
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 number | Title of the application | Filing Date | Status |
|---|---|---|---|
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
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[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
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[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
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[patent_no_of_words] => 2112
[patent_no_of_claims] => 20
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[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
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[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
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[patent_no_of_words] => 2676
[patent_no_of_claims] => 39
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[patent_maintenance] => 1
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[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
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[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
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[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
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[patent_no_of_words] => 4061
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[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
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[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
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[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
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[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
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[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
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[patent_title] => 'GAS TURBINE ENGINE'
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[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
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[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 |