Hasanul Mobin

Array ( [id] => 6549269 [patent_doc_number] => 20100058767 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2010-03-11 [patent_title] => 'SWIRL ANGLE OF SECONDARY FUEL NOZZLE FOR TURBOMACHINE COMBUSTOR' [patent_app_type] => utility [patent_app_number] => 12/205503 [patent_app_country] => US [patent_app_date] => 2008-09-05 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 4 [patent_figures_cnt] => 4 [patent_no_of_words] => 1680 [patent_no_of_claims] => 16 [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/A1/0058/20100058767.pdf [firstpage_image] =>[orig_patent_app_number] => 12205503 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 5448618 [patent_doc_number] => 20090064653 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2009-03-12 [patent_title] => 'PARTIAL LOAD COMBUSTION CYCLES' [patent_app_type] => utility [patent_app_number] => 12/202964 [patent_app_country] => US [patent_app_date] => 2008-09-02 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 6 [patent_figures_cnt] => 6 [patent_no_of_words] => 10912 [patent_no_of_claims] => 24 [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/A1/0064/20090064653.pdf [firstpage_image] =>[orig_patent_app_number] => 12202964 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 6213704 [patent_doc_number] => 20100050640 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2010-03-04 [patent_title] => 'THERMALLY COMPLIANT COMBUSTION CAP DEVICE AND SYSTEM' [patent_app_type] => utility [patent_app_number] => 12/201585 [patent_app_country] => US [patent_app_date] => 2008-08-29 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 10 [patent_figures_cnt] => 10 [patent_no_of_words] => 2469 [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/A1/0050/20100050640.pdf [firstpage_image] =>[orig_patent_app_number] => 12201585 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 6213715 [patent_doc_number] => 20100050651 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2010-03-04 [patent_title] => 'Variable Slope Exhaust Nozzle' [patent_app_type] => utility [patent_app_number] => 12/198959 [patent_app_country] => US [patent_app_date] => 2008-08-27 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 5 [patent_figures_cnt] => 5 [patent_no_of_words] => 4832 [patent_no_of_claims] => 28 [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/A1/0050/20100050651.pdf [firstpage_image] =>[orig_patent_app_number] => 12198959 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 6528723 [patent_doc_number] => 20100043442 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2010-02-25 [patent_title] => 'DIMPLED SERRATED FINTUBE STRUCTURE' [patent_app_type] => utility [patent_app_number] => 12/193800 [patent_app_country] => US [patent_app_date] => 2008-08-19 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 4 [patent_figures_cnt] => 4 [patent_no_of_words] => 1946 [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/A1/0043/20100043442.pdf [firstpage_image] =>[orig_patent_app_number] => 12193800 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 6369196 [patent_doc_number] => 20100300111 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2010-12-02 [patent_title] => 'METHOD FOR THE OPERATION OF A POWER PLANT FEATURING INTEGRATED GASIFICATION, AND POWER PLANT' [patent_app_type] => utility [patent_app_number] => 12/675146 [patent_app_country] => US [patent_app_date] => 2008-08-18 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 3 [patent_figures_cnt] => 3 [patent_no_of_words] => 2977 [patent_no_of_claims] => 21 [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/A1/0300/20100300111.pdf [firstpage_image] =>[orig_patent_app_number] => 12675146 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 6437351 [patent_doc_number] => 20100037618 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2010-02-18 [patent_title] => 'TRANSITION WITH A LINEAR FLOW PATH FOR USE IN A GAS TURBINE ENGINE' [patent_app_type] => utility [patent_app_number] => 12/190074 [patent_app_country] => US [patent_app_date] => 2008-08-12 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 7 [patent_figures_cnt] => 7 [patent_no_of_words] => 5245 [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/A1/0037/20100037618.pdf [firstpage_image] =>[orig_patent_app_number] => 12190074 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 6437359 [patent_doc_number] => 20100037619 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2010-02-18 [patent_title] => 'CANTED OUTLET FOR TRANSITION IN A GAS TURBINE ENGINE' [patent_app_type] => utility [patent_app_number] => 12/190092 [patent_app_country] => US [patent_app_date] => 2008-08-12 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 4 [patent_figures_cnt] => 4 [patent_no_of_words] => 4917 [patent_no_of_claims] => 21 [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/A1/0037/20100037619.pdf [firstpage_image] =>[orig_patent_app_number] => 12190092 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 7736224 [patent_doc_number] => 08104264 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2012-01-31 [patent_title] => 'Low minimum impulse bit propellant gas thruster' [patent_app_type] => utility [patent_app_number] => 12/189642 [patent_app_country] => US [patent_app_date] => 2008-08-11 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 3 [patent_figures_cnt] => 5 [patent_no_of_words] => 4732 [patent_no_of_claims] => 18 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 361 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/08/104/08104264.pdf [firstpage_image] =>[orig_patent_app_number] => 12189642 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 5424799 [patent_doc_number] => 20090084109 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2009-04-02 [patent_title] => 'Fuel nozzle of gas turbine combustor for DME and design method thereof' [patent_app_type] => utility [patent_app_number] => 12/215159 [patent_app_country] => US [patent_app_date] => 2008-06-25 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 3 [patent_figures_cnt] => 3 [patent_no_of_words] => 1830 [patent_no_of_claims] => 3 [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/A1/0084/20090084109.pdf [firstpage_image] =>[orig_patent_app_number] => 12215159 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 5393937 [patent_doc_number] => 20090313999 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2009-12-24 [patent_title] => 'METHOD AND APPARATUS FOR CONTROLLING FUEL IN A GAS TURBINE ENGINE' [patent_app_type] => utility [patent_app_number] => 12/120034 [patent_app_country] => US [patent_app_date] => 2008-05-13 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 5 [patent_figures_cnt] => 5 [patent_no_of_words] => 3435 [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/A1/0313/20090313999.pdf [firstpage_image] =>[orig_patent_app_number] => 12120034 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 6528739 [patent_doc_number] => 20100043443 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2010-02-25 [patent_title] => 'METHOD AND APPARATUS FOR SUPPRESSING AEROENGINE CONTRAILS' [patent_app_type] => utility [patent_app_number] => 12/450691 [patent_app_country] => US [patent_app_date] => 2008-04-28 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 3 [patent_figures_cnt] => 3 [patent_no_of_words] => 2666 [patent_no_of_claims] => 19 [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/A1/0043/20100043443.pdf [firstpage_image] =>[orig_patent_app_number] => 12450691 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 5560556 [patent_doc_number] => 20090133408 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2009-05-28 [patent_title] => 'Re-pressurisation device' [patent_app_type] => utility [patent_app_number] => 12/081655 [patent_app_country] => US [patent_app_date] => 2008-04-18 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 3 [patent_figures_cnt] => 3 [patent_no_of_words] => 2576 [patent_no_of_claims] => 15 [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/A1/0133/20090133408.pdf [firstpage_image] =>[orig_patent_app_number] => 12081655 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 6376594 [patent_doc_number] => 20100175381 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2010-07-15 [patent_title] => 'SWIRLER' [patent_app_type] => utility [patent_app_number] => 12/597261 [patent_app_country] => US [patent_app_date] => 2008-04-17 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 3 [patent_figures_cnt] => 3 [patent_no_of_words] => 1191 [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/A1/0175/20100175381.pdf [firstpage_image] =>[orig_patent_app_number] => 12597261 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 5492315 [patent_doc_number] => 20090260343 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2009-10-22 [patent_title] => 'SOLID PROPELLANT MANAGEMENT CONTROL SYSTEM AND METHOD' [patent_app_type] => utility [patent_app_number] => 12/105099 [patent_app_country] => US [patent_app_date] => 2008-04-17 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 3 [patent_figures_cnt] => 3 [patent_no_of_words] => 2961 [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/A1/0260/20090260343.pdf [firstpage_image] =>[orig_patent_app_number] => 12105099 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 6392481 [patent_doc_number] => 20100146933 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2010-06-17 [patent_title] => 'NACELLE REAR ASSEMBLY FOR TURBOJET ENGINE' [patent_app_type] => utility [patent_app_number] => 12/601049 [patent_app_country] => US [patent_app_date] => 2008-03-28 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 4 [patent_figures_cnt] => 4 [patent_no_of_words] => 3604 [patent_no_of_claims] => 12 [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/A1/0146/20100146933.pdf [firstpage_image] =>[orig_patent_app_number] => 12601049 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 6585848 [patent_doc_number] => 20100031631 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2010-02-11 [patent_title] => 'GAS TURBINE COMPRISING A GUIDE RING AND A MIXER' [patent_app_type] => utility [patent_app_number] => 12/525158 [patent_app_country] => US [patent_app_date] => 2008-01-26 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 3 [patent_figures_cnt] => 3 [patent_no_of_words] => 1653 [patent_no_of_claims] => 9 [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/A1/0031/20100031631.pdf [firstpage_image] =>[orig_patent_app_number] => 12525158 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 6586336 [patent_doc_number] => 20100031673 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2010-02-11 [patent_title] => 'CASING OF A GAS TURBINE ENGINE' [patent_app_type] => utility [patent_app_number] => 12/524766 [patent_app_country] => US [patent_app_date] => 2008-01-25 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 5 [patent_figures_cnt] => 5 [patent_no_of_words] => 2169 [patent_no_of_claims] => 21 [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/A1/0031/20100031673.pdf [firstpage_image] =>[orig_patent_app_number] => 12524766 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 9125005 [patent_doc_number] => 08572944 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2013-11-05 [patent_title] => 'Prime mover for an exhaust gas recirculation system' [patent_app_type] => utility [patent_app_number] => 11/960198 [patent_app_country] => US [patent_app_date] => 2007-12-19 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 4 [patent_figures_cnt] => 4 [patent_no_of_words] => 3827 [patent_no_of_claims] => 14 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 217 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 11960198 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 9164616 [patent_doc_number] => 08590286 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2013-11-26 [patent_title] => 'Gas turbine engine systems involving tip fans' [patent_app_type] => utility [patent_app_number] => 11/950614 [patent_app_country] => US [patent_app_date] => 2007-12-05 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 2 [patent_figures_cnt] => 2 [patent_no_of_words] => 2461 [patent_no_of_claims] => 16 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 199 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 11950614 [rel_patent_id] =>[rel_patent_doc_number] =>)