
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] => 9387219
[patent_doc_number] => 08683805
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2014-04-01
[patent_title] => 'Injector seal for a gas turbomachine'
[patent_app_type] => utility
[patent_app_number] => 13/567415
[patent_app_country] => US
[patent_app_date] => 2012-08-06
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Array
(
[id] => 9290090
[patent_doc_number] => 20140033724
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2014-02-06
[patent_title] => 'FUEL NOZZLE ASSEMBLY AND METHODS OF ASSEMBLING SAME'
[patent_app_type] => utility
[patent_app_number] => 13/566506
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Array
(
[id] => 9955621
[patent_doc_number] => 09003803
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[patent_issue_date] => 2015-04-14
[patent_title] => 'Combustor cap assembly'
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Array
(
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[patent_issue_date] => 2014-02-06
[patent_title] => 'MULTI-STEP COMBUSTOR'
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Array
(
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[patent_issue_date] => 2015-09-08
[patent_title] => 'Turbomachine including horizontal joint heating and method of controlling tip clearance in a gas turbomachine'
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Array
(
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[patent_title] => 'System and method for recirculating and recovering energy from compressor discharge bleed air'
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Array
(
[id] => 8633453
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[patent_title] => 'Pulsed Detonation Engine'
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Array
(
[id] => 10187955
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[patent_title] => 'Method for operating a gas turbine power plant with flue gas recirculation'
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[rel_patent_id] =>[rel_patent_doc_number] =>) 13/560551 | Method for operating a gas turbine power plant with flue gas recirculation | Jul 26, 2012 | Issued |
Array
(
[id] => 9276613
[patent_doc_number] => 20140026581
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[patent_kind] => A1
[patent_issue_date] => 2014-01-30
[patent_title] => 'LINER STOP FOR TURBINE SYSTEM COMBUSTOR'
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[rel_patent_id] =>[rel_patent_doc_number] =>) 13/558470 | Liner stop for turbine system combustor | Jul 25, 2012 | Issued |
Array
(
[id] => 12247925
[patent_doc_number] => 09920696
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[patent_kind] => B2
[patent_issue_date] => 2018-03-20
[patent_title] => 'Method for operating a gas turbine and gas turbine unit useful for carrying out the method'
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[rel_patent_id] =>[rel_patent_doc_number] =>) 13/555331 | Method for operating a gas turbine and gas turbine unit useful for carrying out the method | Jul 22, 2012 | Issued |
Array
(
[id] => 9265484
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[patent_title] => 'SYSTEM AND METHOD FOR AUTO-TUNING A COMBUSTION SYSTEM OF A GAS TURBINE'
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[rel_patent_id] =>[rel_patent_doc_number] =>) 13/551702 | SYSTEM AND METHOD FOR AUTO-TUNING A COMBUSTION SYSTEM OF A GAS TURBINE | Jul 17, 2012 | Abandoned |
Array
(
[id] => 8614296
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[patent_title] => 'METHOD OF INHIBITING ICE ACCRETION WITHIN A TURBINE ENGINE AND CONTROL SYSTEM THEREFOR'
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[rel_patent_id] =>[rel_patent_doc_number] =>) 13/546514 | Method of inhibiting ice accretion within a turbine engine and control system therefor | Jul 10, 2012 | Issued |
Array
(
[id] => 9841934
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[patent_title] => 'Fuel flexible fuel injector'
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Array
(
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Array
(
[id] => 9975516
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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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[rel_patent_id] =>[rel_patent_doc_number] =>) 13/523451 | Controlling a combustion device to lower combustion-induced pulsations by changing and resetting fuel stagings at different rates of change | Jun 13, 2012 | Issued |