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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] => 18764635 [patent_doc_number] => 11815024 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2023-11-14 [patent_title] => Thermal management system [patent_app_type] => utility [patent_app_number] => 17/375489 [patent_app_country] => US [patent_app_date] => 2021-07-14 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 4 [patent_figures_cnt] => 6 [patent_no_of_words] => 8656 [patent_no_of_claims] => 19 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 186 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 17375489 [rel_patent_id] =>[rel_patent_doc_number] =>)
17/375489
Thermal management system Jul 13, 2021 Issued
Array ( [id] => 19028052 [patent_doc_number] => 11927402 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2024-03-12 [patent_title] => Heat transfer device with nested layers of helical fluid channels [patent_app_type] => utility [patent_app_number] => 17/374860 [patent_app_country] => US [patent_app_date] => 2021-07-13 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 15 [patent_figures_cnt] => 23 [patent_no_of_words] => 14366 [patent_no_of_claims] => 20 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 174 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 17374860 [rel_patent_id] =>[rel_patent_doc_number] =>)
17/374860
Heat transfer device with nested layers of helical fluid channels Jul 12, 2021 Issued
Array ( [id] => 17414767 [patent_doc_number] => 20220049671 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2022-02-17 [patent_title] => PROPULSION SYSTEM ARRANGEMENT FOR TURBOFAN GAS TURBINE ENGINE [patent_app_type] => utility [patent_app_number] => 17/371672 [patent_app_country] => US [patent_app_date] => 2021-07-09 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 0 [patent_figures_cnt] => 0 [patent_no_of_words] => 10939 [patent_no_of_claims] => 0 [patent_no_of_ind_claims] => -29 [patent_words_short_claim] => 298 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 17371672 [rel_patent_id] =>[rel_patent_doc_number] =>)
17/371672
Propulsion system arrangement for turbofan gas turbine engine Jul 8, 2021 Issued
Array ( [id] => 17259637 [patent_doc_number] => 20210372622 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2021-12-02 [patent_title] => MAIN MIXER IN AN AXIAL STAGED COMBUSTOR FOR A GAS TURBINE ENGINE [patent_app_type] => utility [patent_app_number] => 17/370154 [patent_app_country] => US [patent_app_date] => 2021-07-08 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 0 [patent_figures_cnt] => 0 [patent_no_of_words] => 5489 [patent_no_of_claims] => 0 [patent_no_of_ind_claims] => -17 [patent_words_short_claim] => 50 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 17370154 [rel_patent_id] =>[rel_patent_doc_number] =>)
17/370154
Main mixer in an axial staged combustor for a gas turbine engine Jul 7, 2021 Issued
Array ( [id] => 18605247 [patent_doc_number] => 11746703 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2023-09-05 [patent_title] => Connecting gas turbine engine annular members [patent_app_type] => utility [patent_app_number] => 17/369677 [patent_app_country] => US [patent_app_date] => 2021-07-07 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 10 [patent_figures_cnt] => 13 [patent_no_of_words] => 4350 [patent_no_of_claims] => 20 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 84 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 17369677 [rel_patent_id] =>[rel_patent_doc_number] =>)
17/369677
Connecting gas turbine engine annular members Jul 6, 2021 Issued
Array ( [id] => 18045660 [patent_doc_number] => 11519604 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2022-12-06 [patent_title] => Plug resistant effusion holes for gas turbine engine [patent_app_type] => utility [patent_app_number] => 17/305202 [patent_app_country] => US [patent_app_date] => 2021-07-01 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 8 [patent_figures_cnt] => 8 [patent_no_of_words] => 10300 [patent_no_of_claims] => 20 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 210 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 17305202 [rel_patent_id] =>[rel_patent_doc_number] =>)
17/305202
Plug resistant effusion holes for gas turbine engine Jun 30, 2021 Issued
Array ( [id] => 18103249 [patent_doc_number] => 11543130 [patent_country] => US [patent_kind] => B1 [patent_issue_date] => 2023-01-03 [patent_title] => Passive secondary air assist nozzles [patent_app_type] => utility [patent_app_number] => 17/360207 [patent_app_country] => US [patent_app_date] => 2021-06-28 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 5 [patent_figures_cnt] => 5 [patent_no_of_words] => 2721 [patent_no_of_claims] => 13 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 154 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 17360207 [rel_patent_id] =>[rel_patent_doc_number] =>)
17/360207
Passive secondary air assist nozzles Jun 27, 2021 Issued
Array ( [id] => 18052025 [patent_doc_number] => 11525399 [patent_country] => US [patent_kind] => B1 [patent_issue_date] => 2022-12-13 [patent_title] => Oil system with flow restrictor [patent_app_type] => utility [patent_app_number] => 17/350950 [patent_app_country] => US [patent_app_date] => 2021-06-17 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 6 [patent_figures_cnt] => 7 [patent_no_of_words] => 5150 [patent_no_of_claims] => 18 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 173 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 17350950 [rel_patent_id] =>[rel_patent_doc_number] =>)
17/350950
Oil system with flow restrictor Jun 16, 2021 Issued
Array ( [id] => 17635524 [patent_doc_number] => 11346242 [patent_country] => US [patent_kind] => B1 [patent_issue_date] => 2022-05-31 [patent_title] => Retaining ejected gas turbine blades [patent_app_type] => utility [patent_app_number] => 17/344560 [patent_app_country] => US [patent_app_date] => 2021-06-10 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 8 [patent_figures_cnt] => 8 [patent_no_of_words] => 4225 [patent_no_of_claims] => 21 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 100 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 17344560 [rel_patent_id] =>[rel_patent_doc_number] =>)
17/344560
Retaining ejected gas turbine blades Jun 9, 2021 Issued
Array ( [id] => 18021682 [patent_doc_number] => 20220373181 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2022-11-24 [patent_title] => ACTIVE BOUNDARY LAYER CONTROL IN DIFFUSER [patent_app_type] => utility [patent_app_number] => 17/325938 [patent_app_country] => US [patent_app_date] => 2021-05-20 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 0 [patent_figures_cnt] => 0 [patent_no_of_words] => 7597 [patent_no_of_claims] => 0 [patent_no_of_ind_claims] => -17 [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] => 17325938 [rel_patent_id] =>[rel_patent_doc_number] =>)
17/325938
Active boundary layer control in diffuser May 19, 2021 Issued
Array ( [id] => 18947905 [patent_doc_number] => 11891185 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2024-02-06 [patent_title] => Nacelle for a propulsion assembly with a very high bypass ratio, comprising a removable and structural front internal structure [patent_app_type] => utility [patent_app_number] => 17/999180 [patent_app_country] => US [patent_app_date] => 2021-05-18 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 11 [patent_figures_cnt] => 22 [patent_no_of_words] => 7141 [patent_no_of_claims] => 11 [patent_no_of_ind_claims] => 1 [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] => 17999180 [rel_patent_id] =>[rel_patent_doc_number] =>)
17/999180
Nacelle for a propulsion assembly with a very high bypass ratio, comprising a removable and structural front internal structure May 17, 2021 Issued
Array ( [id] => 19339672 [patent_doc_number] => 12049853 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2024-07-30 [patent_title] => Thrust reverser for an aircraft bypass turbojet engine nacelle [patent_app_type] => utility [patent_app_number] => 17/999106 [patent_app_country] => US [patent_app_date] => 2021-05-17 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 7 [patent_figures_cnt] => 12 [patent_no_of_words] => 3935 [patent_no_of_claims] => 12 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 247 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 17999106 [rel_patent_id] =>[rel_patent_doc_number] =>)
17/999106
Thrust reverser for an aircraft bypass turbojet engine nacelle May 16, 2021 Issued
Array ( [id] => 17357513 [patent_doc_number] => 20220018309 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2022-01-20 [patent_title] => PASSIVELY ACTUATED VARIABLE AREA NOZZLE FOR AN AIRCRAFT PROPULSION SYSTEM [patent_app_type] => utility [patent_app_number] => 17/317380 [patent_app_country] => US [patent_app_date] => 2021-05-11 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 0 [patent_figures_cnt] => 0 [patent_no_of_words] => 5598 [patent_no_of_claims] => 0 [patent_no_of_ind_claims] => -17 [patent_words_short_claim] => 55 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 17317380 [rel_patent_id] =>[rel_patent_doc_number] =>)
17/317380
PASSIVELY ACTUATED VARIABLE AREA NOZZLE FOR AN AIRCRAFT PROPULSION SYSTEM May 10, 2021 Abandoned
Array ( [id] => 18436905 [patent_doc_number] => 20230184199 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2023-06-15 [patent_title] => STRUCTURE FOR ASSEMBLING A PIECE COMPRISING A FIRST METAL PART AND A SECOND PART MADE OF AN ORGANIC MATRIX COMPOSITE MATERIAL [patent_app_type] => utility [patent_app_number] => 17/999343 [patent_app_country] => US [patent_app_date] => 2021-05-11 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 0 [patent_figures_cnt] => 0 [patent_no_of_words] => 2916 [patent_no_of_claims] => 0 [patent_no_of_ind_claims] => -9 [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] => 17999343 [rel_patent_id] =>[rel_patent_doc_number] =>)
17/999343
Structure for assembling a piece comprising a first metal part and a second part made of an organic matrix composite material May 10, 2021 Issued
Array ( [id] => 18029464 [patent_doc_number] => 11512641 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2022-11-29 [patent_title] => Upper axial retention for a cascade-type thrust reverser with sliding vanes of D-shaped structure [patent_app_type] => utility [patent_app_number] => 17/238602 [patent_app_country] => US [patent_app_date] => 2021-04-23 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 4 [patent_figures_cnt] => 10 [patent_no_of_words] => 5504 [patent_no_of_claims] => 11 [patent_no_of_ind_claims] => 3 [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] => 17238602 [rel_patent_id] =>[rel_patent_doc_number] =>)
17/238602
Upper axial retention for a cascade-type thrust reverser with sliding vanes of D-shaped structure Apr 22, 2021 Issued
Array ( [id] => 17954010 [patent_doc_number] => 11480108 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2022-10-25 [patent_title] => Turbine section of high bypass turbofan [patent_app_type] => utility [patent_app_number] => 17/230271 [patent_app_country] => US [patent_app_date] => 2021-04-14 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 4 [patent_figures_cnt] => 5 [patent_no_of_words] => 7151 [patent_no_of_claims] => 30 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 393 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 17230271 [rel_patent_id] =>[rel_patent_doc_number] =>)
17/230271
Turbine section of high bypass turbofan Apr 13, 2021 Issued
Array ( [id] => 17968793 [patent_doc_number] => 11486311 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2022-11-01 [patent_title] => Turbine section of high bypass turbofan [patent_app_type] => utility [patent_app_number] => 17/230326 [patent_app_country] => US [patent_app_date] => 2021-04-14 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 7 [patent_figures_cnt] => 12 [patent_no_of_words] => 7324 [patent_no_of_claims] => 30 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 309 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 17230326 [rel_patent_id] =>[rel_patent_doc_number] =>)
17/230326
Turbine section of high bypass turbofan Apr 13, 2021 Issued
Array ( [id] => 19312373 [patent_doc_number] => 12038179 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2024-07-16 [patent_title] => Cooling for detonation engines [patent_app_type] => utility [patent_app_number] => 17/226444 [patent_app_country] => US [patent_app_date] => 2021-04-09 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 5 [patent_figures_cnt] => 13 [patent_no_of_words] => 5277 [patent_no_of_claims] => 17 [patent_no_of_ind_claims] => 4 [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] => 17226444 [rel_patent_id] =>[rel_patent_doc_number] =>)
17/226444
Cooling for detonation engines Apr 8, 2021 Issued
Array ( [id] => 18325951 [patent_doc_number] => 20230124079 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2023-04-20 [patent_title] => ACOUSTICALLY OPTIMIZED DISCHARGE LINE GRID WITH CHANNELS [patent_app_type] => utility [patent_app_number] => 17/995638 [patent_app_country] => US [patent_app_date] => 2021-04-06 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 0 [patent_figures_cnt] => 0 [patent_no_of_words] => 3026 [patent_no_of_claims] => 0 [patent_no_of_ind_claims] => -11 [patent_words_short_claim] => 118 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 17995638 [rel_patent_id] =>[rel_patent_doc_number] =>)
17/995638
Acoustically optimized discharge line grid with channels Apr 5, 2021 Issued
Array ( [id] => 17913957 [patent_doc_number] => 20220316352 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2022-10-06 [patent_title] => FLOW DIVERTER FOR MID-TURBINE FRAME COOLING AIR DELIVERY [patent_app_type] => utility [patent_app_number] => 17/218352 [patent_app_country] => US [patent_app_date] => 2021-03-31 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 0 [patent_figures_cnt] => 0 [patent_no_of_words] => 5150 [patent_no_of_claims] => 0 [patent_no_of_ind_claims] => -18 [patent_words_short_claim] => 172 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 17218352 [rel_patent_id] =>[rel_patent_doc_number] =>)
17/218352
FLOW DIVERTER FOR MID-TURBINE FRAME COOLING AIR DELIVERY Mar 30, 2021 Abandoned
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