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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] => 16254230 [patent_doc_number] => 20200263604 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2020-08-20 [patent_title] => GAS TURBINE ENGINE BUFFER SYSTEM [patent_app_type] => utility [patent_app_number] => 16/677721 [patent_app_country] => US [patent_app_date] => 2019-11-08 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 0 [patent_figures_cnt] => 0 [patent_no_of_words] => 5530 [patent_no_of_claims] => 0 [patent_no_of_ind_claims] => -17 [patent_words_short_claim] => 166 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 16677721 [rel_patent_id] =>[rel_patent_doc_number] =>)
16/677721
Gas turbine engine buffer system Nov 7, 2019 Issued
Array ( [id] => 17351287 [patent_doc_number] => 11225914 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2022-01-18 [patent_title] => Multi-directional gearbox deflection limiter for a gas turbine engine [patent_app_type] => utility [patent_app_number] => 16/678317 [patent_app_country] => US [patent_app_date] => 2019-11-08 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 6 [patent_figures_cnt] => 7 [patent_no_of_words] => 5789 [patent_no_of_claims] => 20 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 253 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 16678317 [rel_patent_id] =>[rel_patent_doc_number] =>)
16/678317
Multi-directional gearbox deflection limiter for a gas turbine engine Nov 7, 2019 Issued
Array ( [id] => 17135390 [patent_doc_number] => 11136938 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2021-10-05 [patent_title] => Bypass turbofan engine comprising a nacelle equipped with a translationally-mobile thrust-reversal system and with a fan case equipped with supports [patent_app_type] => utility [patent_app_number] => 16/656632 [patent_app_country] => US [patent_app_date] => 2019-10-18 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 3 [patent_figures_cnt] => 6 [patent_no_of_words] => 3336 [patent_no_of_claims] => 4 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 362 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 16656632 [rel_patent_id] =>[rel_patent_doc_number] =>)
16/656632
Bypass turbofan engine comprising a nacelle equipped with a translationally-mobile thrust-reversal system and with a fan case equipped with supports Oct 17, 2019 Issued
Array ( [id] => 16778798 [patent_doc_number] => 20210115876 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2021-04-22 [patent_title] => NOZZLE-TO-ENGINE MOUNT REINFORCEMENT THROUGH WHICH MOUNTING FASTENERS ARE VISIBLE [patent_app_type] => utility [patent_app_number] => 16/654684 [patent_app_country] => US [patent_app_date] => 2019-10-16 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 0 [patent_figures_cnt] => 0 [patent_no_of_words] => 3327 [patent_no_of_claims] => 0 [patent_no_of_ind_claims] => -17 [patent_words_short_claim] => 69 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 16654684 [rel_patent_id] =>[rel_patent_doc_number] =>)
16/654684
Nozzle-to-engine mount reinforcement through which mounting fasteners are visible Oct 15, 2019 Issued
Array ( [id] => 15799417 [patent_doc_number] => 20200122851 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2020-04-23 [patent_title] => FORWARD PART OF AN AIRCRAFT PROPULSION UNIT NACELLE COMPRISING A MAIN PROPAGATION PATH FOR FORCES BETWEEN AN AIR INTAKE LIP AND A BACK SKIN OF AN ACOUSTIC PANEL [patent_app_type] => utility [patent_app_number] => 16/654119 [patent_app_country] => US [patent_app_date] => 2019-10-16 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 0 [patent_figures_cnt] => 0 [patent_no_of_words] => 4807 [patent_no_of_claims] => 0 [patent_no_of_ind_claims] => -10 [patent_words_short_claim] => 124 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 16654119 [rel_patent_id] =>[rel_patent_doc_number] =>)
16/654119
Forward part of an aircraft propulsion unit nacelle comprising a main propagation path for forces between an air intake lip and a back skin of an acoustic panel Oct 15, 2019 Issued
Array ( [id] => 17923388 [patent_doc_number] => 11466626 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2022-10-11 [patent_title] => Method for controlling a turbomachine comprising an electric motor [patent_app_type] => utility [patent_app_number] => 17/282370 [patent_app_country] => US [patent_app_date] => 2019-10-01 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 7 [patent_figures_cnt] => 9 [patent_no_of_words] => 6693 [patent_no_of_claims] => 9 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 288 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 17282370 [rel_patent_id] =>[rel_patent_doc_number] =>)
17/282370
Method for controlling a turbomachine comprising an electric motor Sep 30, 2019 Issued
Array ( [id] => 17307857 [patent_doc_number] => 11208955 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2021-12-28 [patent_title] => Reduced stress boss geometry for a gas turbine engine [patent_app_type] => utility [patent_app_number] => 16/574427 [patent_app_country] => US [patent_app_date] => 2019-09-18 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 6 [patent_figures_cnt] => 7 [patent_no_of_words] => 2232 [patent_no_of_claims] => 17 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 45 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 16574427 [rel_patent_id] =>[rel_patent_doc_number] =>)
16/574427
Reduced stress boss geometry for a gas turbine engine Sep 17, 2019 Issued
Array ( [id] => 15588917 [patent_doc_number] => 20200070993 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2020-03-05 [patent_title] => AIR INTAKE STRUCTURE OF AN AIRCRAFT NACELLE [patent_app_type] => utility [patent_app_number] => 16/560344 [patent_app_country] => US [patent_app_date] => 2019-09-04 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 0 [patent_figures_cnt] => 0 [patent_no_of_words] => 2322 [patent_no_of_claims] => 0 [patent_no_of_ind_claims] => -10 [patent_words_short_claim] => 134 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 16560344 [rel_patent_id] =>[rel_patent_doc_number] =>)
16/560344
Air intake structure of an aircraft nacelle Sep 3, 2019 Issued
Array ( [id] => 15867757 [patent_doc_number] => 20200141282 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2020-05-07 [patent_title] => NATURAL GAS COMBINED POWER GENERATION PROCESS WITH ZERO CARBON EMISSION [patent_app_type] => utility [patent_app_number] => 16/555152 [patent_app_country] => US [patent_app_date] => 2019-08-29 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 0 [patent_figures_cnt] => 0 [patent_no_of_words] => 4771 [patent_no_of_claims] => 0 [patent_no_of_ind_claims] => -10 [patent_words_short_claim] => 173 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 16555152 [rel_patent_id] =>[rel_patent_doc_number] =>)
16/555152
Natural gas combined power generation process with zero carbon emission Aug 28, 2019 Issued
Array ( [id] => 17120331 [patent_doc_number] => 11131457 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2021-09-28 [patent_title] => Combustor for gas turbine [patent_app_type] => utility [patent_app_number] => 16/552909 [patent_app_country] => US [patent_app_date] => 2019-08-27 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 32 [patent_figures_cnt] => 32 [patent_no_of_words] => 8023 [patent_no_of_claims] => 20 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 127 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 16552909 [rel_patent_id] =>[rel_patent_doc_number] =>)
16/552909
Combustor for gas turbine Aug 26, 2019 Issued
Array ( [id] => 17514495 [patent_doc_number] => 11293638 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2022-04-05 [patent_title] => Combustor heat shield and method of cooling same [patent_app_type] => utility [patent_app_number] => 16/549722 [patent_app_country] => US [patent_app_date] => 2019-08-23 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 10 [patent_figures_cnt] => 10 [patent_no_of_words] => 5485 [patent_no_of_claims] => 18 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 179 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 16549722 [rel_patent_id] =>[rel_patent_doc_number] =>)
16/549722
Combustor heat shield and method of cooling same Aug 22, 2019 Issued
Array ( [id] => 15180205 [patent_doc_number] => 20190360694 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2019-11-28 [patent_title] => COMBUSTOR QUENCH APERTURE COOLING [patent_app_type] => utility [patent_app_number] => 16/538207 [patent_app_country] => US [patent_app_date] => 2019-08-12 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 0 [patent_figures_cnt] => 0 [patent_no_of_words] => 6268 [patent_no_of_claims] => 0 [patent_no_of_ind_claims] => -17 [patent_words_short_claim] => 76 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 16538207 [rel_patent_id] =>[rel_patent_doc_number] =>)
16/538207
Combustor quench aperture cooling Aug 11, 2019 Issued
Array ( [id] => 16598804 [patent_doc_number] => 20210025335 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2021-01-28 [patent_title] => LOW POWER HYBRID TURBOFAN DRAG REDUCTION [patent_app_type] => utility [patent_app_number] => 16/521633 [patent_app_country] => US [patent_app_date] => 2019-07-25 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 0 [patent_figures_cnt] => 0 [patent_no_of_words] => 4040 [patent_no_of_claims] => 0 [patent_no_of_ind_claims] => -16 [patent_words_short_claim] => 54 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 16521633 [rel_patent_id] =>[rel_patent_doc_number] =>)
16/521633
LOW POWER HYBRID TURBOFAN DRAG REDUCTION Jul 24, 2019 Abandoned
Array ( [id] => 17179124 [patent_doc_number] => 11156361 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2021-10-26 [patent_title] => Multi-point injection mini mixing fuel nozzle assembly [patent_app_type] => utility [patent_app_number] => 16/516586 [patent_app_country] => US [patent_app_date] => 2019-07-19 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 9 [patent_figures_cnt] => 9 [patent_no_of_words] => 8402 [patent_no_of_claims] => 17 [patent_no_of_ind_claims] => 4 [patent_words_short_claim] => 113 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 16516586 [rel_patent_id] =>[rel_patent_doc_number] =>)
16/516586
Multi-point injection mini mixing fuel nozzle assembly Jul 18, 2019 Issued
Array ( [id] => 17330684 [patent_doc_number] => 11221141 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2022-01-11 [patent_title] => Assembly for a turbomachine [patent_app_type] => utility [patent_app_number] => 17/260719 [patent_app_country] => US [patent_app_date] => 2019-07-18 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 4 [patent_figures_cnt] => 4 [patent_no_of_words] => 2316 [patent_no_of_claims] => 8 [patent_no_of_ind_claims] => 1 [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] => 17260719 [rel_patent_id] =>[rel_patent_doc_number] =>)
17/260719
Assembly for a turbomachine Jul 17, 2019 Issued
Array ( [id] => 17163475 [patent_doc_number] => 11149564 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2021-10-19 [patent_title] => Nacelle thrust reverser compression rod supporting system [patent_app_type] => utility [patent_app_number] => 16/450799 [patent_app_country] => US [patent_app_date] => 2019-06-24 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 10 [patent_figures_cnt] => 10 [patent_no_of_words] => 4159 [patent_no_of_claims] => 20 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 36 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 16450799 [rel_patent_id] =>[rel_patent_doc_number] =>)
16/450799
Nacelle thrust reverser compression rod supporting system Jun 23, 2019 Issued
Array ( [id] => 16467862 [patent_doc_number] => 20200369399 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2020-11-26 [patent_title] => INLET BULKHEAD WITH VENTILATION GROOVE [patent_app_type] => utility [patent_app_number] => 16/422572 [patent_app_country] => US [patent_app_date] => 2019-05-24 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 0 [patent_figures_cnt] => 0 [patent_no_of_words] => 3850 [patent_no_of_claims] => 0 [patent_no_of_ind_claims] => -17 [patent_words_short_claim] => 35 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 16422572 [rel_patent_id] =>[rel_patent_doc_number] =>)
16/422572
Inlet bulkhead with ventilation groove May 23, 2019 Issued
Array ( [id] => 16453298 [patent_doc_number] => 20200362724 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2020-11-19 [patent_title] => MONOLITHIC COMBUSTOR FOR ATTRITIABLE ENGINE APPLICATIONS [patent_app_type] => utility [patent_app_number] => 16/415327 [patent_app_country] => US [patent_app_date] => 2019-05-17 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 0 [patent_figures_cnt] => 0 [patent_no_of_words] => 4359 [patent_no_of_claims] => 0 [patent_no_of_ind_claims] => -17 [patent_words_short_claim] => 92 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 16415327 [rel_patent_id] =>[rel_patent_doc_number] =>)
16/415327
Monolithic combustor for attritiable engine applications May 16, 2019 Issued
Array ( [id] => 17491200 [patent_doc_number] => 11280494 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2022-03-22 [patent_title] => Assembly for a turbomachine combustion chamber [patent_app_type] => utility [patent_app_number] => 16/412958 [patent_app_country] => US [patent_app_date] => 2019-05-15 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 5 [patent_figures_cnt] => 10 [patent_no_of_words] => 3450 [patent_no_of_claims] => 12 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 185 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 16412958 [rel_patent_id] =>[rel_patent_doc_number] =>)
16/412958
Assembly for a turbomachine combustion chamber May 14, 2019 Issued
Array ( [id] => 16422587 [patent_doc_number] => 20200347785 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2020-11-05 [patent_title] => ACOUSTIC LINER WITH OBLIQUELY ANGLED SLOTS [patent_app_type] => utility [patent_app_number] => 16/411728 [patent_app_country] => US [patent_app_date] => 2019-05-14 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 0 [patent_figures_cnt] => 0 [patent_no_of_words] => 4480 [patent_no_of_claims] => 0 [patent_no_of_ind_claims] => -22 [patent_words_short_claim] => 49 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 16411728 [rel_patent_id] =>[rel_patent_doc_number] =>)
16/411728
Acoustic liner with obliquely angled slots May 13, 2019 Issued
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