
Jesus D. Sotelo
Examiner (ID: 4127)
| Most Active Art Unit | 3105 |
| Art Unit(s) | 3612, 3105, 3102, 2899, 3617, 0 |
| Total Applications | 3000 |
| Issued Applications | 2686 |
| Pending Applications | 74 |
| Abandoned Applications | 240 |
Applications
| Application number | Title of the application | Filing Date | Status |
|---|---|---|---|
Array
(
[id] => 10445622
[patent_doc_number] => 20150330636
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2015-11-19
[patent_title] => 'SYSTEM AND METHOD FOR CONTROL OF COMBUSTION DYNAMICS IN COMBUSTION SYSTEM'
[patent_app_type] => utility
[patent_app_number] => 14/276700
[patent_app_country] => US
[patent_app_date] => 2014-05-13
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[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14276700
[rel_patent_id] =>[rel_patent_doc_number] =>) 14/276700 | SYSTEM AND METHOD FOR CONTROL OF COMBUSTION DYNAMICS IN COMBUSTION SYSTEM | May 12, 2014 | Abandoned |
Array
(
[id] => 10437849
[patent_doc_number] => 20150322861
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2015-11-12
[patent_title] => 'Enhanced Turbine Cooling System Using a Blend of Compressor Bleed Air and Ambient Air'
[patent_app_type] => utility
[patent_app_number] => 14/274892
[patent_app_country] => US
[patent_app_date] => 2014-05-12
[patent_effective_date] => 0000-00-00
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Array
(
[id] => 9892978
[patent_doc_number] => 20150048177
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2015-02-19
[patent_title] => 'EXHAUST NOZZLE AND METHOD FOR CHANGING EXHAUST FLOW PATH'
[patent_app_type] => utility
[patent_app_number] => 14/271584
[patent_app_country] => US
[patent_app_date] => 2014-05-07
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[patent_drawing_sheets_cnt] => 8
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[rel_patent_id] =>[rel_patent_doc_number] =>) 14/271584 | Exhaust nozzle and method for changing exhaust flow path | May 6, 2014 | Issued |
Array
(
[id] => 10915116
[patent_doc_number] => 20140318135
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2014-10-30
[patent_title] => 'CAN COMBUSTOR FOR A CAN-ANNULAR COMBUSTOR ARRANGEMENT IN A GAS TURBINE'
[patent_app_type] => utility
[patent_app_number] => 14/260617
[patent_app_country] => US
[patent_app_date] => 2014-04-24
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 7
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[patent_no_of_words] => 3758
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[rel_patent_id] =>[rel_patent_doc_number] =>) 14/260617 | Can combustor for a can-annular combustor arrangement in a gas turbine | Apr 23, 2014 | Issued |
Array
(
[id] => 10908143
[patent_doc_number] => 20140311158
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2014-10-23
[patent_title] => 'HEAT AND POWER PLANT WITH A WASTE GASIFICATION SYSTEM'
[patent_app_type] => utility
[patent_app_number] => 14/251344
[patent_app_country] => US
[patent_app_date] => 2014-04-11
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 2
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[rel_patent_id] =>[rel_patent_doc_number] =>) 14/251344 | HEAT AND POWER PLANT WITH A WASTE GASIFICATION SYSTEM | Apr 10, 2014 | Abandoned |
Array
(
[id] => 10814962
[patent_doc_number] => 20160161122
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2016-06-09
[patent_title] => 'AIRBLAST NOZZLE WITH UPSTREAM FUEL DISTRIBUTION AND NEAR-EXIT SWIRL'
[patent_app_type] => utility
[patent_app_number] => 14/228574
[patent_app_country] => US
[patent_app_date] => 2014-03-28
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[rel_patent_id] =>[rel_patent_doc_number] =>) 14/228574 | Airblast nozzle with upstream fuel distribution and near-exit swirl | Mar 27, 2014 | Issued |
Array
(
[id] => 10814525
[patent_doc_number] => 20160160685
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2016-06-09
[patent_title] => 'ELIMINATIN OF UNFAVORABLE OUTFLOW MARGIN'
[patent_app_type] => utility
[patent_app_number] => 14/221494
[patent_app_country] => US
[patent_app_date] => 2014-03-21
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 7
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[rel_patent_id] =>[rel_patent_doc_number] =>) 14/221494 | Eliminatin of unfavorable outflow margin | Mar 20, 2014 | Issued |
Array
(
[id] => 10694407
[patent_doc_number] => 20160040552
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2016-02-11
[patent_title] => 'MODULATED TURBINE COOLING SYSTEM'
[patent_app_type] => utility
[patent_app_number] => 14/777331
[patent_app_country] => US
[patent_app_date] => 2014-03-14
[patent_effective_date] => 0000-00-00
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[rel_patent_id] =>[rel_patent_doc_number] =>) 14/777331 | Modulated turbine cooling system | Mar 13, 2014 | Issued |
Array
(
[id] => 13027871
[patent_doc_number] => 10036552
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2018-07-31
[patent_title] => Injection system for a combustion chamber of a turbine engine, comprising an annular wall having a convergent inner cross-section
[patent_app_type] => utility
[patent_app_number] => 14/778412
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Array
(
[id] => 9670227
[patent_doc_number] => 20140234090
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2014-08-21
[patent_title] => 'REAR NACELLE ASSEMBLY FOR A TURBOJET ENGINE'
[patent_app_type] => utility
[patent_app_number] => 14/200365
[patent_app_country] => US
[patent_app_date] => 2014-03-07
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[rel_patent_id] =>[rel_patent_doc_number] =>) 14/200365 | Rear nacelle assembly for a turbojet engine | Mar 6, 2014 | Issued |
Array
(
[id] => 10492121
[patent_doc_number] => 20150377142
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2015-12-31
[patent_title] => 'LOW SPOOL STARTER SYSTEM FOR GAS TURBINE ENGINE'
[patent_app_type] => utility
[patent_app_number] => 14/767477
[patent_app_country] => US
[patent_app_date] => 2014-02-27
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[rel_patent_id] =>[rel_patent_doc_number] =>) 14/767477 | Low spool starter system for gas turbine engine | Feb 26, 2014 | Issued |
Array
(
[id] => 9685097
[patent_doc_number] => 20140241860
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2014-08-28
[patent_title] => 'FLIGHT GAS TURBINE WITH A FIRST ROTATABLE SHAFT'
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[rel_patent_id] =>[rel_patent_doc_number] =>) 14/180005 | FLIGHT GAS TURBINE WITH A FIRST ROTATABLE SHAFT | Feb 12, 2014 | Abandoned |
Array
(
[id] => 11192097
[patent_doc_number] => 09422905
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[patent_issue_date] => 2016-08-23
[patent_title] => 'System for in-flight restarting of a multi-shaft turboprop engine'
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[rel_patent_id] =>[rel_patent_doc_number] =>) 14/179059 | System for in-flight restarting of a multi-shaft turboprop engine | Feb 11, 2014 | Issued |
Array
(
[id] => 10664422
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[patent_issue_date] => 2016-01-14
[patent_title] => 'METHOD FOR OPERATING A GAS TURBINE BELOW ITS RATED POWER'
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Array
(
[id] => 12133105
[patent_doc_number] => 09874148
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[patent_issue_date] => 2018-01-23
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[rel_patent_id] =>[rel_patent_doc_number] =>) 14/169618 | Hybrid slinger combustion system | Jan 30, 2014 | Issued |
Array
(
[id] => 10492467
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[patent_title] => 'SUPPLEMENTARY LASER FIRING FOR COMBUSTION STABILITY'
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[rel_patent_id] =>[rel_patent_doc_number] =>) 14/767484 | Supplementary laser firing for combustion stability | Jan 22, 2014 | Issued |
Array
(
[id] => 9473044
[patent_doc_number] => 20140130507
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[patent_issue_date] => 2014-05-15
[patent_title] => 'GAS TURBINE PLANT WITH EXHAUST GAS RECIRCULATION AND ALSO METHOD FOR OPERATING SUCH A PLANT'
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Array
(
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[patent_title] => 'METHOD FOR THE ARRANGEMENT OF IMPINGEMENT COOLING HOLES AND EFFUSION HOLES IN A COMBUSTION CHAMBER WALL OF A GAS TURBINE'
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Array
(
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[patent_title] => 'METHOD AND GAS TURBINE COMBUSTION SYSTEM FOR SAFELY MIXING H2-RICH FUELS WITH AIR'
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[rel_patent_id] =>[rel_patent_doc_number] =>) 14/096210 | Method and gas turbine combustion system for safely mixing H2-rich fuels with air | Dec 3, 2013 | Issued |
Array
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[rel_patent_id] =>[rel_patent_doc_number] =>) 14/070393 | Fan nozzle drive systems that lock thrust reversers | Oct 31, 2013 | Issued |