
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] => 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
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[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
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[rel_patent_id] =>[rel_patent_doc_number] =>) 16/678317 | Multi-directional gearbox deflection limiter for a gas turbine engine | Nov 7, 2019 | Issued |
Array
(
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[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
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[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
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[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
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[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
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[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
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[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
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[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
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[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
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[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
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[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
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[patent_kind] => A1
[patent_issue_date] => 2019-11-28
[patent_title] => COMBUSTOR QUENCH APERTURE COOLING
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[rel_patent_id] =>[rel_patent_doc_number] =>) 16/538207 | Combustor quench aperture cooling | Aug 11, 2019 | Issued |
Array
(
[id] => 16598804
[patent_doc_number] => 20210025335
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[patent_kind] => A1
[patent_issue_date] => 2021-01-28
[patent_title] => LOW POWER HYBRID TURBOFAN DRAG REDUCTION
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[rel_patent_id] =>[rel_patent_doc_number] =>) 16/521633 | LOW POWER HYBRID TURBOFAN DRAG REDUCTION | Jul 24, 2019 | Abandoned |
Array
(
[id] => 17179124
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[patent_issue_date] => 2021-10-26
[patent_title] => Multi-point injection mini mixing fuel nozzle assembly
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[rel_patent_id] =>[rel_patent_doc_number] =>) 16/516586 | Multi-point injection mini mixing fuel nozzle assembly | Jul 18, 2019 | Issued |
Array
(
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Array
(
[id] => 17163475
[patent_doc_number] => 11149564
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[patent_issue_date] => 2021-10-19
[patent_title] => Nacelle thrust reverser compression rod supporting system
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[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
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[patent_issue_date] => 2020-11-26
[patent_title] => INLET BULKHEAD WITH VENTILATION GROOVE
[patent_app_type] => utility
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[rel_patent_id] =>[rel_patent_doc_number] =>) 16/422572 | Inlet bulkhead with ventilation groove | May 23, 2019 | Issued |
Array
(
[id] => 16453298
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[patent_title] => MONOLITHIC COMBUSTOR FOR ATTRITIABLE ENGINE APPLICATIONS
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[rel_patent_id] =>[rel_patent_doc_number] =>) 16/415327 | Monolithic combustor for attritiable engine applications | May 16, 2019 | Issued |
Array
(
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Array
(
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[patent_title] => ACOUSTIC LINER WITH OBLIQUELY ANGLED SLOTS
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[rel_patent_id] =>[rel_patent_doc_number] =>) 16/411728 | Acoustic liner with obliquely angled slots | May 13, 2019 | Issued |