
Phutthiwat Wongwian
Supervisory Patent Examiner (ID: 4354, Phone: (571)270-5426 , Office: P/3741 )
| Most Active Art Unit | 3741 |
| Art Unit(s) | 3747, 3741, 3748, 3746, 4177 |
| Total Applications | 851 |
| Issued Applications | 724 |
| Pending Applications | 12 |
| Abandoned Applications | 118 |
Applications
| Application number | Title of the application | Filing Date | Status |
|---|---|---|---|
Array
(
[id] => 9045226
[patent_doc_number] => 08539774
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2013-09-24
[patent_title] => 'Fuel injector mounting system'
[patent_app_type] => utility
[patent_app_number] => 13/358942
[patent_app_country] => US
[patent_app_date] => 2012-01-26
[patent_effective_date] => 0000-00-00
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[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13358942
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/358942 | Fuel injector mounting system | Jan 25, 2012 | Issued |
Array
(
[id] => 9230769
[patent_doc_number] => 08596069
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2013-12-03
[patent_title] => 'Rational late lean injection'
[patent_app_type] => utility
[patent_app_number] => 13/349923
[patent_app_country] => US
[patent_app_date] => 2012-01-13
[patent_effective_date] => 0000-00-00
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[rel_patent_id] =>[rel_patent_doc_number] =>) 13/349923 | Rational late lean injection | Jan 12, 2012 | Issued |
Array
(
[id] => 8687878
[patent_doc_number] => 08387400
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2013-03-05
[patent_title] => 'Thermal management for fuel injectors'
[patent_app_type] => utility
[patent_app_number] => 13/348682
[patent_app_country] => US
[patent_app_date] => 2012-01-12
[patent_effective_date] => 0000-00-00
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[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13348682
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/348682 | Thermal management for fuel injectors | Jan 11, 2012 | Issued |
Array
(
[id] => 8869141
[patent_doc_number] => 08464511
[patent_country] => US
[patent_kind] => B1
[patent_issue_date] => 2013-06-18
[patent_title] => 'Magnetically coupled contra-rotating propulsion stages'
[patent_app_type] => utility
[patent_app_number] => 13/344697
[patent_app_country] => US
[patent_app_date] => 2012-01-06
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
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[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13344697
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/344697 | Magnetically coupled contra-rotating propulsion stages | Jan 5, 2012 | Issued |
Array
(
[id] => 8800583
[patent_doc_number] => 08438851
[patent_country] => US
[patent_kind] => B1
[patent_issue_date] => 2013-05-14
[patent_title] => 'Combustor assembly for use in a turbine engine and methods of assembling same'
[patent_app_type] => utility
[patent_app_number] => 13/342303
[patent_app_country] => US
[patent_app_date] => 2012-01-03
[patent_effective_date] => 0000-00-00
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[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13342303
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/342303 | Combustor assembly for use in a turbine engine and methods of assembling same | Jan 2, 2012 | Issued |
Array
(
[id] => 8320163
[patent_doc_number] => 20120192567
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2012-08-02
[patent_title] => 'GAS TURBINE ENGINE FLANGE ASSEMBLY INCLUDING FLOW CIRCUIT'
[patent_app_type] => utility
[patent_app_number] => 13/337111
[patent_app_country] => US
[patent_app_date] => 2011-12-24
[patent_effective_date] => 0000-00-00
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[rel_patent_id] =>[rel_patent_doc_number] =>) 13/337111 | Gas turbine engine flange assembly including flow circuit | Dec 23, 2011 | Issued |
Array
(
[id] => 8887242
[patent_doc_number] => 20130160426
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2013-06-27
[patent_title] => 'ROCKET ENGINE INJECTOR ASSEMBLY WITH CRYOGENIC CAVITY INSULATION'
[patent_app_type] => utility
[patent_app_number] => 13/336604
[patent_app_country] => US
[patent_app_date] => 2011-12-23
[patent_effective_date] => 0000-00-00
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[rel_patent_id] =>[rel_patent_doc_number] =>) 13/336604 | ROCKET ENGINE INJECTOR ASSEMBLY WITH CRYOGENIC CAVITY INSULATION | Dec 22, 2011 | Abandoned |
Array
(
[id] => 10842376
[patent_doc_number] => 08869538
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2014-10-28
[patent_title] => 'Gas turbine engine flow path member'
[patent_app_type] => utility
[patent_app_number] => 13/334974
[patent_app_country] => US
[patent_app_date] => 2011-12-22
[patent_effective_date] => 0000-00-00
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[rel_patent_id] =>[rel_patent_doc_number] =>) 13/334974 | Gas turbine engine flow path member | Dec 21, 2011 | Issued |
Array
(
[id] => 10842371
[patent_doc_number] => 08869533
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2014-10-28
[patent_title] => 'Combustion system for a gas turbine comprising a resonator'
[patent_app_type] => utility
[patent_app_number] => 13/994791
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[rel_patent_id] =>[rel_patent_doc_number] =>) 13/994791 | Combustion system for a gas turbine comprising a resonator | Dec 1, 2011 | Issued |
Array
(
[id] => 8531506
[patent_doc_number] => 08307656
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[patent_kind] => B2
[patent_issue_date] => 2012-11-13
[patent_title] => 'Gas turbine engine systems involving cooling of combustion section liners'
[patent_app_type] => utility
[patent_app_number] => 13/287619
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[rel_patent_id] =>[rel_patent_doc_number] =>) 13/287619 | Gas turbine engine systems involving cooling of combustion section liners | Nov 1, 2011 | Issued |
Array
(
[id] => 8190351
[patent_doc_number] => 20120117978
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2012-05-17
[patent_title] => 'Generating Power Using an Ion Transport Membrane'
[patent_app_type] => utility
[patent_app_number] => 13/271994
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[firstpage_image] =>[orig_patent_app_number] => 13271994
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/271994 | Generating power using an ion transport membrane | Oct 11, 2011 | Issued |
Array
(
[id] => 8757920
[patent_doc_number] => 08418436
[patent_country] => US
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[patent_issue_date] => 2013-04-16
[patent_title] => 'Variable area fan nozzle and thrust reverser'
[patent_app_type] => utility
[patent_app_number] => 13/238028
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[rel_patent_id] =>[rel_patent_doc_number] =>) 13/238028 | Variable area fan nozzle and thrust reverser | Sep 20, 2011 | Issued |
Array
(
[id] => 9342691
[patent_doc_number] => 08661829
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[patent_issue_date] => 2014-03-04
[patent_title] => 'Aerodynamic shroud for the back of a combustion chamber of a turbomachine'
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[rel_patent_id] =>[rel_patent_doc_number] =>) 13/820763 | Aerodynamic shroud for the back of a combustion chamber of a turbomachine | Sep 12, 2011 | Issued |
Array
(
[id] => 8704304
[patent_doc_number] => 20130061593
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[patent_issue_date] => 2013-03-14
[patent_title] => 'SYSTEM AND METHOD FOR CONTROLLING A COMBUSTOR ASSEMBLY'
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[rel_patent_id] =>[rel_patent_doc_number] =>) 13/229950 | System and method for controlling a combustor assembly | Sep 11, 2011 | Issued |
Array
(
[id] => 8705136
[patent_doc_number] => 20130062425
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[patent_issue_date] => 2013-03-14
[patent_title] => 'SYSTEM AND METHOD FOR DAMPING COMBUSTOR NOZZLE VIBRATIONS'
[patent_app_type] => utility
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Array
(
[id] => 9521735
[patent_doc_number] => 08745988
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[patent_issue_date] => 2014-06-10
[patent_title] => 'Pin fin arrangement for heat shield of gas turbine engine'
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Array
(
[id] => 7658987
[patent_doc_number] => 20110308256
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[patent_issue_date] => 2011-12-22
[patent_title] => 'Control Systems and Method for Controlling a Load Point of a Gas Turbine Engine'
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[rel_patent_id] =>[rel_patent_doc_number] =>) 13/218712 | Control systems and method for controlling a load point of a gas turbine engine | Aug 25, 2011 | Issued |
Array
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Array
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Array
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