
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] => 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 |