [id] => 18013839 [patent_doc_number] => 11506124 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2022-11-22 [patent_title] => Supercritical CO2 cycle for gas turbine engines having supplemental cooling [patent_app_type] => utility [patent_app_number] => 16/832535 [patent_app_country] => US [patent_app_date] => 2020-03-27 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 8 [patent_figures_cnt] => 9 [patent_no_of_words] => 10978 [patent_no_of_claims] => 19 [patent_no_of_ind_claims] => 9 [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] => 16832535 [rel_patent_id] =>[rel_patent_doc_number] =>)
16/832535
Supercritical CO2 cycle for gas turbine engines having supplemental cooling Mar 26, 2020 Issued
Array ( [id] => 17267962 [patent_doc_number] => 11193379 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2021-12-07 [patent_title] => Turbofan comprising a set of rotatable blades for blocking off the bypass flow duct [patent_app_type] => utility [patent_app_number] => 16/826963 [patent_app_country] => US [patent_app_date] => 2020-03-23 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 3 [patent_figures_cnt] => 5 [patent_no_of_words] => 3047 [patent_no_of_claims] => 3 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 378 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 16826963 [rel_patent_id] =>[rel_patent_doc_number] =>)
16/826963
Turbofan comprising a set of rotatable blades for blocking off the bypass flow duct Mar 22, 2020 Issued
Array ( [id] => 17656684 [patent_doc_number] => 20220177149 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2022-06-09 [patent_title] => AIR INLET DUCT FOR A NACELLE OF AN AIRCRAFT PROPULSION ASSEMBLY [patent_app_type] => utility [patent_app_number] => 17/598987 [patent_app_country] => US [patent_app_date] => 2020-03-19 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 0 [patent_figures_cnt] => 0 [patent_no_of_words] => 2665 [patent_no_of_claims] => 0 [patent_no_of_ind_claims] => -4 [patent_words_short_claim] => 194 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 17598987 [rel_patent_id] =>[rel_patent_doc_number] =>)
17/598987
Air inlet duct for a nacelle of an aircraft propulsion assembly Mar 18, 2020 Issued
Array ( [id] => 17612367 [patent_doc_number] => 20220154646 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2022-05-19 [patent_title] => AMMONIA DECOMPOSITION FACILITY, GAS TURBINE PLANT EQUIPPED WITH SAME, AND AMMONIA DECOMPOSITION METHOD [patent_app_type] => utility [patent_app_number] => 17/437708 [patent_app_country] => US [patent_app_date] => 2020-03-13 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 0 [patent_figures_cnt] => 0 [patent_no_of_words] => 15393 [patent_no_of_claims] => 0 [patent_no_of_ind_claims] => -14 [patent_words_short_claim] => 100 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 17437708 [rel_patent_id] =>[rel_patent_doc_number] =>)
17/437708
Ammonia decomposition facility, gas turbine plant equipped with same, and ammonia decomposition method Mar 12, 2020 Issued
Array ( [id] => 16422584 [patent_doc_number] => 20200347782 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2020-11-05 [patent_title] => AIRCRAFT PROPULSION SYSTEM INCLUDING A HEAT EXCHANGER SYSTEM [patent_app_type] => utility [patent_app_number] => 16/814506 [patent_app_country] => US [patent_app_date] => 2020-03-10 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 0 [patent_figures_cnt] => 0 [patent_no_of_words] => 3532 [patent_no_of_claims] => 0 [patent_no_of_ind_claims] => -5 [patent_words_short_claim] => 440 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 16814506 [rel_patent_id] =>[rel_patent_doc_number] =>)
16/814506
Aircraft propulsion system including a heat exchanger system Mar 9, 2020 Issued
Array ( [id] => 17282136 [patent_doc_number] => 11199159 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2021-12-14 [patent_title] => Thrust efficient turbofan engine [patent_app_type] => utility [patent_app_number] => 16/809092 [patent_app_country] => US [patent_app_date] => 2020-03-04 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 2 [patent_figures_cnt] => 2 [patent_no_of_words] => 5167 [patent_no_of_claims] => 30 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 192 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 16809092 [rel_patent_id] =>[rel_patent_doc_number] =>)
16/809092
Thrust efficient turbofan engine Mar 3, 2020 Issued
Array ( [id] => 17673761 [patent_doc_number] => 20220186928 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2022-06-16 [patent_title] => TUBULAR COMBUSTION CHAMBER SYSTEM AND GAS TURBINE UNIT HAVING A TUBULAR COMBUSTION CHAMBER SYSTEM OF THIS TYPE [patent_app_type] => utility [patent_app_number] => 17/440354 [patent_app_country] => US [patent_app_date] => 2020-03-03 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 0 [patent_figures_cnt] => 0 [patent_no_of_words] => 2337 [patent_no_of_claims] => 0 [patent_no_of_ind_claims] => -10 [patent_words_short_claim] => 81 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 17440354 [rel_patent_id] =>[rel_patent_doc_number] =>)
17/440354
Tubular combustion chamber system and gas turbine unit having a tubular combustion chamber system of this type Mar 2, 2020 Issued
Array ( [id] => 17468159 [patent_doc_number] => 11274631 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2022-03-15 [patent_title] => Methodology for minimizing aerodynamic buzz in an exhaust nozzle [patent_app_type] => utility [patent_app_number] => 16/803517 [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] => 8562 [patent_no_of_claims] => 19 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 184 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 16803517 [rel_patent_id] =>[rel_patent_doc_number] =>)
16/803517
Methodology for minimizing aerodynamic buzz in an exhaust nozzle Feb 26, 2020 Issued
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