
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] => 5109301
[patent_doc_number] => 20070193216
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2007-08-23
[patent_title] => 'Wall elements for gas turbine engine combustors'
[patent_app_type] => utility
[patent_app_number] => 11/652124
[patent_app_country] => US
[patent_app_date] => 2007-01-11
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 8
[patent_figures_cnt] => 8
[patent_no_of_words] => 3951
[patent_no_of_claims] => 18
[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/A1/0193/20070193216.pdf
[firstpage_image] =>[orig_patent_app_number] => 11652124
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/652124 | Wall elements for gas turbine engine combustors | Jan 10, 2007 | Issued |
Array
(
[id] => 4924241
[patent_doc_number] => 20080163604
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2008-07-10
[patent_title] => 'Turbine blade with reverse cooling air film hole direction'
[patent_app_type] => utility
[patent_app_number] => 11/651226
[patent_app_country] => US
[patent_app_date] => 2007-01-09
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 4
[patent_no_of_words] => 1337
[patent_no_of_claims] => 8
[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/A1/0163/20080163604.pdf
[firstpage_image] =>[orig_patent_app_number] => 11651226
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/651226 | Turbine blade with reverse cooling air film hole direction | Jan 8, 2007 | Issued |
Array
(
[id] => 6260330
[patent_doc_number] => 20100251723
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2010-10-07
[patent_title] => 'THIMBLE, SLEEVE, AND METHOD FOR COOLING A COMBUSTOR ASSEMBLY'
[patent_app_type] => utility
[patent_app_number] => 11/621197
[patent_app_country] => US
[patent_app_date] => 2007-01-09
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 10
[patent_figures_cnt] => 10
[patent_no_of_words] => 5013
[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/A1/0251/20100251723.pdf
[firstpage_image] =>[orig_patent_app_number] => 11621197
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/621197 | Thimble, sleeve, and method for cooling a combustor assembly | Jan 8, 2007 | Issued |
Array
(
[id] => 6504997
[patent_doc_number] => 20100229529
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2010-09-16
[patent_title] => 'Timing control system for pulse detonation engines'
[patent_app_type] => utility
[patent_app_number] => 11/651188
[patent_app_country] => US
[patent_app_date] => 2007-01-08
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 8
[patent_figures_cnt] => 8
[patent_no_of_words] => 4205
[patent_no_of_claims] => 23
[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/A1/0229/20100229529.pdf
[firstpage_image] =>[orig_patent_app_number] => 11651188
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/651188 | Timing control system for pulse detonation engines | Jan 7, 2007 | Issued |
Array
(
[id] => 1266
[patent_doc_number] => 07810311
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2010-10-12
[patent_title] => 'Cooling exchanger ducts'
[patent_app_type] => utility
[patent_app_number] => 11/650825
[patent_app_country] => US
[patent_app_date] => 2007-01-08
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 6
[patent_figures_cnt] => 6
[patent_no_of_words] => 2497
[patent_no_of_claims] => 15
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 274
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/07/810/07810311.pdf
[firstpage_image] =>[orig_patent_app_number] => 11650825
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/650825 | Cooling exchanger ducts | Jan 7, 2007 | Issued |
Array
(
[id] => 165086
[patent_doc_number] => 07665310
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2010-02-23
[patent_title] => 'Gas turbine engine having a cooling-air nacelle-cowl duct integral with a nacelle cowl'
[patent_app_type] => utility
[patent_app_number] => 11/616446
[patent_app_country] => US
[patent_app_date] => 2006-12-27
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 9
[patent_no_of_words] => 4022
[patent_no_of_claims] => 21
[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/07/665/07665310.pdf
[firstpage_image] =>[orig_patent_app_number] => 11616446
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/616446 | Gas turbine engine having a cooling-air nacelle-cowl duct integral with a nacelle cowl | Dec 26, 2006 | Issued |
Array
(
[id] => 5406205
[patent_doc_number] => 20090120103
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2009-05-14
[patent_title] => 'METHOD AND APPARATUS FOR SUB SEA POWER GENERATION'
[patent_app_type] => utility
[patent_app_number] => 12/158733
[patent_app_country] => US
[patent_app_date] => 2006-12-21
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 3
[patent_no_of_words] => 5403
[patent_no_of_claims] => 13
[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/A1/0120/20090120103.pdf
[firstpage_image] =>[orig_patent_app_number] => 12158733
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/158733 | METHOD AND APPARATUS FOR SUB SEA POWER GENERATION | Dec 20, 2006 | Abandoned |
Array
(
[id] => 4868230
[patent_doc_number] => 20080147289
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2008-06-19
[patent_title] => 'METHODS AND APPARATUS TO FACILITATE GAS TURBINE FUEL CONTROL'
[patent_app_type] => utility
[patent_app_number] => 11/612907
[patent_app_country] => US
[patent_app_date] => 2006-12-19
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 3
[patent_no_of_words] => 1964
[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/A1/0147/20080147289.pdf
[firstpage_image] =>[orig_patent_app_number] => 11612907
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/612907 | Methods and apparatus to facilitate gas turbine fuel control | Dec 18, 2006 | Issued |
Array
(
[id] => 4967413
[patent_doc_number] => 20070107415
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2007-05-17
[patent_title] => 'Method for operating a power plant and power plant'
[patent_app_type] => utility
[patent_app_number] => 11/635516
[patent_app_country] => US
[patent_app_date] => 2006-12-08
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
[patent_figures_cnt] => 5
[patent_no_of_words] => 3793
[patent_no_of_claims] => 20
[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/A1/0107/20070107415.pdf
[firstpage_image] =>[orig_patent_app_number] => 11635516
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/635516 | Method for operating a power plant and power plant | Dec 7, 2006 | Issued |
Array
(
[id] => 4781355
[patent_doc_number] => 20080134684
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2008-06-12
[patent_title] => 'APPARATUS AND METHOD FOR GAS TURBINE ACTIVE COMBUSTION CONTROL SYSTEM'
[patent_app_type] => utility
[patent_app_number] => 11/567950
[patent_app_country] => US
[patent_app_date] => 2006-12-07
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 13
[patent_figures_cnt] => 13
[patent_no_of_words] => 4787
[patent_no_of_claims] => 14
[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/A1/0134/20080134684.pdf
[firstpage_image] =>[orig_patent_app_number] => 11567950
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/567950 | Apparatus and method for gas turbine active combustion control system | Dec 6, 2006 | Issued |
Array
(
[id] => 59914
[patent_doc_number] => 07762077
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2010-07-27
[patent_title] => 'Single-stage hypersonic vehicle featuring advanced swirl combustion'
[patent_app_type] => utility
[patent_app_number] => 11/633836
[patent_app_country] => US
[patent_app_date] => 2006-12-05
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
[patent_figures_cnt] => 5
[patent_no_of_words] => 7778
[patent_no_of_claims] => 32
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 162
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/07/762/07762077.pdf
[firstpage_image] =>[orig_patent_app_number] => 11633836
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/633836 | Single-stage hypersonic vehicle featuring advanced swirl combustion | Dec 4, 2006 | Issued |
Array
(
[id] => 4503743
[patent_doc_number] => 07908840
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2011-03-22
[patent_title] => 'Turbine engine with integrated generator having shared lubrication system'
[patent_app_type] => utility
[patent_app_number] => 11/605671
[patent_app_country] => US
[patent_app_date] => 2006-11-29
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 6
[patent_figures_cnt] => 6
[patent_no_of_words] => 5578
[patent_no_of_claims] => 15
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 205
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/07/908/07908840.pdf
[firstpage_image] =>[orig_patent_app_number] => 11605671
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/605671 | Turbine engine with integrated generator having shared lubrication system | Nov 28, 2006 | Issued |
Array
(
[id] => 4428803
[patent_doc_number] => 07895820
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2011-03-01
[patent_title] => 'Seal for pulse detonation engine'
[patent_app_type] => utility
[patent_app_number] => 11/560600
[patent_app_country] => US
[patent_app_date] => 2006-11-16
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 21
[patent_figures_cnt] => 25
[patent_no_of_words] => 3828
[patent_no_of_claims] => 27
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 202
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/07/895/07895820.pdf
[firstpage_image] =>[orig_patent_app_number] => 11560600
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/560600 | Seal for pulse detonation engine | Nov 15, 2006 | Issued |
Array
(
[id] => 4903386
[patent_doc_number] => 20080112799
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2008-05-15
[patent_title] => 'Gas turbine engine providing simulated boundary layer thickness increase'
[patent_app_type] => utility
[patent_app_number] => 11/595040
[patent_app_country] => US
[patent_app_date] => 2006-11-10
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
[patent_figures_cnt] => 5
[patent_no_of_words] => 2650
[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/A1/0112/20080112799.pdf
[firstpage_image] =>[orig_patent_app_number] => 11595040
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/595040 | Gas turbine engine providing simulated boundary layer thickness increase | Nov 9, 2006 | Issued |
Array
(
[id] => 4568417
[patent_doc_number] => 07849668
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2010-12-14
[patent_title] => 'Rotor brake and windmilling lubrication system for geared turbofan engine'
[patent_app_type] => utility
[patent_app_number] => 11/552750
[patent_app_country] => US
[patent_app_date] => 2006-10-25
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
[patent_figures_cnt] => 6
[patent_no_of_words] => 2022
[patent_no_of_claims] => 18
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 94
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/07/849/07849668.pdf
[firstpage_image] =>[orig_patent_app_number] => 11552750
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/552750 | Rotor brake and windmilling lubrication system for geared turbofan engine | Oct 24, 2006 | Issued |
Array
(
[id] => 4911921
[patent_doc_number] => 20080092520
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2008-04-24
[patent_title] => 'Smart wireless engine sensor'
[patent_app_type] => utility
[patent_app_number] => 11/585475
[patent_app_country] => US
[patent_app_date] => 2006-10-24
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 4
[patent_no_of_words] => 1648
[patent_no_of_claims] => 16
[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/A1/0092/20080092520.pdf
[firstpage_image] =>[orig_patent_app_number] => 11585475
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/585475 | Smart wireless engine sensor | Oct 23, 2006 | Issued |
Array
(
[id] => 18552
[patent_doc_number] => 07797944
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2010-09-21
[patent_title] => 'Gas turbine engine having slim-line nacelle'
[patent_app_type] => utility
[patent_app_number] => 11/584030
[patent_app_country] => US
[patent_app_date] => 2006-10-20
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
[patent_figures_cnt] => 5
[patent_no_of_words] => 3092
[patent_no_of_claims] => 14
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 125
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/07/797/07797944.pdf
[firstpage_image] =>[orig_patent_app_number] => 11584030
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/584030 | Gas turbine engine having slim-line nacelle | Oct 19, 2006 | Issued |
Array
(
[id] => 4930264
[patent_doc_number] => 20080001039
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2008-01-03
[patent_title] => 'Thrust vectorable fan variable area nozzle for a gas turbine engine fan nacelle'
[patent_app_type] => utility
[patent_app_number] => 11/582219
[patent_app_country] => US
[patent_app_date] => 2006-10-17
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 15
[patent_figures_cnt] => 15
[patent_no_of_words] => 2439
[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/A1/0001/20080001039.pdf
[firstpage_image] =>[orig_patent_app_number] => 11582219
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/582219 | Thrust vectorable fan variable area nozzle for a gas turbine engine fan nacelle | Oct 16, 2006 | Issued |
Array
(
[id] => 4525533
[patent_doc_number] => 07870719
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2011-01-18
[patent_title] => 'Plasma enhanced rapidly expanded gas turbine engine transition duct'
[patent_app_type] => utility
[patent_app_number] => 11/580788
[patent_app_country] => US
[patent_app_date] => 2006-10-13
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 6
[patent_no_of_words] => 2040
[patent_no_of_claims] => 23
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 69
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/07/870/07870719.pdf
[firstpage_image] =>[orig_patent_app_number] => 11580788
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/580788 | Plasma enhanced rapidly expanded gas turbine engine transition duct | Oct 12, 2006 | Issued |
Array
(
[id] => 8640541
[patent_doc_number] => 08365513
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2013-02-05
[patent_title] => 'Turbofan engine operation control'
[patent_app_type] => utility
[patent_app_number] => 12/444856
[patent_app_country] => US
[patent_app_date] => 2006-10-12
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 2
[patent_figures_cnt] => 2
[patent_no_of_words] => 1949
[patent_no_of_claims] => 11
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 78
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 12444856
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/444856 | Turbofan engine operation control | Oct 11, 2006 | Issued |