
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] => 4622471
[patent_doc_number] => 08001764
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2011-08-23
[patent_title] => 'Vibration isolation engine mount system and method for ducted fans'
[patent_app_type] => utility
[patent_app_number] => 11/228336
[patent_app_country] => US
[patent_app_date] => 2005-09-19
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 6
[patent_figures_cnt] => 6
[patent_no_of_words] => 3368
[patent_no_of_claims] => 8
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 115
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/08/001/08001764.pdf
[firstpage_image] =>[orig_patent_app_number] => 11228336
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/228336 | Vibration isolation engine mount system and method for ducted fans | Sep 18, 2005 | Issued |
Array
(
[id] => 88157
[patent_doc_number] => 07735310
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2010-06-15
[patent_title] => 'Gas turbine and method for shutting off a gas turbine when breakage of a shaft is identified'
[patent_app_type] => utility
[patent_app_number] => 11/664356
[patent_app_country] => US
[patent_app_date] => 2005-09-17
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 2
[patent_figures_cnt] => 2
[patent_no_of_words] => 1469
[patent_no_of_claims] => 16
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 129
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/07/735/07735310.pdf
[firstpage_image] =>[orig_patent_app_number] => 11664356
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/664356 | Gas turbine and method for shutting off a gas turbine when breakage of a shaft is identified | Sep 16, 2005 | Issued |
Array
(
[id] => 231284
[patent_doc_number] => 07596950
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2009-10-06
[patent_title] => 'Augmentor radial fuel spray bar with counterswirling heat shield'
[patent_app_type] => utility
[patent_app_number] => 11/228793
[patent_app_country] => US
[patent_app_date] => 2005-09-16
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 7
[patent_figures_cnt] => 8
[patent_no_of_words] => 2909
[patent_no_of_claims] => 22
[patent_no_of_ind_claims] => 5
[patent_words_short_claim] => 67
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/07/596/07596950.pdf
[firstpage_image] =>[orig_patent_app_number] => 11228793
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/228793 | Augmentor radial fuel spray bar with counterswirling heat shield | Sep 15, 2005 | Issued |
Array
(
[id] => 167960
[patent_doc_number] => 07661272
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2010-02-16
[patent_title] => 'Turbofan jet engine with an ancillary-connecting arm, and the ancillary-connecting arm'
[patent_app_type] => utility
[patent_app_number] => 11/226384
[patent_app_country] => US
[patent_app_date] => 2005-09-15
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 8
[patent_no_of_words] => 4482
[patent_no_of_claims] => 8
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 170
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/07/661/07661272.pdf
[firstpage_image] =>[orig_patent_app_number] => 11226384
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/226384 | Turbofan jet engine with an ancillary-connecting arm, and the ancillary-connecting arm | Sep 14, 2005 | Issued |
Array
(
[id] => 5853471
[patent_doc_number] => 20060225404
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2006-10-12
[patent_title] => 'Vertical or short take off and landing vehicle'
[patent_app_type] => utility
[patent_app_number] => 11/226619
[patent_app_country] => US
[patent_app_date] => 2005-09-13
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 16
[patent_figures_cnt] => 16
[patent_no_of_words] => 10985
[patent_no_of_claims] => 11
[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/A1/0225/20060225404.pdf
[firstpage_image] =>[orig_patent_app_number] => 11226619
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/226619 | Vertical or short take off and landing vehicle | Sep 12, 2005 | Abandoned |
Array
(
[id] => 5122464
[patent_doc_number] => 20070234733
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2007-10-11
[patent_title] => 'Small gas turbine engine with multiple burn zones'
[patent_app_type] => utility
[patent_app_number] => 11/224906
[patent_app_country] => US
[patent_app_date] => 2005-09-12
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
[patent_figures_cnt] => 5
[patent_no_of_words] => 5711
[patent_no_of_claims] => 31
[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/A1/0234/20070234733.pdf
[firstpage_image] =>[orig_patent_app_number] => 11224906
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/224906 | Small gas turbine engine with multiple burn zones | Sep 11, 2005 | Issued |
Array
(
[id] => 309901
[patent_doc_number] => 07526921
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2009-05-05
[patent_title] => 'Auxiliary power unit with integral firebox'
[patent_app_type] => utility
[patent_app_number] => 11/225556
[patent_app_country] => US
[patent_app_date] => 2005-09-12
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 6
[patent_figures_cnt] => 11
[patent_no_of_words] => 3990
[patent_no_of_claims] => 13
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 177
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/07/526/07526921.pdf
[firstpage_image] =>[orig_patent_app_number] => 11225556
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/225556 | Auxiliary power unit with integral firebox | Sep 11, 2005 | Issued |
Array
(
[id] => 273038
[patent_doc_number] => 07559201
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2009-07-14
[patent_title] => 'Redundant fuel manifold sealing arrangement'
[patent_app_type] => utility
[patent_app_number] => 11/220849
[patent_app_country] => US
[patent_app_date] => 2005-09-08
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
[patent_figures_cnt] => 5
[patent_no_of_words] => 2815
[patent_no_of_claims] => 17
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 142
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/07/559/07559201.pdf
[firstpage_image] =>[orig_patent_app_number] => 11220849
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/220849 | Redundant fuel manifold sealing arrangement | Sep 7, 2005 | Issued |
Array
(
[id] => 50424
[patent_doc_number] => 07765786
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2010-08-03
[patent_title] => 'Aircraft engine with separate auxiliary rotor and fan rotor'
[patent_app_type] => utility
[patent_app_number] => 11/219469
[patent_app_country] => US
[patent_app_date] => 2005-09-02
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 2
[patent_figures_cnt] => 2
[patent_no_of_words] => 2229
[patent_no_of_claims] => 16
[patent_no_of_ind_claims] => 6
[patent_words_short_claim] => 137
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/07/765/07765786.pdf
[firstpage_image] =>[orig_patent_app_number] => 11219469
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/219469 | Aircraft engine with separate auxiliary rotor and fan rotor | Sep 1, 2005 | Issued |
Array
(
[id] => 262588
[patent_doc_number] => 07568344
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2009-08-04
[patent_title] => 'Hydrostatic flow barrier for flexible fuel manifold'
[patent_app_type] => utility
[patent_app_number] => 11/216139
[patent_app_country] => US
[patent_app_date] => 2005-09-01
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 3
[patent_no_of_words] => 2467
[patent_no_of_claims] => 4
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 208
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/07/568/07568344.pdf
[firstpage_image] =>[orig_patent_app_number] => 11216139
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/216139 | Hydrostatic flow barrier for flexible fuel manifold | Aug 31, 2005 | Issued |
Array
(
[id] => 4951684
[patent_doc_number] => 20080184708
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2008-08-07
[patent_title] => 'Gas Turbine Combustor'
[patent_app_type] => utility
[patent_app_number] => 11/574203
[patent_app_country] => US
[patent_app_date] => 2005-09-01
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 17
[patent_figures_cnt] => 17
[patent_no_of_words] => 5243
[patent_no_of_claims] => 15
[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/A1/0184/20080184708.pdf
[firstpage_image] =>[orig_patent_app_number] => 11574203
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/574203 | Gas turbine combustor | Aug 31, 2005 | Issued |
Array
(
[id] => 298667
[patent_doc_number] => 07536862
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2009-05-26
[patent_title] => 'Fuel nozzle for gas turbine engines'
[patent_app_type] => utility
[patent_app_number] => 11/217505
[patent_app_country] => US
[patent_app_date] => 2005-09-01
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
[patent_figures_cnt] => 7
[patent_no_of_words] => 2932
[patent_no_of_claims] => 15
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 172
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/07/536/07536862.pdf
[firstpage_image] =>[orig_patent_app_number] => 11217505
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/217505 | Fuel nozzle for gas turbine engines | Aug 31, 2005 | Issued |
Array
(
[id] => 5897027
[patent_doc_number] => 20060042260
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2006-03-02
[patent_title] => 'Arrangement for controlling flow of fluid to a component of a gas turbine engine'
[patent_app_type] => utility
[patent_app_number] => 11/216124
[patent_app_country] => US
[patent_app_date] => 2005-09-01
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 10
[patent_figures_cnt] => 10
[patent_no_of_words] => 6731
[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/A1/0042/20060042260.pdf
[firstpage_image] =>[orig_patent_app_number] => 11216124
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/216124 | Arrangement for controlling flow of fluid to a component of a gas turbine engine | Aug 31, 2005 | Issued |
Array
(
[id] => 245852
[patent_doc_number] => 07584601
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2009-09-08
[patent_title] => 'Charged particle thrust engine'
[patent_app_type] => utility
[patent_app_number] => 11/219047
[patent_app_country] => US
[patent_app_date] => 2005-09-01
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 25
[patent_figures_cnt] => 177
[patent_no_of_words] => 21422
[patent_no_of_claims] => 41
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 283
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/07/584/07584601.pdf
[firstpage_image] =>[orig_patent_app_number] => 11219047
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/219047 | Charged particle thrust engine | Aug 31, 2005 | Issued |
Array
(
[id] => 5846117
[patent_doc_number] => 20060230742
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2006-10-19
[patent_title] => 'Micro reaction turbine with integrated combustion chamber and rotor'
[patent_app_type] => utility
[patent_app_number] => 11/212782
[patent_app_country] => US
[patent_app_date] => 2005-08-29
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
[patent_figures_cnt] => 5
[patent_no_of_words] => 3149
[patent_no_of_claims] => 17
[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/A1/0230/20060230742.pdf
[firstpage_image] =>[orig_patent_app_number] => 11212782
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/212782 | Micro reaction turbine with integrated combustion chamber and rotor | Aug 28, 2005 | Abandoned |
Array
(
[id] => 5100704
[patent_doc_number] => 20070183966
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2007-08-09
[patent_title] => 'Waste heat recovery apparatus, waste heat recovery system, and method of recovering waste heat'
[patent_app_type] => utility
[patent_app_number] => 11/629590
[patent_app_country] => US
[patent_app_date] => 2005-06-29
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 12
[patent_figures_cnt] => 12
[patent_no_of_words] => 9262
[patent_no_of_claims] => 21
[patent_no_of_ind_claims] => 17
[patent_words_short_claim] => 0
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0183/20070183966.pdf
[firstpage_image] =>[orig_patent_app_number] => 11629590
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/629590 | Waste heat recovery apparatus, waste heat recovery system, and method of recovering waste heat | Jun 28, 2005 | Abandoned |
Array
(
[id] => 317421
[patent_doc_number] => 07520123
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2009-04-21
[patent_title] => 'Mixing-enhancement inserts for pulse detonation chambers'
[patent_app_type] => utility
[patent_app_number] => 11/127459
[patent_app_country] => US
[patent_app_date] => 2005-05-12
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 15
[patent_figures_cnt] => 14
[patent_no_of_words] => 6521
[patent_no_of_claims] => 10
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 269
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/07/520/07520123.pdf
[firstpage_image] =>[orig_patent_app_number] => 11127459
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/127459 | Mixing-enhancement inserts for pulse detonation chambers | May 11, 2005 | Issued |
Array
(
[id] => 5639440
[patent_doc_number] => 20060277895
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2006-12-14
[patent_title] => 'Aircraft systems including cascade thrust reversers'
[patent_app_type] => utility
[patent_app_number] => 11/127424
[patent_app_country] => US
[patent_app_date] => 2005-05-11
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
[patent_figures_cnt] => 5
[patent_no_of_words] => 3323
[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/A1/0277/20060277895.pdf
[firstpage_image] =>[orig_patent_app_number] => 11127424
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/127424 | Aircraft systems including cascade thrust reversers | May 10, 2005 | Issued |
Array
(
[id] => 8723637
[patent_doc_number] => 08402745
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2013-03-26
[patent_title] => 'Pulse jet engines'
[patent_app_type] => utility
[patent_app_number] => 11/579212
[patent_app_country] => US
[patent_app_date] => 2005-05-03
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 8
[patent_figures_cnt] => 17
[patent_no_of_words] => 6651
[patent_no_of_claims] => 38
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 113
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 11579212
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/579212 | Pulse jet engines | May 2, 2005 | Issued |
Array
(
[id] => 5333373
[patent_doc_number] => 20090049837
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2009-02-26
[patent_title] => 'GAS TURBINE ENGINE AIR VALVE ASSEMBLY'
[patent_app_type] => utility
[patent_app_number] => 11/118584
[patent_app_country] => US
[patent_app_date] => 2005-04-28
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 9
[patent_figures_cnt] => 9
[patent_no_of_words] => 2985
[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/A1/0049/20090049837.pdf
[firstpage_image] =>[orig_patent_app_number] => 11118584
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/118584 | Gas turbine engine air valve assembly | Apr 27, 2005 | Issued |