
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] => 11664032
[patent_doc_number] => 20170152751
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[patent_kind] => A1
[patent_issue_date] => 2017-06-01
[patent_title] => 'COOLING PASSAGES FOR A GAS PATH COMPONENT OF A GAS TURBINE ENGINE'
[patent_app_type] => utility
[patent_app_number] => 14/955167
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[rel_patent_id] =>[rel_patent_doc_number] =>) 14/955167 | Cooling passages for a gas path component of a gas turbine engine | Nov 30, 2015 | Issued |
Array
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[patent_kind] => B2
[patent_issue_date] => 2018-10-02
[patent_title] => Pressure damping device for fuel manifold
[patent_app_type] => utility
[patent_app_number] => 14/954658
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[rel_patent_id] =>[rel_patent_doc_number] =>) 14/954658 | Pressure damping device for fuel manifold | Nov 29, 2015 | Issued |
Array
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[patent_issue_date] => 2016-06-02
[patent_title] => 'FRAME SEGMENT FOR A COMBUSTOR TURBINE INTERFACE'
[patent_app_type] => utility
[patent_app_number] => 14/948846
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[patent_app_date] => 2015-11-23
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[rel_patent_id] =>[rel_patent_doc_number] =>) 14/948846 | Frame segment for a combustor turbine interface | Nov 22, 2015 | Issued |
Array
(
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[patent_doc_number] => 20180313535
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[patent_issue_date] => 2018-11-01
[patent_title] => COMBUSTION SYSTEM WITH INJECTOR ASSEMBLY INCLUDING AERODYNAMICALLY-SHAPED BODY AND/OR EJECTION ORIFICES
[patent_app_type] => utility
[patent_app_number] => 15/771778
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[rel_patent_id] =>[rel_patent_doc_number] =>) 15/771778 | COMBUSTION SYSTEM WITH INJECTOR ASSEMBLY INCLUDING AERODYNAMICALLY-SHAPED BODY AND/OR EJECTION ORIFICES | Oct 27, 2015 | Abandoned |
Array
(
[id] => 11569196
[patent_doc_number] => 20170107840
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[patent_issue_date] => 2017-04-20
[patent_title] => 'SHROUDS AND METHODS FOR FORMING TURBINE COMPONENTS'
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Array
(
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[patent_doc_number] => 20160024934
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[patent_issue_date] => 2016-01-28
[patent_title] => 'ALUMINUM FAN BLADE CONSTRUCTION WITH WELDED COVER'
[patent_app_type] => utility
[patent_app_number] => 14/877254
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[rel_patent_id] =>[rel_patent_doc_number] =>) 14/877254 | Aluminum fan blade construction with welded cover | Oct 6, 2015 | Issued |
Array
(
[id] => 12001386
[patent_doc_number] => 20170305541
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[patent_kind] => A1
[patent_issue_date] => 2017-10-26
[patent_title] => 'ARCHITECTURE FOR A PROPULSION SYSTEM OF A HELICOPTER INCLUDING A HYBRID TURBOSHAFT ENGINE AND A SYSTEM FOR REACTIVATING SAID HYBRID TURBOSHAFT ENGINE'
[patent_app_type] => utility
[patent_app_number] => 15/517924
[patent_app_country] => US
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[rel_patent_id] =>[rel_patent_doc_number] =>) 15/517924 | Architecture for a propulsion system of a helicopter including a hybrid turboshaft engine and a system for reactivating said hybrid turboshaft engine | Oct 5, 2015 | Issued |
Array
(
[id] => 15542107
[patent_doc_number] => 10570823
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2020-02-25
[patent_title] => Heat recovery unit and power plant
[patent_app_type] => utility
[patent_app_number] => 15/513171
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[rel_patent_id] =>[rel_patent_doc_number] =>) 15/513171 | Heat recovery unit and power plant | Sep 23, 2015 | Issued |
Array
(
[id] => 15195045
[patent_doc_number] => 10495004
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[patent_issue_date] => 2019-12-03
[patent_title] => Multi-directional gearbox deflection limiter for a gas turbine engine
[patent_app_type] => utility
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[rel_patent_id] =>[rel_patent_doc_number] =>) 14/857164 | Multi-directional gearbox deflection limiter for a gas turbine engine | Sep 16, 2015 | Issued |
Array
(
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[patent_doc_number] => 10113559
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[patent_issue_date] => 2018-10-30
[patent_title] => Gas turbine engine impact liner
[patent_app_type] => utility
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[rel_patent_id] =>[rel_patent_doc_number] =>) 14/850438 | Gas turbine engine impact liner | Sep 9, 2015 | Issued |
Array
(
[id] => 13888879
[patent_doc_number] => 10196986
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[patent_kind] => B2
[patent_issue_date] => 2019-02-05
[patent_title] => Hydrodynamic seals in bearing compartments of gas turbine engines
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[rel_patent_id] =>[rel_patent_doc_number] =>) 14/845625 | Hydrodynamic seals in bearing compartments of gas turbine engines | Sep 3, 2015 | Issued |
Array
(
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[patent_title] => 'INJECTORS FOR MULTIPOINT INJECTION'
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Array
(
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[patent_title] => Gas turbine combustor
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Array
(
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[patent_doc_number] => 10260419
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[patent_title] => Cooling system
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Array
(
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[patent_title] => 'TURBINE SECTION OF HIGH BYPASS TURBOFAN'
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Array
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Array
(
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[patent_title] => 'LINER ELEMENT FOR A COMBUSTOR'
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Array
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Array
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