Search

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 numberTitle of the applicationFiling DateStatus
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 [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/A1/0266/20090266047.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 [patent_words_short_claim] => 0 [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 [patent_figures_cnt] => 5 [patent_no_of_words] => 4601 [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/A1/0133/20090133377.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 [patent_figures_cnt] => 9 [patent_no_of_words] => 6238 [patent_no_of_claims] => 16 [patent_no_of_ind_claims] => 4 [patent_words_short_claim] => 140 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [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 [patent_figures_cnt] => 7 [patent_no_of_words] => 6640 [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/A1/0115/20100115955.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 [patent_drawing_sheets_cnt] => 3 [patent_figures_cnt] => 4 [patent_no_of_words] => 4030 [patent_no_of_claims] => 14 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 201 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [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 [patent_figures_cnt] => 2 [patent_no_of_words] => 1718 [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/A1/0115/20100115912.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
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