
Phutthiwat Wongwian
Supervisory Patent Examiner (ID: 3946, Phone: (571)270-5426 , Office: P/3741 )
| Most Active Art Unit | 3741 |
| Art Unit(s) | 4177, 3746, 3748, 3747, 3741 |
| Total Applications | 868 |
| Issued Applications | 730 |
| Pending Applications | 23 |
| Abandoned Applications | 118 |
Applications
| Application number | Title of the application | Filing Date | Status |
|---|---|---|---|
Array
(
[id] => 4541010
[patent_doc_number] => 07836675
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2010-11-23
[patent_title] => 'Supercore sump vent pressure control'
[patent_app_type] => utility
[patent_app_number] => 11/358252
[patent_app_country] => US
[patent_app_date] => 2006-02-21
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 6
[patent_figures_cnt] => 7
[patent_no_of_words] => 2447
[patent_no_of_claims] => 10
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[patent_words_short_claim] => 169
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/07/836/07836675.pdf
[firstpage_image] =>[orig_patent_app_number] => 11358252
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/358252 | Supercore sump vent pressure control | Feb 20, 2006 | Issued |
Array
(
[id] => 5639459
[patent_doc_number] => 20060277914
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2006-12-14
[patent_title] => 'Combi-Supersonic-Adjusting-Nozzle'
[patent_app_type] => utility
[patent_app_number] => 11/357608
[patent_app_country] => US
[patent_app_date] => 2006-02-21
[patent_effective_date] => 0000-00-00
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[pdf_file] => publications/A1/0277/20060277914.pdf
[firstpage_image] =>[orig_patent_app_number] => 11357608
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/357608 | Combi-Supersonic-Adjusting-Nozzle | Feb 20, 2006 | Abandoned |
Array
(
[id] => 99238
[patent_doc_number] => 07721524
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2010-05-25
[patent_title] => 'Integrated airbreathing and non-airbreathing engine system'
[patent_app_type] => utility
[patent_app_number] => 11/354453
[patent_app_country] => US
[patent_app_date] => 2006-02-15
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 18
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[patent_no_of_words] => 6094
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[pdf_file] => patents/07/721/07721524.pdf
[firstpage_image] =>[orig_patent_app_number] => 11354453
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/354453 | Integrated airbreathing and non-airbreathing engine system | Feb 14, 2006 | Issued |
Array
(
[id] => 5097571
[patent_doc_number] => 20070180831
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2007-08-09
[patent_title] => 'Fuel flow tuning for a stage of a gas turbine engine'
[patent_app_type] => utility
[patent_app_number] => 11/350561
[patent_app_country] => US
[patent_app_date] => 2006-02-09
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 2
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[patent_no_of_words] => 2366
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[firstpage_image] =>[orig_patent_app_number] => 11350561
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/350561 | Fuel flow tuning for a stage of a gas turbine engine | Feb 8, 2006 | Issued |
Array
(
[id] => 5100625
[patent_doc_number] => 20070183887
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2007-08-09
[patent_title] => 'Particle collector for gas turbine engine'
[patent_app_type] => utility
[patent_app_number] => 11/350494
[patent_app_country] => US
[patent_app_date] => 2006-02-09
[patent_effective_date] => 0000-00-00
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[patent_no_of_words] => 1416
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[pdf_file] => publications/A1/0183/20070183887.pdf
[firstpage_image] =>[orig_patent_app_number] => 11350494
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/350494 | Particle collector for gas turbine engine | Feb 8, 2006 | Issued |
Array
(
[id] => 4537146
[patent_doc_number] => 07818955
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2010-10-26
[patent_title] => 'Fuel injection system and purging method'
[patent_app_type] => utility
[patent_app_number] => 11/346798
[patent_app_country] => US
[patent_app_date] => 2006-02-03
[patent_effective_date] => 0000-00-00
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[pdf_file] => patents/07/818/07818955.pdf
[firstpage_image] =>[orig_patent_app_number] => 11346798
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/346798 | Fuel injection system and purging method | Feb 2, 2006 | Issued |
Array
(
[id] => 39243
[patent_doc_number] => 07779637
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2010-08-24
[patent_title] => 'Heat shield'
[patent_app_type] => utility
[patent_app_number] => 11/347545
[patent_app_country] => US
[patent_app_date] => 2006-02-03
[patent_effective_date] => 0000-00-00
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[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/07/779/07779637.pdf
[firstpage_image] =>[orig_patent_app_number] => 11347545
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/347545 | Heat shield | Feb 2, 2006 | Issued |
Array
(
[id] => 4809480
[patent_doc_number] => 20080190111
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2008-08-14
[patent_title] => 'Thermoacoustic Oscillation Damping In Gas Turbine Combustors With Annular Plenum'
[patent_app_type] => utility
[patent_app_number] => 11/883823
[patent_app_country] => US
[patent_app_date] => 2006-02-01
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 4
[patent_no_of_words] => 5099
[patent_no_of_claims] => 9
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[pdf_file] => publications/A1/0190/20080190111.pdf
[firstpage_image] =>[orig_patent_app_number] => 11883823
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/883823 | Thermoacoustic Oscillation Damping In Gas Turbine Combustors With Annular Plenum | Jan 31, 2006 | Abandoned |
Array
(
[id] => 5174144
[patent_doc_number] => 20070175201
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2007-08-02
[patent_title] => 'Power system'
[patent_app_type] => utility
[patent_app_number] => 11/342618
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[firstpage_image] =>[orig_patent_app_number] => 11342618
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/342618 | Power system | Jan 30, 2006 | Abandoned |
Array
(
[id] => 5174165
[patent_doc_number] => 20070175222
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2007-08-02
[patent_title] => 'Multipurpose gas generator ramjet/scramjet cold start system'
[patent_app_type] => utility
[patent_app_number] => 11/344764
[patent_app_country] => US
[patent_app_date] => 2006-01-31
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 2
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[pdf_file] => publications/A1/0175/20070175222.pdf
[firstpage_image] =>[orig_patent_app_number] => 11344764
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/344764 | Multipurpose gas generator ramjet/scramjet cold start system | Jan 30, 2006 | Abandoned |
Array
(
[id] => 5888404
[patent_doc_number] => 20060275633
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2006-12-07
[patent_title] => 'Fuel processor'
[patent_app_type] => utility
[patent_app_number] => 11/342839
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[patent_effective_date] => 0000-00-00
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[pdf_file] => publications/A1/0275/20060275633.pdf
[firstpage_image] =>[orig_patent_app_number] => 11342839
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/342839 | Fuel processor | Jan 30, 2006 | Issued |
Array
(
[id] => 258879
[patent_doc_number] => 07571597
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2009-08-11
[patent_title] => 'Airframe mounted motor driven lubrication pump control system and method'
[patent_app_type] => utility
[patent_app_number] => 11/339160
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[pdf_file] => patents/07/571/07571597.pdf
[firstpage_image] =>[orig_patent_app_number] => 11339160
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/339160 | Airframe mounted motor driven lubrication pump control system and method | Jan 24, 2006 | Issued |
Array
(
[id] => 287703
[patent_doc_number] => 07546737
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[patent_issue_date] => 2009-06-16
[patent_title] => 'Segmented effusion cooled gas turbine engine combustor'
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[firstpage_image] =>[orig_patent_app_number] => 11339439
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/339439 | Segmented effusion cooled gas turbine engine combustor | Jan 23, 2006 | Issued |
Array
(
[id] => 159396
[patent_doc_number] => 07669421
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2010-03-02
[patent_title] => 'Combustor of gas turbine with concentric swirler vanes'
[patent_app_type] => utility
[patent_app_number] => 11/334744
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[pdf_file] => patents/07/669/07669421.pdf
[firstpage_image] =>[orig_patent_app_number] => 11334744
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/334744 | Combustor of gas turbine with concentric swirler vanes | Jan 18, 2006 | Issued |
Array
(
[id] => 5184922
[patent_doc_number] => 20070163228
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2007-07-19
[patent_title] => 'Gas augmented rocket engine'
[patent_app_type] => utility
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[firstpage_image] =>[orig_patent_app_number] => 11334965
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/334965 | Gas augmented rocket engine | Jan 18, 2006 | Abandoned |
Array
(
[id] => 5581620
[patent_doc_number] => 20090100822
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2009-04-23
[patent_title] => 'INTEGRATED GASIFICATION COMBINED CYCLE AND THE CONTROL METHOD'
[patent_app_type] => utility
[patent_app_number] => 11/915287
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[pdf_file] => publications/A1/0100/20090100822.pdf
[firstpage_image] =>[orig_patent_app_number] => 11915287
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/915287 | Integrated gasification combined cycle and the control method | Jan 17, 2006 | Issued |
Array
(
[id] => 332823
[patent_doc_number] => 07506510
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[patent_issue_date] => 2009-03-24
[patent_title] => 'System and method for cooling a staged airblast fuel injector'
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Array
(
[id] => 5577975
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[patent_title] => 'PIEZO-RESONANCE IGNITER AND IGNITION METHOD FOR PROPELLANT LIQUID ROCKET ENGINE'
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[rel_patent_id] =>[rel_patent_doc_number] =>) 11/333691 | Piezo-resonance igniter and ignition method for propellant liquid rocket engine | Jan 16, 2006 | Issued |
Array
(
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[patent_title] => 'Externally fueled trapped vortex cavity augmentor'
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[rel_patent_id] =>[rel_patent_doc_number] =>) 11/330782 | Externally fueled trapped vortex cavity augmentor | Jan 11, 2006 | Issued |
Array
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[rel_patent_id] =>[rel_patent_doc_number] =>) 11/330596 | Pilot fuel flow tuning for gas turbine combustors | Jan 11, 2006 | Issued |