
Benjamin S. Fields
Examiner (ID: 4456, Phone: (571)272-9734 , Office: P/3623 )
| Most Active Art Unit | 3684 |
| Art Unit(s) | 3624, 3623, 3692, 3684 |
| Total Applications | 372 |
| Issued Applications | 203 |
| Pending Applications | 0 |
| Abandoned Applications | 170 |
Applications
| Application number | Title of the application | Filing Date | Status |
|---|---|---|---|
Array
(
[id] => 12625833
[patent_doc_number] => 20180100441
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2018-04-12
[patent_title] => BLEED VALVE ASSEMBLY FOR A GAS TURBINE ENGINE
[patent_app_type] => utility
[patent_app_number] => 15/287782
[patent_app_country] => US
[patent_app_date] => 2016-10-07
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[rel_patent_id] =>[rel_patent_doc_number] =>) 15/287782 | Bleed valve assembly for a gas turbine engine | Oct 6, 2016 | Issued |
Array
(
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[patent_doc_number] => 20170227226
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[patent_kind] => A1
[patent_issue_date] => 2017-08-10
[patent_title] => 'LIGHT WEIGHT SWIRLER FOR GAS TURBINE ENGINE COMBUSTOR AND A METHOD FOR LIGHTENING A SWIRLER FOR A GAS TURBINE ENGINE'
[patent_app_type] => utility
[patent_app_number] => 15/267468
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[patent_app_date] => 2016-09-16
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[rel_patent_id] =>[rel_patent_doc_number] =>) 15/267468 | Light weight swirler for gas turbine engine combustor and a method for lightening a swirler for a gas turbine engine | Sep 15, 2016 | Issued |
Array
(
[id] => 11291218
[patent_doc_number] => 20160341149
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2016-11-24
[patent_title] => 'FULL RING SLIDING NACELLE WITH THRUST REVERSER'
[patent_app_type] => utility
[patent_app_number] => 15/230086
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[patent_app_date] => 2016-08-05
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[rel_patent_id] =>[rel_patent_doc_number] =>) 15/230086 | Full ring sliding nacelle with thrust reverser | Aug 4, 2016 | Issued |
Array
(
[id] => 17015696
[patent_doc_number] => 11085324
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2021-08-10
[patent_title] => Gas turbine and gas turbine operating method
[patent_app_type] => utility
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Array
(
[id] => 13326833
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[patent_issue_date] => 2018-08-02
[patent_title] => TURBOMACHINE COMPONENT AND METHOD OF MANUFACTURING OF SUCH COMPONENT WITH AN INCORPORATED FLUID CHANNEL
[patent_app_type] => utility
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Array
(
[id] => 15397353
[patent_doc_number] => 10539328
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[patent_kind] => B2
[patent_issue_date] => 2020-01-21
[patent_title] => Structure for supporting nozzle guide of gas turbine engine
[patent_app_type] => utility
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Array
(
[id] => 12152215
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[patent_title] => 'AIR SUPPLY CONTROL DURING MOTORING OF A GAS TURBINE ENGINE'
[patent_app_type] => utility
[patent_app_number] => 15/216168
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Array
(
[id] => 13290357
[patent_doc_number] => 10156363
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2018-12-18
[patent_title] => Compact multi-piece spring-loaded crossfire tube
[patent_app_type] => utility
[patent_app_number] => 15/214751
[patent_app_country] => US
[patent_app_date] => 2016-07-20
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[rel_patent_id] =>[rel_patent_doc_number] =>) 15/214751 | Compact multi-piece spring-loaded crossfire tube | Jul 19, 2016 | Issued |
Array
(
[id] => 12139174
[patent_doc_number] => 20180017257
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2018-01-18
[patent_title] => 'COMBUSTOR CASSETTE LINER MOUNTING ASSEMBLY'
[patent_app_type] => utility
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[rel_patent_id] =>[rel_patent_doc_number] =>) 15/208290 | Combustor cassette liner mounting assembly | Jul 11, 2016 | Issued |
Array
(
[id] => 11402712
[patent_doc_number] => 20170023250
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2017-01-26
[patent_title] => 'COWLING PART AND COMBUSTOR ASSEMBLY FOR A GAS TURBINE'
[patent_app_type] => utility
[patent_app_number] => 15/208315
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[rel_patent_id] =>[rel_patent_doc_number] =>) 15/208315 | COWLING PART AND COMBUSTOR ASSEMBLY FOR A GAS TURBINE | Jul 11, 2016 | Abandoned |
Array
(
[id] => 12126879
[patent_doc_number] => 20180010465
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2018-01-11
[patent_title] => 'COOLING HOLE WITH SHAPED METER'
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[rel_patent_id] =>[rel_patent_doc_number] =>) 15/207472 | Cooling hole with shaped meter | Jul 10, 2016 | Issued |
Array
(
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Array
(
[id] => 17105230
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[patent_title] => Bent combustion chamber from a turbine engine
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Array
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Array
(
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Array
(
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[patent_title] => Fuel injection locations based on combustor flow path
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Array
(
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Array
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Array
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Array
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