
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] => 8373416
[patent_doc_number] => 08256202
[patent_country] => US
[patent_kind] => B1
[patent_issue_date] => 2012-09-04
[patent_title] => 'High bypass turbofan'
[patent_app_type] => utility
[patent_app_number] => 12/277541
[patent_app_country] => US
[patent_app_date] => 2008-11-25
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 2
[patent_figures_cnt] => 4
[patent_no_of_words] => 2499
[patent_no_of_claims] => 26
[patent_no_of_ind_claims] => 7
[patent_words_short_claim] => 92
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 12277541
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/277541 | High bypass turbofan | Nov 24, 2008 | Issued |
Array
(
[id] => 5571882
[patent_doc_number] => 20090139241
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2009-06-04
[patent_title] => 'COMBUSTING SYSTEM, REMODELING METHOD FOR COMBUSTING SYSTEM, AND FUEL INJECTION METHOD FOR COMBUSTING SYSTEM'
[patent_app_type] => utility
[patent_app_number] => 12/277324
[patent_app_country] => US
[patent_app_date] => 2008-11-25
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 9
[patent_figures_cnt] => 9
[patent_no_of_words] => 7202
[patent_no_of_claims] => 9
[patent_no_of_ind_claims] => 6
[patent_words_short_claim] => 0
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0139/20090139241.pdf
[firstpage_image] =>[orig_patent_app_number] => 12277324
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/277324 | Combusting system, remodeling method for combusting system, and fuel injection method for combusting system | Nov 24, 2008 | Issued |
Array
(
[id] => 8350198
[patent_doc_number] => 08245519
[patent_country] => US
[patent_kind] => B1
[patent_issue_date] => 2012-08-21
[patent_title] => 'Laser shaped film cooling hole'
[patent_app_type] => utility
[patent_app_number] => 12/277586
[patent_app_country] => US
[patent_app_date] => 2008-11-25
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 8
[patent_no_of_words] => 2644
[patent_no_of_claims] => 9
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 124
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 12277586
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/277586 | Laser shaped film cooling hole | Nov 24, 2008 | Issued |
Array
(
[id] => 6535145
[patent_doc_number] => 20100126181
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2010-05-27
[patent_title] => 'METHOD FOR CONTROLLING AN EXHAUST GAS RECIRCULATION SYSTEM'
[patent_app_type] => utility
[patent_app_number] => 12/275318
[patent_app_country] => US
[patent_app_date] => 2008-11-21
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
[patent_figures_cnt] => 5
[patent_no_of_words] => 6593
[patent_no_of_claims] => 17
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 0
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0126/20100126181.pdf
[firstpage_image] =>[orig_patent_app_number] => 12275318
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/275318 | Method for controlling an exhaust gas recirculation system | Nov 20, 2008 | Issued |
Array
(
[id] => 5560554
[patent_doc_number] => 20090133406
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2009-05-28
[patent_title] => 'FAN NOZZLE OF ADJUSTABLE SECTION'
[patent_app_type] => utility
[patent_app_number] => 12/275729
[patent_app_country] => US
[patent_app_date] => 2008-11-21
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 3
[patent_no_of_words] => 1375
[patent_no_of_claims] => 7
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 0
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0133/20090133406.pdf
[firstpage_image] =>[orig_patent_app_number] => 12275729
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/275729 | Fan nozzle of adjustable section | Nov 20, 2008 | Issued |
Array
(
[id] => 7521784
[patent_doc_number] => 08024935
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2011-09-27
[patent_title] => 'Flush inlet scoop design for aircraft bleed air system'
[patent_app_type] => utility
[patent_app_number] => 12/275990
[patent_app_country] => US
[patent_app_date] => 2008-11-21
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 4
[patent_no_of_words] => 3531
[patent_no_of_claims] => 20
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 95
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/08/024/08024935.pdf
[firstpage_image] =>[orig_patent_app_number] => 12275990
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/275990 | Flush inlet scoop design for aircraft bleed air system | Nov 20, 2008 | Issued |
Array
(
[id] => 8150270
[patent_doc_number] => 08166748
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2012-05-01
[patent_title] => 'Gas turbine engine booster having rotatable radially inwardly extending blades and non-rotatable vanes'
[patent_app_type] => utility
[patent_app_number] => 12/275813
[patent_app_country] => US
[patent_app_date] => 2008-11-21
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 6
[patent_figures_cnt] => 6
[patent_no_of_words] => 3985
[patent_no_of_claims] => 19
[patent_no_of_ind_claims] => 4
[patent_words_short_claim] => 58
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/08/166/08166748.pdf
[firstpage_image] =>[orig_patent_app_number] => 12275813
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/275813 | Gas turbine engine booster having rotatable radially inwardly extending blades and non-rotatable vanes | Nov 20, 2008 | Issued |
Array
(
[id] => 6511639
[patent_doc_number] => 20100122538
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2010-05-20
[patent_title] => 'METHODS, APPARATUS AND SYSTEMS CONCERNING THE CIRCUMFERENTIAL CLOCKING OF TURBINE AIRFOILS IN RELATION TO COMBUSTOR CANS AND THE FLOW OF COOLING AIR THROUGH THE TURBINE HOT GAS FLOWPATH'
[patent_app_type] => utility
[patent_app_number] => 12/274568
[patent_app_country] => US
[patent_app_date] => 2008-11-20
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 12
[patent_figures_cnt] => 12
[patent_no_of_words] => 8682
[patent_no_of_claims] => 24
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 0
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0122/20100122538.pdf
[firstpage_image] =>[orig_patent_app_number] => 12274568
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/274568 | Methods, apparatus and systems concerning the circumferential clocking of turbine airfoils in relation to combustor cans and the flow of cooling air through the turbine hot gas flowpath | Nov 19, 2008 | Issued |
Array
(
[id] => 5560555
[patent_doc_number] => 20090133407
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2009-05-28
[patent_title] => 'PLASMA GASIFICATION SYSTEM'
[patent_app_type] => utility
[patent_app_number] => 12/274473
[patent_app_country] => US
[patent_app_date] => 2008-11-20
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 2
[patent_figures_cnt] => 2
[patent_no_of_words] => 2869
[patent_no_of_claims] => 18
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 0
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0133/20090133407.pdf
[firstpage_image] =>[orig_patent_app_number] => 12274473
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/274473 | PLASMA GASIFICATION SYSTEM | Nov 19, 2008 | Abandoned |
Array
(
[id] => 6511627
[patent_doc_number] => 20100122537
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2010-05-20
[patent_title] => 'COMBUSTORS WITH INSERTS BETWEEN DUAL WALL LINERS'
[patent_app_type] => utility
[patent_app_number] => 12/275050
[patent_app_country] => US
[patent_app_date] => 2008-11-20
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 3
[patent_no_of_words] => 3348
[patent_no_of_claims] => 20
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 0
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0122/20100122537.pdf
[firstpage_image] =>[orig_patent_app_number] => 12275050
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/275050 | Combustors with inserts between dual wall liners | Nov 19, 2008 | Issued |
Array
(
[id] => 6511613
[patent_doc_number] => 20100122535
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2010-05-20
[patent_title] => 'FUEL CONTROL SYSTEM FOR GAS TURBINE AND FEED FORWARD CONTROL METHOD'
[patent_app_type] => utility
[patent_app_number] => 12/272874
[patent_app_country] => US
[patent_app_date] => 2008-11-18
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
[patent_figures_cnt] => 5
[patent_no_of_words] => 4591
[patent_no_of_claims] => 20
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 0
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0122/20100122535.pdf
[firstpage_image] =>[orig_patent_app_number] => 12272874
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/272874 | Fuel control system for gas turbine and feed forward control method | Nov 17, 2008 | Issued |
Array
(
[id] => 6511620
[patent_doc_number] => 20100122536
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2010-05-20
[patent_title] => 'PLASMA FLOW CONTROLLED DIFFUSER SYSTEM'
[patent_app_type] => utility
[patent_app_number] => 12/272511
[patent_app_country] => US
[patent_app_date] => 2008-11-17
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 10
[patent_figures_cnt] => 10
[patent_no_of_words] => 6839
[patent_no_of_claims] => 20
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 0
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0122/20100122536.pdf
[firstpage_image] =>[orig_patent_app_number] => 12272511
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/272511 | Plasma flow controlled diffuser system | Nov 16, 2008 | Issued |
Array
(
[id] => 5571840
[patent_doc_number] => 20090139199
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2009-06-04
[patent_title] => 'PULSE DETONATION COMBUSTOR VALVE FOR HIGH TEMPERATURE AND HIGH PRESSURE OPERATION'
[patent_app_type] => utility
[patent_app_number] => 12/271082
[patent_app_country] => US
[patent_app_date] => 2008-11-14
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 9
[patent_figures_cnt] => 9
[patent_no_of_words] => 4471
[patent_no_of_claims] => 22
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 0
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0139/20090139199.pdf
[firstpage_image] =>[orig_patent_app_number] => 12271082
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/271082 | PULSE DETONATION COMBUSTOR VALVE FOR HIGH TEMPERATURE AND HIGH PRESSURE OPERATION | Nov 13, 2008 | Abandoned |
Array
(
[id] => 5554470
[patent_doc_number] => 20090266047
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2009-10-29
[patent_title] => 'MULTI-TUBE, CAN-ANNULAR PULSE DETONATION COMBUSTOR BASED ENGINE WITH TANGENTIALLY AND LONGITUDINALLY ANGLED PULSE DETONATION COMBUSTORS'
[patent_app_type] => utility
[patent_app_number] => 12/271070
[patent_app_country] => US
[patent_app_date] => 2008-11-14
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 6
[patent_figures_cnt] => 6
[patent_no_of_words] => 5314
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[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0266/20090266047.pdf
[firstpage_image] =>[orig_patent_app_number] => 12271070
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/271070 | MULTI-TUBE, CAN-ANNULAR PULSE DETONATION COMBUSTOR BASED ENGINE WITH TANGENTIALLY AND LONGITUDINALLY ANGLED PULSE DETONATION COMBUSTORS | Nov 13, 2008 | Abandoned |
Array
(
[id] => 5571844
[patent_doc_number] => 20090139203
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2009-06-04
[patent_title] => 'METHOD AND APPARATUS FOR TAILORING THE EQUIVALENCE RATIO IN A VALVED PULSE DETONATION COMBUSTOR'
[patent_app_type] => utility
[patent_app_number] => 12/271091
[patent_app_country] => US
[patent_app_date] => 2008-11-14
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 9
[patent_figures_cnt] => 9
[patent_no_of_words] => 7849
[patent_no_of_claims] => 24
[patent_no_of_ind_claims] => 2
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[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0139/20090139203.pdf
[firstpage_image] =>[orig_patent_app_number] => 12271091
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/271091 | METHOD AND APPARATUS FOR TAILORING THE EQUIVALENCE RATIO IN A VALVED PULSE DETONATION COMBUSTOR | Nov 13, 2008 | Abandoned |
Array
(
[id] => 5560525
[patent_doc_number] => 20090133377
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2009-05-28
[patent_title] => 'MULTI-TUBE PULSE DETONATION COMBUSTOR BASED ENGINE'
[patent_app_type] => utility
[patent_app_number] => 12/270980
[patent_app_country] => US
[patent_app_date] => 2008-11-14
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
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[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0133/20090133377.pdf
[firstpage_image] =>[orig_patent_app_number] => 12270980
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/270980 | MULTI-TUBE PULSE DETONATION COMBUSTOR BASED ENGINE | Nov 13, 2008 | Abandoned |
Array
(
[id] => 7799266
[patent_doc_number] => 08127531
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2012-03-06
[patent_title] => 'Radially translating fan nozzle nacelle'
[patent_app_type] => utility
[patent_app_number] => 12/268902
[patent_app_country] => US
[patent_app_date] => 2008-11-11
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 7
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[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/08/127/08127531.pdf
[firstpage_image] =>[orig_patent_app_number] => 12268902
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/268902 | Radially translating fan nozzle nacelle | Nov 10, 2008 | Issued |
Array
(
[id] => 6267969
[patent_doc_number] => 20100115955
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2010-05-13
[patent_title] => 'THERMAL MANAGEMENT FOR FUEL INJECTORS'
[patent_app_type] => utility
[patent_app_number] => 12/268511
[patent_app_country] => US
[patent_app_date] => 2008-11-11
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 7
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[pdf_file] => publications/A1/0115/20100115955.pdf
[firstpage_image] =>[orig_patent_app_number] => 12268511
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/268511 | Thermal management for fuel injectors | Nov 10, 2008 | Issued |
Array
(
[id] => 8673430
[patent_doc_number] => 08381531
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2013-02-26
[patent_title] => 'Gas turbine fuel injector with a rich catalyst'
[patent_app_type] => utility
[patent_app_number] => 12/289969
[patent_app_country] => US
[patent_app_date] => 2008-11-07
[patent_effective_date] => 0000-00-00
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[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 12289969
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/289969 | Gas turbine fuel injector with a rich catalyst | Nov 6, 2008 | Issued |
Array
(
[id] => 6267877
[patent_doc_number] => 20100115912
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2010-05-13
[patent_title] => 'PARALLEL TURBINE ARRANGEMENT AND METHOD'
[patent_app_type] => utility
[patent_app_number] => 12/266897
[patent_app_country] => US
[patent_app_date] => 2008-11-07
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 2
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[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0115/20100115912.pdf
[firstpage_image] =>[orig_patent_app_number] => 12266897
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/266897 | PARALLEL TURBINE ARRANGEMENT AND METHOD | Nov 6, 2008 | Abandoned |