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] => 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
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