
Harold Joyce
Examiner (ID: 10744)
| Most Active Art Unit | 3404 |
| Art Unit(s) | 3502, 3749, 3744, 2899, 3404 |
| Total Applications | 2782 |
| Issued Applications | 2512 |
| Pending Applications | 61 |
| Abandoned Applications | 209 |
Applications
| Application number | Title of the application | Filing Date | Status |
|---|---|---|---|
Array
(
[id] => 15728083
[patent_doc_number] => 10612468
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2020-04-07
[patent_title] => Gas turbine engine with thermoelectric intercooler
[patent_app_type] => utility
[patent_app_number] => 15/424164
[patent_app_country] => US
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Array
(
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[patent_doc_number] => 11181041
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[patent_kind] => B2
[patent_issue_date] => 2021-11-23
[patent_title] => Heat recovery steam generator with electrical heater system and method
[patent_app_type] => utility
[patent_app_number] => 15/423511
[patent_app_country] => US
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Array
(
[id] => 13329975
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[patent_kind] => A1
[patent_issue_date] => 2018-08-02
[patent_title] => GAS TURBINE ENGINE ARCHITECTURE WITH SPLIT COMPRESSOR SYSTEM
[patent_app_type] => utility
[patent_app_number] => 15/419160
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Array
(
[id] => 13329979
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[patent_issue_date] => 2018-08-02
[patent_title] => RADIAL VARIABLE INLET GUIDE VANE FOR AXIAL OR AXI-CENTRIFUGAL COMPRESSORS
[patent_app_type] => utility
[patent_app_number] => 15/417937
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Array
(
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[patent_title] => 'REVERSE FLOW GAS TURBINE ENGINE WITH OFFSET RGB'
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Array
(
[id] => 12840094
[patent_doc_number] => 20180171871
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[patent_kind] => A1
[patent_issue_date] => 2018-06-21
[patent_title] => Surface Cooler with Flow Recirculation
[patent_app_type] => utility
[patent_app_number] => 15/380205
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[patent_app_date] => 2016-12-15
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Array
(
[id] => 15979907
[patent_doc_number] => 10670270
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[patent_kind] => B2
[patent_issue_date] => 2020-06-02
[patent_title] => Gas turbine combustion chamber with wall contouring
[patent_app_type] => utility
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Array
(
[id] => 12815362
[patent_doc_number] => 20180163624
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[patent_title] => SYSTEMS AND METHODS FOR GAS TURBINE COMPRESSOR CLEANING
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Array
(
[id] => 12730873
[patent_doc_number] => 20180135458
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[patent_kind] => A1
[patent_issue_date] => 2018-05-17
[patent_title] => GAS TURBINE ENGINE COMPONENT WITH DEGRADATION COOLING SCHEME
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[rel_patent_id] =>[rel_patent_doc_number] =>) 15/353855 | Gas turbine engine component with degradation cooling scheme | Nov 16, 2016 | Issued |
Array
(
[id] => 15072267
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[patent_issue_date] => 2019-11-05
[patent_title] => Reverse flow multi-spool gas turbine engine with aft-end accessory gearbox drivingly connected to both high pressure spool and low pressure spool
[patent_app_type] => utility
[patent_app_number] => 15/351818
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[rel_patent_id] =>[rel_patent_doc_number] =>) 15/351818 | Reverse flow multi-spool gas turbine engine with aft-end accessory gearbox drivingly connected to both high pressure spool and low pressure spool | Nov 14, 2016 | Issued |
Array
(
[id] => 12683359
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[patent_issue_date] => 2018-05-03
[patent_title] => GAS TURBINE ENGINE WITH BLEED SLOTS AND METHOD OF FORMING
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Array
(
[id] => 13538097
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[patent_title] => COMBUSTION CYLINDER, GAS TURBINE COMBUSTOR, AND GAS TURBINE
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[rel_patent_id] =>[rel_patent_doc_number] =>) 15/769193 | Combustion cylinder, gas turbine combustor, and gas turbine | Oct 27, 2016 | Issued |
Array
(
[id] => 16832988
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[patent_title] => Aerodynamic injection system for aircraft turbine engine, having improved air/fuel mixing
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Array
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Array
(
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Array
(
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Array
(
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Array
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