
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] => 8268488
[patent_doc_number] => 08209986
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2012-07-03
[patent_title] => 'Multi-tube thermal fuse for nozzle protection from a flame holding or flashback event'
[patent_app_type] => utility
[patent_app_number] => 12/260451
[patent_app_country] => US
[patent_app_date] => 2008-10-29
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 11
[patent_figures_cnt] => 13
[patent_no_of_words] => 5399
[patent_no_of_claims] => 17
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 222
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 12260451
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/260451 | Multi-tube thermal fuse for nozzle protection from a flame holding or flashback event | Oct 28, 2008 | Issued |
Array
(
[id] => 5326671
[patent_doc_number] => 20090107148
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2009-04-30
[patent_title] => 'ANNULAR COMBUSTION CHAMBER OF A GAS TURBINE ENGINE'
[patent_app_type] => utility
[patent_app_number] => 12/259714
[patent_app_country] => US
[patent_app_date] => 2008-10-28
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 3
[patent_no_of_words] => 2648
[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/A1/0107/20090107148.pdf
[firstpage_image] =>[orig_patent_app_number] => 12259714
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/259714 | Annular combustion chamber of a gas turbine engine | Oct 27, 2008 | Issued |
Array
(
[id] => 6417138
[patent_doc_number] => 20100101543
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2010-04-29
[patent_title] => 'SYSTEM AND METHOD FOR HEATING A FUEL USING AN EXHAUST GAS RECIRCULATION SYSTEM'
[patent_app_type] => utility
[patent_app_number] => 12/258670
[patent_app_country] => US
[patent_app_date] => 2008-10-27
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 3
[patent_no_of_words] => 2919
[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/A1/0101/20100101543.pdf
[firstpage_image] =>[orig_patent_app_number] => 12258670
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/258670 | System and method for heating a fuel using an exhaust gas recirculation system | Oct 26, 2008 | Issued |
Array
(
[id] => 6563812
[patent_doc_number] => 20100095679
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2010-04-22
[patent_title] => 'DUAL WALL STRUCTURE FOR USE IN A COMBUSTOR OF A GAS TURBINE ENGINE'
[patent_app_type] => utility
[patent_app_number] => 12/256226
[patent_app_country] => US
[patent_app_date] => 2008-10-22
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 7
[patent_figures_cnt] => 7
[patent_no_of_words] => 4932
[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/A1/0095/20100095679.pdf
[firstpage_image] =>[orig_patent_app_number] => 12256226
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/256226 | DUAL WALL STRUCTURE FOR USE IN A COMBUSTOR OF A GAS TURBINE ENGINE | Oct 21, 2008 | Abandoned |
Array
(
[id] => 5581637
[patent_doc_number] => 20090100839
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2009-04-23
[patent_title] => 'COMBUSTION CHAMBER WALL WITH OPTIMIZED DILUTION AND COOLING, AND COMBUSTION CHAMBER AND TURBOMACHINE BOTH PROVIDED THEREWITH'
[patent_app_type] => utility
[patent_app_number] => 12/255987
[patent_app_country] => US
[patent_app_date] => 2008-10-22
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
[patent_figures_cnt] => 5
[patent_no_of_words] => 3253
[patent_no_of_claims] => 5
[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/A1/0100/20090100839.pdf
[firstpage_image] =>[orig_patent_app_number] => 12255987
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/255987 | COMBUSTION CHAMBER WALL WITH OPTIMIZED DILUTION AND COOLING, AND COMBUSTION CHAMBER AND TURBOMACHINE BOTH PROVIDED THEREWITH | Oct 21, 2008 | Abandoned |
Array
(
[id] => 6563829
[patent_doc_number] => 20100095680
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2010-04-22
[patent_title] => 'DUAL WALL STRUCTURE FOR USE IN A COMBUSTOR OF A GAS TURBINE ENGINE'
[patent_app_type] => utility
[patent_app_number] => 12/256246
[patent_app_country] => US
[patent_app_date] => 2008-10-22
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 6
[patent_figures_cnt] => 6
[patent_no_of_words] => 3971
[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/A1/0095/20100095680.pdf
[firstpage_image] =>[orig_patent_app_number] => 12256246
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/256246 | DUAL WALL STRUCTURE FOR USE IN A COMBUSTOR OF A GAS TURBINE ENGINE | Oct 21, 2008 | Abandoned |
Array
(
[id] => 5535864
[patent_doc_number] => 20090217669
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2009-09-03
[patent_title] => 'Fuel nozzles'
[patent_app_type] => utility
[patent_app_number] => 12/289117
[patent_app_country] => US
[patent_app_date] => 2008-10-21
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
[patent_figures_cnt] => 5
[patent_no_of_words] => 3915
[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/A1/0217/20090217669.pdf
[firstpage_image] =>[orig_patent_app_number] => 12289117
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/289117 | Fuel nozzles | Oct 20, 2008 | Abandoned |
Array
(
[id] => 10886498
[patent_doc_number] => 08910483
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2014-12-16
[patent_title] => 'Lean premix burner for a gas-turbine engine'
[patent_app_type] => utility
[patent_app_number] => 12/289051
[patent_app_country] => US
[patent_app_date] => 2008-10-20
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 2
[patent_figures_cnt] => 2
[patent_no_of_words] => 2163
[patent_no_of_claims] => 19
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 395
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 12289051
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/289051 | Lean premix burner for a gas-turbine engine | Oct 19, 2008 | Issued |
Array
(
[id] => 6563432
[patent_doc_number] => 20100095648
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2010-04-22
[patent_title] => 'Combined Cycle Power Plant'
[patent_app_type] => utility
[patent_app_number] => 12/253435
[patent_app_country] => US
[patent_app_date] => 2008-10-17
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 3
[patent_no_of_words] => 1229
[patent_no_of_claims] => 10
[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/A1/0095/20100095648.pdf
[firstpage_image] =>[orig_patent_app_number] => 12253435
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/253435 | Combined Cycle Power Plant | Oct 16, 2008 | Abandoned |
Array
(
[id] => 6423091
[patent_doc_number] => 20100186411
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2010-07-29
[patent_title] => 'GAS TURBINE'
[patent_app_type] => utility
[patent_app_number] => 12/671046
[patent_app_country] => US
[patent_app_date] => 2008-10-17
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 9
[patent_figures_cnt] => 9
[patent_no_of_words] => 4400
[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/A1/0186/20100186411.pdf
[firstpage_image] =>[orig_patent_app_number] => 12671046
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/671046 | Gas turbine having a combustion oscillation suppressing device | Oct 16, 2008 | Issued |
Array
(
[id] => 7736270
[patent_doc_number] => 08104290
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2012-01-31
[patent_title] => 'Combustion liner damper'
[patent_app_type] => utility
[patent_app_number] => 12/251973
[patent_app_country] => US
[patent_app_date] => 2008-10-15
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 8
[patent_figures_cnt] => 8
[patent_no_of_words] => 2469
[patent_no_of_claims] => 5
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 205
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/08/104/08104290.pdf
[firstpage_image] =>[orig_patent_app_number] => 12251973
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/251973 | Combustion liner damper | Oct 14, 2008 | Issued |
Array
(
[id] => 6444781
[patent_doc_number] => 20100089020
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2010-04-15
[patent_title] => 'METERING OF DILUENT FLOW IN COMBUSTOR'
[patent_app_type] => utility
[patent_app_number] => 12/250933
[patent_app_country] => US
[patent_app_date] => 2008-10-14
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 9
[patent_figures_cnt] => 9
[patent_no_of_words] => 1826
[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/A1/0089/20100089020.pdf
[firstpage_image] =>[orig_patent_app_number] => 12250933
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/250933 | METERING OF DILUENT FLOW IN COMBUSTOR | Oct 13, 2008 | Abandoned |
Array
(
[id] => 6444798
[patent_doc_number] => 20100089021
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2010-04-15
[patent_title] => 'METHOD AND APPARATUS OF INTRODUCING DILUENT FLOW INTO A COMBUSTOR'
[patent_app_type] => utility
[patent_app_number] => 12/250995
[patent_app_country] => US
[patent_app_date] => 2008-10-14
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 11
[patent_figures_cnt] => 11
[patent_no_of_words] => 1977
[patent_no_of_claims] => 19
[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/A1/0089/20100089021.pdf
[firstpage_image] =>[orig_patent_app_number] => 12250995
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/250995 | Method and apparatus of introducing diluent flow into a combustor | Oct 13, 2008 | Issued |
Array
(
[id] => 6444801
[patent_doc_number] => 20100089022
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2010-04-15
[patent_title] => 'METHOD AND APPARATUS OF FUEL NOZZLE DILUENT INTRODUCTION'
[patent_app_type] => utility
[patent_app_number] => 12/251050
[patent_app_country] => US
[patent_app_date] => 2008-10-14
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
[patent_figures_cnt] => 5
[patent_no_of_words] => 1373
[patent_no_of_claims] => 15
[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/A1/0089/20100089022.pdf
[firstpage_image] =>[orig_patent_app_number] => 12251050
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/251050 | METHOD AND APPARATUS OF FUEL NOZZLE DILUENT INTRODUCTION | Oct 13, 2008 | Abandoned |
Array
(
[id] => 5406157
[patent_doc_number] => 20090120055
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2009-05-14
[patent_title] => 'METHOD AND APPARATUS FOR PROPELLING A VESSEL IN A ZERO GRAVITY ENVIRONMENT'
[patent_app_type] => utility
[patent_app_number] => 12/247211
[patent_app_country] => US
[patent_app_date] => 2008-10-07
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 7
[patent_figures_cnt] => 7
[patent_no_of_words] => 4400
[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/A1/0120/20090120055.pdf
[firstpage_image] =>[orig_patent_app_number] => 12247211
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/247211 | METHOD AND APPARATUS FOR PROPELLING A VESSEL IN A ZERO GRAVITY ENVIRONMENT | Oct 6, 2008 | Abandoned |
| 12/245343 | Liquid Propellant Injection Elements with Self-Adjusted Inlet Area for Rocket and Other Combustion-Type Engine Applications | Oct 2, 2008 | Abandoned |
Array
(
[id] => 6352692
[patent_doc_number] => 20100077762
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2010-04-01
[patent_title] => 'Off Center Combustor Liner'
[patent_app_type] => utility
[patent_app_number] => 12/243122
[patent_app_country] => US
[patent_app_date] => 2008-10-01
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 3
[patent_no_of_words] => 1500
[patent_no_of_claims] => 16
[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/A1/0077/20100077762.pdf
[firstpage_image] =>[orig_patent_app_number] => 12243122
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/243122 | Off center combustor liner | Sep 30, 2008 | Issued |
Array
(
[id] => 6352689
[patent_doc_number] => 20100077761
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2010-04-01
[patent_title] => 'IMPINGEMENT COOLED COMBUSTOR SEAL'
[patent_app_type] => utility
[patent_app_number] => 12/242013
[patent_app_country] => US
[patent_app_date] => 2008-09-30
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 6
[patent_figures_cnt] => 6
[patent_no_of_words] => 2285
[patent_no_of_claims] => 20
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[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0077/20100077761.pdf
[firstpage_image] =>[orig_patent_app_number] => 12242013
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/242013 | Impingement cooled combustor seal | Sep 29, 2008 | Issued |
Array
(
[id] => 9872665
[patent_doc_number] => 08959924
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2015-02-24
[patent_title] => 'Aircraft turbofan engine'
[patent_app_type] => utility
[patent_app_number] => 12/238089
[patent_app_country] => US
[patent_app_date] => 2008-09-25
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 4
[patent_no_of_words] => 2742
[patent_no_of_claims] => 4
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 555
[patent_maintenance] => 1
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[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 12238089
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/238089 | Aircraft turbofan engine | Sep 24, 2008 | Issued |
Array
(
[id] => 6549166
[patent_doc_number] => 20100058758
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2010-03-11
[patent_title] => 'EXHAUST GAS RECIRCULATION SYSTEM, TURBOMACHINE SYSTEM HAVING THE EXHAUST GAS RECIRCULATION SYSTEM AND EXHAUST GAS RECIRCULATION CONTROL METHOD'
[patent_app_type] => utility
[patent_app_number] => 12/208728
[patent_app_country] => US
[patent_app_date] => 2008-09-11
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 8
[patent_figures_cnt] => 8
[patent_no_of_words] => 3255
[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/A1/0058/20100058758.pdf
[firstpage_image] =>[orig_patent_app_number] => 12208728
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/208728 | Exhaust gas recirculation system, turbomachine system having the exhaust gas recirculation system and exhaust gas recirculation control method | Sep 10, 2008 | Issued |