Search

Hasanul Mobin

Examiner (ID: 17357, Phone: (571)270-1289 , Office: P/2168 )

Most Active Art Unit
2168
Art Unit(s)
2168, 2169
Total Applications
792
Issued Applications
570
Pending Applications
54
Abandoned Applications
186

Applications

Application numberTitle of the applicationFiling DateStatus
Array ( [id] => 6384518 [patent_doc_number] => 20100162714 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2010-07-01 [patent_title] => 'FUEL NOZZLE WITH SWIRLER VANES' [patent_app_type] => utility [patent_app_number] => 12/636487 [patent_app_country] => US [patent_app_date] => 2009-12-11 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 3 [patent_figures_cnt] => 3 [patent_no_of_words] => 3585 [patent_no_of_claims] => 20 [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/A1/0162/20100162714.pdf [firstpage_image] =>[orig_patent_app_number] => 12636487 [rel_patent_id] =>[rel_patent_doc_number] =>)
12/636487
FUEL NOZZLE WITH SWIRLER VANES Dec 10, 2009 Abandoned
Array ( [id] => 8800560 [patent_doc_number] => 08438828 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2013-05-14 [patent_title] => 'Flow divider having breaking points for a fan engine' [patent_app_type] => utility [patent_app_number] => 12/631521 [patent_app_country] => US [patent_app_date] => 2009-12-04 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 2 [patent_figures_cnt] => 5 [patent_no_of_words] => 2243 [patent_no_of_claims] => 25 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 138 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 12631521 [rel_patent_id] =>[rel_patent_doc_number] =>)
12/631521
Flow divider having breaking points for a fan engine Dec 3, 2009 Issued
Array ( [id] => 6198606 [patent_doc_number] => 20110061392 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2011-03-17 [patent_title] => 'COMBUSTION CAVITY LAYOUTS FOR FUEL STAGING IN TRAPPED VORTEX COMBUSTORS' [patent_app_type] => utility [patent_app_number] => 12/627852 [patent_app_country] => US [patent_app_date] => 2009-11-30 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 10 [patent_figures_cnt] => 10 [patent_no_of_words] => 7322 [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/A1/0061/20110061392.pdf [firstpage_image] =>[orig_patent_app_number] => 12627852 [rel_patent_id] =>[rel_patent_doc_number] =>)
12/627852
Combustion cavity layouts for fuel staging in trapped vortex combustors Nov 29, 2009 Issued
Array ( [id] => 6198605 [patent_doc_number] => 20110061391 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2011-03-17 [patent_title] => 'VORTEX PREMIXER FOR COMBUSTION APPARATUS' [patent_app_type] => utility [patent_app_number] => 12/627766 [patent_app_country] => US [patent_app_date] => 2009-11-30 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 10 [patent_figures_cnt] => 10 [patent_no_of_words] => 7325 [patent_no_of_claims] => 13 [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/A1/0061/20110061391.pdf [firstpage_image] =>[orig_patent_app_number] => 12627766 [rel_patent_id] =>[rel_patent_doc_number] =>)
12/627766
Vortex premixer for combustion apparatus Nov 29, 2009 Issued
Array ( [id] => 10002189 [patent_doc_number] => 09046272 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2015-06-02 [patent_title] => 'Combustion liner assembly having a mount stake coupled to an upstream support' [patent_app_type] => utility [patent_app_number] => 12/625349 [patent_app_country] => US [patent_app_date] => 2009-11-24 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 3 [patent_figures_cnt] => 3 [patent_no_of_words] => 3596 [patent_no_of_claims] => 19 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 161 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 12625349 [rel_patent_id] =>[rel_patent_doc_number] =>)
12/625349
Combustion liner assembly having a mount stake coupled to an upstream support Nov 23, 2009 Issued
Array ( [id] => 6482680 [patent_doc_number] => 20100199626 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2010-08-12 [patent_title] => 'TURBINE ENGINE EXHAUST GAS TUBE MIXER' [patent_app_type] => utility [patent_app_number] => 12/623987 [patent_app_country] => US [patent_app_date] => 2009-11-23 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 7 [patent_figures_cnt] => 7 [patent_no_of_words] => 2848 [patent_no_of_claims] => 22 [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/A1/0199/20100199626.pdf [firstpage_image] =>[orig_patent_app_number] => 12623987 [rel_patent_id] =>[rel_patent_doc_number] =>)
12/623987
TURBINE ENGINE EXHAUST GAS TUBE MIXER Nov 22, 2009 Abandoned
Array ( [id] => 9298062 [patent_doc_number] => 08646276 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2014-02-11 [patent_title] => 'Combustor assembly for a turbine engine with enhanced cooling' [patent_app_type] => utility [patent_app_number] => 12/616304 [patent_app_country] => US [patent_app_date] => 2009-11-11 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 10 [patent_figures_cnt] => 10 [patent_no_of_words] => 2518 [patent_no_of_claims] => 14 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 160 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 12616304 [rel_patent_id] =>[rel_patent_doc_number] =>)
12/616304
Combustor assembly for a turbine engine with enhanced cooling Nov 10, 2009 Issued
Array ( [id] => 6049540 [patent_doc_number] => 20110107768 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2011-05-12 [patent_title] => 'Variable Performance Valve' [patent_app_type] => utility [patent_app_number] => 12/614567 [patent_app_country] => US [patent_app_date] => 2009-11-09 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 4 [patent_figures_cnt] => 4 [patent_no_of_words] => 3229 [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/A1/0107/20110107768.pdf [firstpage_image] =>[orig_patent_app_number] => 12614567 [rel_patent_id] =>[rel_patent_doc_number] =>)
12/614567
Variable performance valve of a fuel nozzle for a turbine engine Nov 8, 2009 Issued
Array ( [id] => 6049537 [patent_doc_number] => 20110107767 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2011-05-12 [patent_title] => 'SECONDARY FUEL NOZZLE VENTURI' [patent_app_type] => utility [patent_app_number] => 12/613583 [patent_app_country] => US [patent_app_date] => 2009-11-06 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 4 [patent_figures_cnt] => 4 [patent_no_of_words] => 2112 [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/A1/0107/20110107767.pdf [firstpage_image] =>[orig_patent_app_number] => 12613583 [rel_patent_id] =>[rel_patent_doc_number] =>)
12/613583
SECONDARY FUEL NOZZLE VENTURI Nov 5, 2009 Abandoned
Array ( [id] => 5938494 [patent_doc_number] => 20110100015 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2011-05-05 [patent_title] => 'GAS TURBINE SYSTEM TO INHIBIT COKE FORMATION AND METHODS OF USE' [patent_app_type] => utility [patent_app_number] => 12/613011 [patent_app_country] => US [patent_app_date] => 2009-11-05 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 3 [patent_figures_cnt] => 3 [patent_no_of_words] => 6332 [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/A1/0100/20110100015.pdf [firstpage_image] =>[orig_patent_app_number] => 12613011 [rel_patent_id] =>[rel_patent_doc_number] =>)
12/613011
GAS TURBINE SYSTEM TO INHIBIT COKE FORMATION AND METHODS OF USE Nov 4, 2009 Abandoned
Array ( [id] => 6275659 [patent_doc_number] => 20100154383 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2010-06-24 [patent_title] => 'GAS TURBINE ENGINE' [patent_app_type] => utility [patent_app_number] => 12/582339 [patent_app_country] => US [patent_app_date] => 2009-10-20 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 4 [patent_figures_cnt] => 4 [patent_no_of_words] => 2676 [patent_no_of_claims] => 39 [patent_no_of_ind_claims] => 16 [patent_words_short_claim] => 0 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] => publications/A1/0154/20100154383.pdf [firstpage_image] =>[orig_patent_app_number] => 12582339 [rel_patent_id] =>[rel_patent_doc_number] =>)
12/582339
Three spool gas turbine engine having a clutch and compressor bypass Oct 19, 2009 Issued
Array ( [id] => 9348889 [patent_doc_number] => 08667775 [patent_country] => US [patent_kind] => B1 [patent_issue_date] => 2014-03-11 [patent_title] => 'Reverse flow engine core having a ducted fan with integrated secondary flow blades' [patent_app_type] => utility [patent_app_number] => 12/536426 [patent_app_country] => US [patent_app_date] => 2009-08-05 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 9 [patent_figures_cnt] => 9 [patent_no_of_words] => 2907 [patent_no_of_claims] => 14 [patent_no_of_ind_claims] => 4 [patent_words_short_claim] => 83 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 12536426 [rel_patent_id] =>[rel_patent_doc_number] =>)
12/536426
Reverse flow engine core having a ducted fan with integrated secondary flow blades Aug 4, 2009 Issued
Array ( [id] => 5945661 [patent_doc_number] => 20110030375 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2011-02-10 [patent_title] => 'AERODYNAMIC PYLON FUEL INJECTOR SYSTEM FOR COMBUSTORS' [patent_app_type] => utility [patent_app_number] => 12/535313 [patent_app_country] => US [patent_app_date] => 2009-08-04 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 5 [patent_figures_cnt] => 5 [patent_no_of_words] => 2765 [patent_no_of_claims] => 22 [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/A1/0030/20110030375.pdf [firstpage_image] =>[orig_patent_app_number] => 12535313 [rel_patent_id] =>[rel_patent_doc_number] =>)
12/535313
Aerodynamic pylon fuel injector system for combustors Aug 3, 2009 Issued
Array ( [id] => 6213711 [patent_doc_number] => 20100050647 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2010-03-04 [patent_title] => 'Swirler for a fuel injector' [patent_app_type] => utility [patent_app_number] => 12/461021 [patent_app_country] => US [patent_app_date] => 2009-07-29 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 3 [patent_figures_cnt] => 3 [patent_no_of_words] => 4061 [patent_no_of_claims] => 22 [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/A1/0050/20100050647.pdf [firstpage_image] =>[orig_patent_app_number] => 12461021 [rel_patent_id] =>[rel_patent_doc_number] =>)
12/461021
Swirler for a fuel injector Jul 28, 2009 Issued
Array ( [id] => 6143368 [patent_doc_number] => 20110016878 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2011-01-27 [patent_title] => 'Systems and Methods for Gas Turbine Combustors' [patent_app_type] => utility [patent_app_number] => 12/508918 [patent_app_country] => US [patent_app_date] => 2009-07-24 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 3 [patent_figures_cnt] => 3 [patent_no_of_words] => 1090 [patent_no_of_claims] => 18 [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/A1/0016/20110016878.pdf [firstpage_image] =>[orig_patent_app_number] => 12508918 [rel_patent_id] =>[rel_patent_doc_number] =>)
12/508918
System and method for a gas turbine combustor having a bleed duct from a diffuser to a fuel nozzle Jul 23, 2009 Issued
Array ( [id] => 6322349 [patent_doc_number] => 20100326079 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2010-12-30 [patent_title] => 'METHOD AND SYSTEM TO REDUCE VANE SWIRL ANGLE IN A GAS TURBINE ENGINE' [patent_app_type] => utility [patent_app_number] => 12/491393 [patent_app_country] => US [patent_app_date] => 2009-06-25 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 6 [patent_figures_cnt] => 6 [patent_no_of_words] => 2995 [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/A1/0326/20100326079.pdf [firstpage_image] =>[orig_patent_app_number] => 12491393 [rel_patent_id] =>[rel_patent_doc_number] =>)
12/491393
METHOD AND SYSTEM TO REDUCE VANE SWIRL ANGLE IN A GAS TURBINE ENGINE Jun 24, 2009 Abandoned
Array ( [id] => 8783054 [patent_doc_number] => 08429892 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2013-04-30 [patent_title] => 'Combustion apparatus having a fuel controlled valve that temporarily flows purging air' [patent_app_type] => utility [patent_app_number] => 12/476857 [patent_app_country] => US [patent_app_date] => 2009-06-02 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 4 [patent_figures_cnt] => 6 [patent_no_of_words] => 2335 [patent_no_of_claims] => 4 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 247 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 12476857 [rel_patent_id] =>[rel_patent_doc_number] =>)
12/476857
Combustion apparatus having a fuel controlled valve that temporarily flows purging air Jun 1, 2009 Issued
Array ( [id] => 6252716 [patent_doc_number] => 20100293952 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2010-11-25 [patent_title] => 'Resonating Swirler' [patent_app_type] => utility [patent_app_number] => 12/469858 [patent_app_country] => US [patent_app_date] => 2009-05-21 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 5 [patent_figures_cnt] => 5 [patent_no_of_words] => 1643 [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/A1/0293/20100293952.pdf [firstpage_image] =>[orig_patent_app_number] => 12469858 [rel_patent_id] =>[rel_patent_doc_number] =>)
12/469858
Resonating Swirler May 20, 2009 Abandoned
Array ( [id] => 6444779 [patent_doc_number] => 20100089019 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2010-04-15 [patent_title] => 'GAS TURBINE ENGINE' [patent_app_type] => utility [patent_app_number] => 12/468978 [patent_app_country] => US [patent_app_date] => 2009-05-20 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 5 [patent_figures_cnt] => 5 [patent_no_of_words] => 3433 [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/A1/0089/20100089019.pdf [firstpage_image] =>[orig_patent_app_number] => 12468978 [rel_patent_id] =>[rel_patent_doc_number] =>)
12/468978
GAS TURBINE ENGINE May 19, 2009 Abandoned
Array ( [id] => 9243293 [patent_doc_number] => 08607568 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2013-12-17 [patent_title] => 'Dry low NOx combustion system with pre-mixed direct-injection secondary fuel nozzle' [patent_app_type] => utility [patent_app_number] => 12/465805 [patent_app_country] => US [patent_app_date] => 2009-05-14 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 4 [patent_figures_cnt] => 4 [patent_no_of_words] => 4962 [patent_no_of_claims] => 13 [patent_no_of_ind_claims] => 4 [patent_words_short_claim] => 16 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 12465805 [rel_patent_id] =>[rel_patent_doc_number] =>)
12/465805
Dry low NOx combustion system with pre-mixed direct-injection secondary fuel nozzle May 13, 2009 Issued
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