
Rachel A. Voorhies
Examiner (ID: 6186, Phone: (571)270-3756 , Office: P/2923 )
| Most Active Art Unit | 2923 |
| Art Unit(s) | 2953, 2923 |
| Total Applications | 1493 |
| Issued Applications | 1458 |
| Pending Applications | 10 |
| Abandoned Applications | 24 |
Applications
| Application number | Title of the application | Filing Date | Status |
|---|---|---|---|
Array
(
[id] => 14059305
[patent_doc_number] => 10233939
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2019-03-19
[patent_title] => Aviation turbine engine fan assembly including a fitted platform
[patent_app_type] => utility
[patent_app_number] => 15/205265
[patent_app_country] => US
[patent_app_date] => 2016-07-08
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Array
(
[id] => 13315803
[patent_doc_number] => 20180209438
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2018-07-26
[patent_title] => COMPACT AXIAL FAN
[patent_app_type] => utility
[patent_app_number] => 15/743067
[patent_app_country] => US
[patent_app_date] => 2016-07-08
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Array
(
[id] => 17998333
[patent_doc_number] => 11499432
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[patent_kind] => B2
[patent_issue_date] => 2022-11-15
[patent_title] => Method for altering the law of twist of the aerodynamic surface of a gas turbine engine fan blade
[patent_app_type] => utility
[patent_app_number] => 15/741374
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[patent_app_date] => 2016-07-01
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Array
(
[id] => 12119607
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[patent_issue_date] => 2018-01-04
[patent_title] => 'COOLING SYSTEM FOR STREAMLINED AIRFLOW'
[patent_app_type] => utility
[patent_app_number] => 15/197507
[patent_app_country] => US
[patent_app_date] => 2016-06-29
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[rel_patent_id] =>[rel_patent_doc_number] =>) 15/197507 | Cooling system for streamlined airflow | Jun 28, 2016 | Issued |
Array
(
[id] => 15817675
[patent_doc_number] => 10634006
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2020-04-28
[patent_title] => Guide vane of a gas turbine engine, in particular of an aircraft engine
[patent_app_type] => utility
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[rel_patent_id] =>[rel_patent_doc_number] =>) 15/194797 | Guide vane of a gas turbine engine, in particular of an aircraft engine | Jun 27, 2016 | Issued |
Array
(
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[patent_title] => 'TURBINE'
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Array
(
[id] => 11351041
[patent_doc_number] => 20160369781
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[patent_issue_date] => 2016-12-22
[patent_title] => 'LIGHTNING PROTECTION SYSTEM FOR WIND TURBINE BLADES WITH AN EFFECTIVE INJECTION AREA TO CARBON FIBER LAMINATES AND A BALANCED LIGHTNING CURRENT AND VOLTAGE DISTRIBUTION BETWEEN DIFFERENT CONDUCTIVE PATHS'
[patent_app_type] => utility
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[rel_patent_id] =>[rel_patent_doc_number] =>) 15/173896 | Lightning protection system for wind turbine blades with an effective injection area to carbon fiber laminates and a balanced lightning current and voltage distribution between different conductive paths | Jun 5, 2016 | Issued |
Array
(
[id] => 11291284
[patent_doc_number] => 20160341216
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[patent_issue_date] => 2016-11-24
[patent_title] => 'Blade and Shroud with Socket for a Compressor of an Axial Turbomachine'
[patent_app_type] => utility
[patent_app_number] => 15/159160
[patent_app_country] => US
[patent_app_date] => 2016-05-19
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[rel_patent_id] =>[rel_patent_doc_number] =>) 15/159160 | Blade and shroud with socket for a compressor of an axial turbomachine | May 18, 2016 | Issued |
Array
(
[id] => 14598275
[patent_doc_number] => 10352326
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[patent_kind] => B2
[patent_issue_date] => 2019-07-16
[patent_title] => Assembly for an engine which can define a blade break-off test device
[patent_app_type] => utility
[patent_app_number] => 15/157187
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[rel_patent_id] =>[rel_patent_doc_number] =>) 15/157187 | Assembly for an engine which can define a blade break-off test device | May 16, 2016 | Issued |
Array
(
[id] => 12051877
[patent_doc_number] => 20170328221
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[patent_kind] => A1
[patent_issue_date] => 2017-11-16
[patent_title] => 'ENGINE COMPONENT WALL WITH A COOLING CIRCUIT'
[patent_app_type] => utility
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[patent_app_date] => 2016-05-12
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[rel_patent_id] =>[rel_patent_doc_number] =>) 15/152887 | Engine component wall with a cooling circuit | May 11, 2016 | Issued |
Array
(
[id] => 12793189
[patent_doc_number] => 20180156232
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2018-06-07
[patent_title] => COMPOSITE BLADE, COMPRISING A LEADING-EDGE REINFORCEMENT MADE OF ANOTHER MATERIAL
[patent_app_type] => utility
[patent_app_number] => 15/570003
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[rel_patent_id] =>[rel_patent_doc_number] =>) 15/570003 | Composite blade, comprising a leading-edge reinforcement made of another material | Apr 27, 2016 | Issued |
Array
(
[id] => 12233673
[patent_doc_number] => 20180066536
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[patent_title] => 'COMPRESSOR STAGE'
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[rel_patent_id] =>[rel_patent_doc_number] =>) 15/561192 | COMPRESSOR STAGE | Mar 24, 2016 | Abandoned |
Array
(
[id] => 12240521
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[patent_issue_date] => 2018-03-15
[patent_title] => 'AIRCRAFT TURBINE ENGINE WITH PLANETARY OR EPICYCLIC GEAR TRAIN'
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[rel_patent_id] =>[rel_patent_doc_number] =>) 15/560464 | Aircraft turbine engine with planetary or epicyclic gear train | Mar 21, 2016 | Issued |
Array
(
[id] => 11084772
[patent_doc_number] => 20160281736
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2016-09-29
[patent_title] => 'MOVEABLE INLET GUIDE VANES'
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[rel_patent_id] =>[rel_patent_doc_number] =>) 15/075537 | MOVEABLE INLET GUIDE VANES | Mar 20, 2016 | Abandoned |
Array
(
[id] => 10987985
[patent_doc_number] => 20160184930
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[patent_kind] => A1
[patent_issue_date] => 2016-06-30
[patent_title] => 'METHOD OF WELDING SHAFT AND WHEEL IN TURBINE SHAFT, TURBINE SHAFT, AND WELDING DEVICE'
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[rel_patent_id] =>[rel_patent_doc_number] =>) 15/062492 | Method of welding shaft and wheel in turbine shaft, turbine shaft, and welding device | Mar 6, 2016 | Issued |
Array
(
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[patent_title] => 'Modulated Hybrid Variable Area Turbine Nozzle for Gas Turbine Engine'
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Array
(
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[rel_patent_id] =>[rel_patent_doc_number] =>) 16/078819 | Cooling device and compressor system | Feb 25, 2016 | Issued |
Array
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Array
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[rel_patent_id] =>[rel_patent_doc_number] =>) 15/051392 | Submersible pump thrust surface arrangement | Feb 22, 2016 | Issued |
Array
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[rel_patent_id] =>[rel_patent_doc_number] =>) 15/051106 | Rotary assembly for an aviation turbine engine, the assembly comprising a separate fan blade platform mounted on a fan disk | Feb 22, 2016 | Issued |