
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] => 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 |