Phutthiwat Wongwian

Array ( [id] => 5523713 [patent_doc_number] => 20090193789 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2009-08-06 [patent_title] => 'VARIABLE AREA FAN NOZZLE THRUST REVERSER' [patent_app_type] => utility [patent_app_number] => 12/306329 [patent_app_country] => US [patent_app_date] => 2006-10-12 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 5 [patent_figures_cnt] => 5 [patent_no_of_words] => 3173 [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/A1/0193/20090193789.pdf [firstpage_image] =>[orig_patent_app_number] => 12306329 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 4503889 [patent_doc_number] => 07908864 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2011-03-22 [patent_title] => 'Combustor nozzle for a fuel-flexible combustion system' [patent_app_type] => utility [patent_app_number] => 11/539195 [patent_app_country] => US [patent_app_date] => 2006-10-06 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 8 [patent_figures_cnt] => 8 [patent_no_of_words] => 4955 [patent_no_of_claims] => 22 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 204 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/07/908/07908864.pdf [firstpage_image] =>[orig_patent_app_number] => 11539195 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 4690457 [patent_doc_number] => 20080083227 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2008-04-10 [patent_title] => 'Oil distributing unit' [patent_app_type] => utility [patent_app_number] => 11/543793 [patent_app_country] => US [patent_app_date] => 2006-10-06 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 6 [patent_figures_cnt] => 6 [patent_no_of_words] => 2313 [patent_no_of_claims] => 17 [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/A1/0083/20080083227.pdf [firstpage_image] =>[orig_patent_app_number] => 11543793 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 4690455 [patent_doc_number] => 20080083225 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2008-04-10 [patent_title] => 'REDUCED STRESS INTERNAL MANIFOLD HEAT SHIELD ATTACHMENT' [patent_app_type] => utility [patent_app_number] => 11/538670 [patent_app_country] => US [patent_app_date] => 2006-10-04 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 4 [patent_figures_cnt] => 4 [patent_no_of_words] => 1929 [patent_no_of_claims] => 7 [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/A1/0083/20080083225.pdf [firstpage_image] =>[orig_patent_app_number] => 11538670 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 4940860 [patent_doc_number] => 20080078180 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2008-04-03 [patent_title] => 'METHODS AND APPARATUS FOR INJECTING FLUIDS INTO A TURBINE ENGINE' [patent_app_type] => utility [patent_app_number] => 11/537066 [patent_app_country] => US [patent_app_date] => 2006-09-29 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 6 [patent_figures_cnt] => 6 [patent_no_of_words] => 2319 [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/A1/0078/20080078180.pdf [firstpage_image] =>[orig_patent_app_number] => 11537066 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 4940841 [patent_doc_number] => 20080078161 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2008-04-03 [patent_title] => 'Quick change fastener system for attaching liner bracket to convergent flap and seal in turbine nozzle' [patent_app_type] => utility [patent_app_number] => 11/529836 [patent_app_country] => US [patent_app_date] => 2006-09-29 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 5 [patent_figures_cnt] => 5 [patent_no_of_words] => 1968 [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/A1/0078/20080078161.pdf [firstpage_image] =>[orig_patent_app_number] => 11529836 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 4935257 [patent_doc_number] => 20080072569 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2008-03-27 [patent_title] => 'GUIDE VANE AND METHOD OF FABRICATING THE SAME' [patent_app_type] => utility [patent_app_number] => 11/535676 [patent_app_country] => US [patent_app_date] => 2006-09-27 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 8 [patent_figures_cnt] => 8 [patent_no_of_words] => 2962 [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/A1/0072/20080072569.pdf [firstpage_image] =>[orig_patent_app_number] => 11535676 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 18555 [patent_doc_number] => 07797947 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2010-09-21 [patent_title] => 'Mounting assembly for securing an engine to an aircraft wing' [patent_app_type] => utility [patent_app_number] => 12/067191 [patent_app_country] => US [patent_app_date] => 2006-09-26 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 6 [patent_figures_cnt] => 8 [patent_no_of_words] => 5882 [patent_no_of_claims] => 15 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 131 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/07/797/07797947.pdf [firstpage_image] =>[orig_patent_app_number] => 12067191 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 4935289 [patent_doc_number] => 20080072601 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2008-03-27 [patent_title] => 'INTERNAL FUEL MANIFOLD AND FUEL FAIRING INTERFACE' [patent_app_type] => utility [patent_app_number] => 11/534246 [patent_app_country] => US [patent_app_date] => 2006-09-22 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 4 [patent_figures_cnt] => 4 [patent_no_of_words] => 2444 [patent_no_of_claims] => 7 [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/A1/0072/20080072601.pdf [firstpage_image] =>[orig_patent_app_number] => 11534246 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 4736999 [patent_doc_number] => 20080230651 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2008-09-25 [patent_title] => 'Turbofan Provided With a Pre-Cooler' [patent_app_type] => utility [patent_app_number] => 12/067931 [patent_app_country] => US [patent_app_date] => 2006-09-13 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 5 [patent_figures_cnt] => 5 [patent_no_of_words] => 2437 [patent_no_of_claims] => 11 [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/A1/0230/20080230651.pdf [firstpage_image] =>[orig_patent_app_number] => 12067931 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 199804 [patent_doc_number] => 07631503 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2009-12-15 [patent_title] => 'Combustor with enhanced cooling access' [patent_app_type] => utility [patent_app_number] => 11/518876 [patent_app_country] => US [patent_app_date] => 2006-09-12 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 4 [patent_figures_cnt] => 5 [patent_no_of_words] => 1535 [patent_no_of_claims] => 6 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 109 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/07/631/07631503.pdf [firstpage_image] =>[orig_patent_app_number] => 11518876 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 4700821 [patent_doc_number] => 20080060343 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2008-03-13 [patent_title] => 'Asymmetric serrated nozzle for exhaust noise reduction' [patent_app_type] => utility [patent_app_number] => 11/519606 [patent_app_country] => US [patent_app_date] => 2006-09-12 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 6 [patent_figures_cnt] => 6 [patent_no_of_words] => 4556 [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/A1/0060/20080060343.pdf [firstpage_image] =>[orig_patent_app_number] => 11519606 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 5234137 [patent_doc_number] => 20070126292 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2007-06-07 [patent_title] => 'Advanced hypersonic magnetic jet/electric turbine engine (AHMJET)' [patent_app_type] => utility [patent_app_number] => 11/518276 [patent_app_country] => US [patent_app_date] => 2006-09-11 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 13 [patent_figures_cnt] => 13 [patent_no_of_words] => 16471 [patent_no_of_claims] => 36 [patent_no_of_ind_claims] => 10 [patent_words_short_claim] => 0 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] => publications/A1/0126/20070126292.pdf [firstpage_image] =>[orig_patent_app_number] => 11518276 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 4767448 [patent_doc_number] => 20080053102 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2008-03-06 [patent_title] => 'METHOD AND APPARATUS FOR COOLING GAS TURBINE ENGINE COMBUSTORS' [patent_app_type] => utility [patent_app_number] => 11/468486 [patent_app_country] => US [patent_app_date] => 2006-08-30 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 7 [patent_figures_cnt] => 7 [patent_no_of_words] => 4320 [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/A1/0053/20080053102.pdf [firstpage_image] =>[orig_patent_app_number] => 11468486 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 6497014 [patent_doc_number] => 20100218482 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2010-09-02 [patent_title] => 'SYSTEM AND METHOD FOR COOLING ROCKET ENGINES' [patent_app_type] => utility [patent_app_number] => 11/509905 [patent_app_country] => US [patent_app_date] => 2006-08-25 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 8 [patent_figures_cnt] => 8 [patent_no_of_words] => 4072 [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/A1/0218/20100218482.pdf [firstpage_image] =>[orig_patent_app_number] => 11509905 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 148352 [patent_doc_number] => 07681401 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2010-03-23 [patent_title] => 'Methods and systems for operating a gas turbine' [patent_app_type] => utility [patent_app_number] => 11/467016 [patent_app_country] => US [patent_app_date] => 2006-08-24 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 3 [patent_figures_cnt] => 3 [patent_no_of_words] => 2746 [patent_no_of_claims] => 20 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 149 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/07/681/07681401.pdf [firstpage_image] =>[orig_patent_app_number] => 11467016 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 4637800 [patent_doc_number] => 08015823 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2011-09-13 [patent_title] => 'Endothermic cracking aircraft fuel system' [patent_app_type] => utility [patent_app_number] => 11/507382 [patent_app_country] => US [patent_app_date] => 2006-08-21 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 1 [patent_figures_cnt] => 2 [patent_no_of_words] => 3866 [patent_no_of_claims] => 14 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 140 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/08/015/08015823.pdf [firstpage_image] =>[orig_patent_app_number] => 11507382 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 4666001 [patent_doc_number] => 20080041061 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2008-02-21 [patent_title] => 'Multiple vane variable geometry nozzle' [patent_app_type] => utility [patent_app_number] => 11/506242 [patent_app_country] => US [patent_app_date] => 2006-08-18 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 12 [patent_figures_cnt] => 12 [patent_no_of_words] => 4981 [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/A1/0041/20080041061.pdf [firstpage_image] =>[orig_patent_app_number] => 11506242 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 7521783 [patent_doc_number] => 08024934 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2011-09-27 [patent_title] => 'System and method for attenuating combustion oscillations in a gas turbine engine' [patent_app_type] => utility [patent_app_number] => 11/506328 [patent_app_country] => US [patent_app_date] => 2006-08-18 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 7 [patent_figures_cnt] => 7 [patent_no_of_words] => 2850 [patent_no_of_claims] => 7 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 117 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/08/024/08024934.pdf [firstpage_image] =>[orig_patent_app_number] => 11506328 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 10197 [patent_doc_number] => 07805925 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2010-10-05 [patent_title] => 'Gas turbine engine exhaust duct ventilation' [patent_app_type] => utility [patent_app_number] => 11/465670 [patent_app_country] => US [patent_app_date] => 2006-08-18 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 4 [patent_figures_cnt] => 5 [patent_no_of_words] => 2913 [patent_no_of_claims] => 19 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 180 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/07/805/07805925.pdf [firstpage_image] =>[orig_patent_app_number] => 11465670 [rel_patent_id] =>[rel_patent_doc_number] =>)