
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] => 9782001
[patent_doc_number] => 20140298820
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2014-10-09
[patent_title] => 'GAS TURBINE ENGINE AND METHOD FOR STARTING SAME'
[patent_app_type] => utility
[patent_app_number] => 14/307954
[patent_app_country] => US
[patent_app_date] => 2014-06-18
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
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Array
(
[id] => 9830168
[patent_doc_number] => 08938974
[patent_country] => US
[patent_kind] => B1
[patent_issue_date] => 2015-01-27
[patent_title] => 'Method for determining optimum injector inlet geometry'
[patent_app_type] => utility
[patent_app_number] => 14/282890
[patent_app_country] => US
[patent_app_date] => 2014-05-20
[patent_effective_date] => 0000-00-00
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[rel_patent_id] =>[rel_patent_doc_number] =>) 14/282890 | Method for determining optimum injector inlet geometry | May 19, 2014 | Issued |
Array
(
[id] => 9487127
[patent_doc_number] => 20140137534
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2014-05-22
[patent_title] => 'INTERNALLY COOLED SPOKE'
[patent_app_type] => utility
[patent_app_number] => 14/166320
[patent_app_country] => US
[patent_app_date] => 2014-01-28
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
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[rel_patent_id] =>[rel_patent_doc_number] =>) 14/166320 | INTERNALLY COOLED SPOKE | Jan 27, 2014 | Abandoned |
Array
(
[id] => 10868322
[patent_doc_number] => 08893511
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2014-11-25
[patent_title] => 'Systems and methods for a gas turbine combustor having a bleed duct'
[patent_app_type] => utility
[patent_app_number] => 13/909297
[patent_app_country] => US
[patent_app_date] => 2013-06-04
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 2
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[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13909297
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/909297 | Systems and methods for a gas turbine combustor having a bleed duct | Jun 3, 2013 | Issued |
Array
(
[id] => 8894729
[patent_doc_number] => 08474240
[patent_country] => US
[patent_kind] => B1
[patent_issue_date] => 2013-07-02
[patent_title] => 'Regenerative gas generator'
[patent_app_type] => utility
[patent_app_number] => 13/706345
[patent_app_country] => US
[patent_app_date] => 2012-12-05
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[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13706345
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/706345 | Regenerative gas generator | Dec 4, 2012 | Issued |
Array
(
[id] => 10071192
[patent_doc_number] => 09109540
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2015-08-18
[patent_title] => 'Airplane jet engine thrust reverser having gratings or cascades'
[patent_app_type] => utility
[patent_app_number] => 13/681210
[patent_app_country] => US
[patent_app_date] => 2012-11-19
[patent_effective_date] => 0000-00-00
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[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13681210
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/681210 | Airplane jet engine thrust reverser having gratings or cascades | Nov 18, 2012 | Issued |
Array
(
[id] => 8614272
[patent_doc_number] => 20130019584
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2013-01-24
[patent_title] => 'BURNER, GAS TURBINE COMBUSTOR, BURNER COOLING METHOD, AND BURNER MODIFYING METHOD'
[patent_app_type] => utility
[patent_app_number] => 13/627565
[patent_app_country] => US
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[patent_effective_date] => 0000-00-00
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[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13627565
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/627565 | BURNER, GAS TURBINE COMBUSTOR, BURNER COOLING METHOD, AND BURNER MODIFYING METHOD | Sep 25, 2012 | Abandoned |
Array
(
[id] => 9572955
[patent_doc_number] => 08763362
[patent_country] => US
[patent_kind] => B1
[patent_issue_date] => 2014-07-01
[patent_title] => 'Injector element which maintains a constant mean spray angle and optimum pressure drop during throttling by varying the geometry of tangential inlets'
[patent_app_type] => utility
[patent_app_number] => 13/452303
[patent_app_country] => US
[patent_app_date] => 2012-04-20
[patent_effective_date] => 0000-00-00
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[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13452303
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/452303 | Injector element which maintains a constant mean spray angle and optimum pressure drop during throttling by varying the geometry of tangential inlets | Apr 19, 2012 | Issued |
Array
(
[id] => 8332148
[patent_doc_number] => 20120198851
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2012-08-09
[patent_title] => 'TRAVERSING FUEL NOZZLES IN CAP-LESS COMBUSTOR ASSEMBLY'
[patent_app_type] => utility
[patent_app_number] => 13/449904
[patent_app_country] => US
[patent_app_date] => 2012-04-18
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[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13449904
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/449904 | Traversing fuel nozzles in cap-less combustor assembly | Apr 17, 2012 | Issued |
Array
(
[id] => 8992915
[patent_doc_number] => 08516787
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2013-08-27
[patent_title] => 'Combined-cycle power plant having a once-through cooler'
[patent_app_type] => utility
[patent_app_number] => 13/408140
[patent_app_country] => US
[patent_app_date] => 2012-02-29
[patent_effective_date] => 0000-00-00
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[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13408140
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/408140 | Combined-cycle power plant having a once-through cooler | Feb 28, 2012 | Issued |
Array
(
[id] => 10629228
[patent_doc_number] => 09347374
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2016-05-24
[patent_title] => 'Gas turbine engine buffer cooling system'
[patent_app_type] => utility
[patent_app_number] => 13/405514
[patent_app_country] => US
[patent_app_date] => 2012-02-27
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[rel_patent_id] =>[rel_patent_doc_number] =>) 13/405514 | Gas turbine engine buffer cooling system | Feb 26, 2012 | Issued |
Array
(
[id] => 10595039
[patent_doc_number] => 09316117
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2016-04-19
[patent_title] => 'Internally cooled spoke'
[patent_app_type] => utility
[patent_app_number] => 13/361480
[patent_app_country] => US
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[rel_patent_id] =>[rel_patent_doc_number] =>) 13/361480 | Internally cooled spoke | Jan 29, 2012 | Issued |
Array
(
[id] => 10542319
[patent_doc_number] => 09267434
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2016-02-23
[patent_title] => 'Heat exchanger'
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[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13360745
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/360745 | Heat exchanger | Jan 28, 2012 | Issued |
Array
(
[id] => 8924492
[patent_doc_number] => 20130180252
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2013-07-18
[patent_title] => 'COMBUSTOR ASSEMBLY WITH IMPINGEMENT SLEEVE HOLES AND TURBULATORS'
[patent_app_type] => utility
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[rel_patent_id] =>[rel_patent_doc_number] =>) 13/353071 | COMBUSTOR ASSEMBLY WITH IMPINGEMENT SLEEVE HOLES AND TURBULATORS | Jan 17, 2012 | Abandoned |
Array
(
[id] => 10516466
[patent_doc_number] => 09243507
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2016-01-26
[patent_title] => 'Late lean injection system transition piece'
[patent_app_type] => utility
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Array
(
[id] => 8900039
[patent_doc_number] => 20130167542
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2013-07-04
[patent_title] => 'FLOWSLEEVE OF A TURBOMACHINE COMPONENT'
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[rel_patent_id] =>[rel_patent_doc_number] =>) 13/343200 | Flowsleeve of a turbomachine component | Jan 3, 2012 | Issued |
Array
(
[id] => 8260495
[patent_doc_number] => 20120159922
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2012-06-28
[patent_title] => 'TOP CYCLE POWER GENERATION WITH HIGH RADIANT AND EMISSIVITY EXHAUST'
[patent_app_type] => utility
[patent_app_number] => 13/337019
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[rel_patent_id] =>[rel_patent_doc_number] =>) 13/337019 | TOP CYCLE POWER GENERATION WITH HIGH RADIANT AND EMISSIVITY EXHAUST | Dec 22, 2011 | Abandoned |
Array
(
[id] => 8728946
[patent_doc_number] => 20130074515
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2013-03-28
[patent_title] => 'GAS TURBINE ENGINE SYSTEM AND METHOD OF PROVIDING A FUEL SUPPLIED TO ONE OR MORE COMBUSTORS IN A GAS TURBINE ENGINE SYSTEM'
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Array
(
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Array
(
[id] => 8389564
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[rel_patent_id] =>[rel_patent_doc_number] =>) 13/235125 | SYSTEMS AND METHODS OF PRESSURE DROP CONTROL IN FLUID CIRCUITS THROUGH SWIRLING FLOW MITIGATION | Sep 15, 2011 | Abandoned |