
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] => 5018216
[patent_doc_number] => 20070144180
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2007-06-28
[patent_title] => 'Dual bayonet engagement and method of assembling a combustor liner in a gas turbine engine'
[patent_app_type] => utility
[patent_app_number] => 11/316801
[patent_app_country] => US
[patent_app_date] => 2005-12-22
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 8
[patent_figures_cnt] => 8
[patent_no_of_words] => 3678
[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/A1/0144/20070144180.pdf
[firstpage_image] =>[orig_patent_app_number] => 11316801
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/316801 | Dual bayonet engagement and method of assembling a combustor liner in a gas turbine engine | Dec 21, 2005 | Abandoned |
Array
(
[id] => 5018176
[patent_doc_number] => 20070144140
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2007-06-28
[patent_title] => 'High propellant mass fraction hybrid rocket propulsion'
[patent_app_type] => utility
[patent_app_number] => 11/314467
[patent_app_country] => US
[patent_app_date] => 2005-12-22
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 0
[patent_figures_cnt] => 0
[patent_no_of_words] => 2973
[patent_no_of_claims] => 4
[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/A1/0144/20070144140.pdf
[firstpage_image] =>[orig_patent_app_number] => 11314467
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/314467 | High propellant mass fraction hybrid rocket propulsion | Dec 21, 2005 | Abandoned |
Array
(
[id] => 4460380
[patent_doc_number] => 07934382
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2011-05-03
[patent_title] => 'Combustor turbine interface'
[patent_app_type] => utility
[patent_app_number] => 11/315838
[patent_app_country] => US
[patent_app_date] => 2005-12-22
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 7
[patent_no_of_words] => 2610
[patent_no_of_claims] => 10
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 115
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/07/934/07934382.pdf
[firstpage_image] =>[orig_patent_app_number] => 11315838
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/315838 | Combustor turbine interface | Dec 21, 2005 | Issued |
Array
(
[id] => 4541191
[patent_doc_number] => 07836699
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2010-11-23
[patent_title] => 'Combustor nozzle'
[patent_app_type] => utility
[patent_app_number] => 11/312158
[patent_app_country] => US
[patent_app_date] => 2005-12-20
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 6
[patent_figures_cnt] => 9
[patent_no_of_words] => 1689
[patent_no_of_claims] => 9
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 71
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/07/836/07836699.pdf
[firstpage_image] =>[orig_patent_app_number] => 11312158
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/312158 | Combustor nozzle | Dec 19, 2005 | Issued |
Array
(
[id] => 5115461
[patent_doc_number] => 20070137174
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2007-06-21
[patent_title] => 'Axial flow positive displacement worm gas generator'
[patent_app_type] => utility
[patent_app_number] => 11/313146
[patent_app_country] => US
[patent_app_date] => 2005-12-19
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 11
[patent_figures_cnt] => 11
[patent_no_of_words] => 3381
[patent_no_of_claims] => 44
[patent_no_of_ind_claims] => 4
[patent_words_short_claim] => 0
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0137/20070137174.pdf
[firstpage_image] =>[orig_patent_app_number] => 11313146
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/313146 | Axial flow positive displacement worm gas generator | Dec 18, 2005 | Issued |
Array
(
[id] => 291153
[patent_doc_number] => 07543440
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2009-06-09
[patent_title] => 'Multiple turbine system with a single recuperator'
[patent_app_type] => utility
[patent_app_number] => 11/305112
[patent_app_country] => US
[patent_app_date] => 2005-12-19
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 4
[patent_no_of_words] => 5488
[patent_no_of_claims] => 15
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 107
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/07/543/07543440.pdf
[firstpage_image] =>[orig_patent_app_number] => 11305112
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/305112 | Multiple turbine system with a single recuperator | Dec 18, 2005 | Issued |
Array
(
[id] => 5115504
[patent_doc_number] => 20070137217
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2007-06-21
[patent_title] => 'Engine with fuel/lubricant supply system for bearing lubrication'
[patent_app_type] => utility
[patent_app_number] => 11/305608
[patent_app_country] => US
[patent_app_date] => 2005-12-16
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 4
[patent_no_of_words] => 1364
[patent_no_of_claims] => 32
[patent_no_of_ind_claims] => 4
[patent_words_short_claim] => 0
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0137/20070137217.pdf
[firstpage_image] =>[orig_patent_app_number] => 11305608
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/305608 | Engine with fuel/lubricant supply system for bearing lubrication | Dec 15, 2005 | Issued |
Array
(
[id] => 5115460
[patent_doc_number] => 20070137173
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2007-06-21
[patent_title] => 'Axial flow positive displacement gas generator with combustion extending into an expansion section'
[patent_app_type] => utility
[patent_app_number] => 11/303143
[patent_app_country] => US
[patent_app_date] => 2005-12-16
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 10
[patent_figures_cnt] => 10
[patent_no_of_words] => 3615
[patent_no_of_claims] => 45
[patent_no_of_ind_claims] => 4
[patent_words_short_claim] => 0
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0137/20070137173.pdf
[firstpage_image] =>[orig_patent_app_number] => 11303143
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/303143 | Axial flow positive displacement gas generator with combustion extending into an expansion section | Dec 15, 2005 | Issued |
Array
(
[id] => 336560
[patent_doc_number] => 07503179
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2009-03-17
[patent_title] => 'System and method to exhaust spent cooling air of gas turbine engine active clearance control'
[patent_app_type] => utility
[patent_app_number] => 11/303305
[patent_app_country] => US
[patent_app_date] => 2005-12-16
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 11
[patent_figures_cnt] => 11
[patent_no_of_words] => 3207
[patent_no_of_claims] => 20
[patent_no_of_ind_claims] => 4
[patent_words_short_claim] => 76
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/07/503/07503179.pdf
[firstpage_image] =>[orig_patent_app_number] => 11303305
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/303305 | System and method to exhaust spent cooling air of gas turbine engine active clearance control | Dec 15, 2005 | Issued |
Array
(
[id] => 1075702
[patent_doc_number] => 07614211
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2009-11-10
[patent_title] => 'Swirling flows and swirler to enhance pulse detonation engine operation'
[patent_app_type] => utility
[patent_app_number] => 11/304411
[patent_app_country] => US
[patent_app_date] => 2005-12-15
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 3
[patent_no_of_words] => 5101
[patent_no_of_claims] => 12
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 215
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/07/614/07614211.pdf
[firstpage_image] =>[orig_patent_app_number] => 11304411
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/304411 | Swirling flows and swirler to enhance pulse detonation engine operation | Dec 14, 2005 | Issued |
Array
(
[id] => 5249654
[patent_doc_number] => 20070131110
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2007-06-14
[patent_title] => 'Vacuum system for membrane fuel stabilization unit'
[patent_app_type] => utility
[patent_app_number] => 11/302910
[patent_app_country] => US
[patent_app_date] => 2005-12-14
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 3
[patent_no_of_words] => 1472
[patent_no_of_claims] => 19
[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/A1/0131/20070131110.pdf
[firstpage_image] =>[orig_patent_app_number] => 11302910
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/302910 | Vacuum system for membrane fuel stabilization unit | Dec 13, 2005 | Issued |
Array
(
[id] => 5249456
[patent_doc_number] => 20070130912
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2007-06-14
[patent_title] => 'Shrouded turbofan bleed duct'
[patent_app_type] => utility
[patent_app_number] => 11/297698
[patent_app_country] => US
[patent_app_date] => 2005-12-08
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 8
[patent_figures_cnt] => 8
[patent_no_of_words] => 6104
[patent_no_of_claims] => 35
[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/A1/0130/20070130912.pdf
[firstpage_image] =>[orig_patent_app_number] => 11297698
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/297698 | Shrouded turbofan bleed duct | Dec 7, 2005 | Issued |
Array
(
[id] => 5075922
[patent_doc_number] => 20070119146
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2007-05-31
[patent_title] => 'Retarding and filter cleaning method and system'
[patent_app_type] => utility
[patent_app_number] => 11/289321
[patent_app_country] => US
[patent_app_date] => 2005-11-30
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 4
[patent_no_of_words] => 3817
[patent_no_of_claims] => 36
[patent_no_of_ind_claims] => 7
[patent_words_short_claim] => 0
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0119/20070119146.pdf
[firstpage_image] =>[orig_patent_app_number] => 11289321
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/289321 | Retarding and filter cleaning method and system | Nov 29, 2005 | Abandoned |
Array
(
[id] => 5081851
[patent_doc_number] => 20070271901
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2007-11-29
[patent_title] => 'AN OUTLET NOZZLE FOR A JET ENGINE, AN AIRCRAFT COMPRISING THE OUTLET NOZZLE AND A METHOD FOR CONTROLLING A GAS FLOW FROM THE JET ENGINE'
[patent_app_type] => utility
[patent_app_number] => 11/577506
[patent_app_country] => US
[patent_app_date] => 2005-11-01
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 7
[patent_figures_cnt] => 7
[patent_no_of_words] => 3626
[patent_no_of_claims] => 29
[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/A1/0271/20070271901.pdf
[firstpage_image] =>[orig_patent_app_number] => 11577506
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/577506 | Outlet nozzle for a jet engine, an aircraft comprising the outlet nozzle and a method for controlling a gas flow from the jet engine | Oct 31, 2005 | Issued |
Array
(
[id] => 5037142
[patent_doc_number] => 20070089424
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2007-04-26
[patent_title] => 'Gas turbine engine combustor hot streak control'
[patent_app_type] => utility
[patent_app_number] => 11/256786
[patent_app_country] => US
[patent_app_date] => 2005-10-24
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 3
[patent_no_of_words] => 2135
[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/A1/0089/20070089424.pdf
[firstpage_image] =>[orig_patent_app_number] => 11256786
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/256786 | Gas turbine engine combustor hot streak control | Oct 23, 2005 | Issued |
Array
(
[id] => 8281001
[patent_doc_number] => 08215096
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2012-07-10
[patent_title] => 'Outlet device for a jet engine and a craft comprising such an outlet device'
[patent_app_type] => utility
[patent_app_number] => 11/718728
[patent_app_country] => US
[patent_app_date] => 2005-10-20
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 7
[patent_figures_cnt] => 10
[patent_no_of_words] => 2982
[patent_no_of_claims] => 17
[patent_no_of_ind_claims] => 4
[patent_words_short_claim] => 128
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 11718728
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/718728 | Outlet device for a jet engine and a craft comprising such an outlet device | Oct 19, 2005 | Issued |
Array
(
[id] => 4468129
[patent_doc_number] => 07866159
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2011-01-11
[patent_title] => 'Variable geometry hysteresis control for a gas turbine engine'
[patent_app_type] => utility
[patent_app_number] => 11/253159
[patent_app_country] => US
[patent_app_date] => 2005-10-18
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 8
[patent_figures_cnt] => 9
[patent_no_of_words] => 8274
[patent_no_of_claims] => 17
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 122
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/07/866/07866159.pdf
[firstpage_image] =>[orig_patent_app_number] => 11253159
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/253159 | Variable geometry hysteresis control for a gas turbine engine | Oct 17, 2005 | Issued |
Array
(
[id] => 4456500
[patent_doc_number] => 07877979
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2011-02-01
[patent_title] => 'Integrated gasification combined cycle plant, method of controlling the plant, and method of producing fuel gas'
[patent_app_type] => utility
[patent_app_number] => 11/576636
[patent_app_country] => US
[patent_app_date] => 2005-10-04
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
[patent_figures_cnt] => 7
[patent_no_of_words] => 7700
[patent_no_of_claims] => 9
[patent_no_of_ind_claims] => 4
[patent_words_short_claim] => 206
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/07/877/07877979.pdf
[firstpage_image] =>[orig_patent_app_number] => 11576636
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/576636 | Integrated gasification combined cycle plant, method of controlling the plant, and method of producing fuel gas | Oct 3, 2005 | Issued |
Array
(
[id] => 4642787
[patent_doc_number] => 08020387
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2011-09-20
[patent_title] => 'Method of operating a burner, including a combustion chamber with a low nitrous oxide emission'
[patent_app_type] => utility
[patent_app_number] => 11/665101
[patent_app_country] => US
[patent_app_date] => 2005-09-30
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 2
[patent_figures_cnt] => 3
[patent_no_of_words] => 3776
[patent_no_of_claims] => 5
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 142
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/08/020/08020387.pdf
[firstpage_image] =>[orig_patent_app_number] => 11665101
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/665101 | Method of operating a burner, including a combustion chamber with a low nitrous oxide emission | Sep 29, 2005 | Issued |
Array
(
[id] => 4678828
[patent_doc_number] => 20080245054
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2008-10-09
[patent_title] => 'Cooling System for an Aircraft, Aircraft Comprising the Cooling System and Cooling Method'
[patent_app_type] => utility
[patent_app_number] => 12/065513
[patent_app_country] => US
[patent_app_date] => 2005-09-20
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 4
[patent_no_of_words] => 2526
[patent_no_of_claims] => 26
[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/A1/0245/20080245054.pdf
[firstpage_image] =>[orig_patent_app_number] => 12065513
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/065513 | Cooling System for an Aircraft, Aircraft Comprising the Cooling System and Cooling Method | Sep 19, 2005 | Abandoned |