Search

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 numberTitle of the applicationFiling DateStatus
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 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 5 [patent_figures_cnt] => 5 [patent_no_of_words] => 9509 [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] =>[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 [patent_drawing_sheets_cnt] => 5 [patent_figures_cnt] => 5 [patent_no_of_words] => 2586 [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] =>[firstpage_image] =>[orig_patent_app_number] => 14274892 [rel_patent_id] =>[rel_patent_doc_number] =>)
14/274892
Enhanced Turbine Cooling System Using a Blend of Compressor Bleed Air and Ambient Air May 11, 2014 Abandoned
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 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 8 [patent_figures_cnt] => 8 [patent_no_of_words] => 4619 [patent_no_of_claims] => 6 [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] =>[firstpage_image] =>[orig_patent_app_number] => 14271584 [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 [patent_figures_cnt] => 7 [patent_no_of_words] => 3758 [patent_no_of_claims] => 33 [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] =>[firstpage_image] =>[orig_patent_app_number] => 14260617 [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 [patent_figures_cnt] => 2 [patent_no_of_words] => 1038 [patent_no_of_claims] => 8 [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] =>[firstpage_image] =>[orig_patent_app_number] => 14251344 [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 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 7 [patent_figures_cnt] => 7 [patent_no_of_words] => 2187 [patent_no_of_claims] => 15 [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] =>[firstpage_image] =>[orig_patent_app_number] => 14228574 [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 [patent_figures_cnt] => 7 [patent_no_of_words] => 2962 [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] =>[firstpage_image] =>[orig_patent_app_number] => 14221494 [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 [patent_drawing_sheets_cnt] => 6 [patent_figures_cnt] => 6 [patent_no_of_words] => 3772 [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] =>[firstpage_image] =>[orig_patent_app_number] => 14777331 [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 [patent_app_country] => US [patent_app_date] => 2014-03-14 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 4 [patent_figures_cnt] => 6 [patent_no_of_words] => 4834 [patent_no_of_claims] => 6 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 376 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14778412 [rel_patent_id] =>[rel_patent_doc_number] =>)
14/778412
Injection system for a combustion chamber of a turbine engine, comprising an annular wall having a convergent inner cross-section Mar 13, 2014 Issued
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 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 9 [patent_figures_cnt] => 9 [patent_no_of_words] => 8092 [patent_no_of_claims] => 20 [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] =>[firstpage_image] =>[orig_patent_app_number] => 14200365 [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 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 7 [patent_figures_cnt] => 7 [patent_no_of_words] => 5552 [patent_no_of_claims] => 23 [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] =>[firstpage_image] =>[orig_patent_app_number] => 14767477 [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' [patent_app_type] => utility [patent_app_number] => 14/180005 [patent_app_country] => US [patent_app_date] => 2014-02-13 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 3 [patent_figures_cnt] => 3 [patent_no_of_words] => 3185 [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] =>[firstpage_image] =>[orig_patent_app_number] => 14180005 [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 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2016-08-23 [patent_title] => 'System for in-flight restarting of a multi-shaft turboprop engine' [patent_app_type] => utility [patent_app_number] => 14/179059 [patent_app_country] => US [patent_app_date] => 2014-02-12 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 7 [patent_figures_cnt] => 7 [patent_no_of_words] => 2976 [patent_no_of_claims] => 9 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 250 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14179059 [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 [patent_doc_number] => 20160010566 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2016-01-14 [patent_title] => 'METHOD FOR OPERATING A GAS TURBINE BELOW ITS RATED POWER' [patent_app_type] => utility [patent_app_number] => 14/768827 [patent_app_country] => US [patent_app_date] => 2014-02-06 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 2 [patent_figures_cnt] => 2 [patent_no_of_words] => 2632 [patent_no_of_claims] => 5 [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] =>[firstpage_image] =>[orig_patent_app_number] => 14768827 [rel_patent_id] =>[rel_patent_doc_number] =>)
14/768827
METHOD FOR OPERATING A GAS TURBINE BELOW ITS RATED POWER Feb 5, 2014 Abandoned
Array ( [id] => 12133105 [patent_doc_number] => 09874148 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2018-01-23 [patent_title] => 'Hybrid slinger combustion system' [patent_app_type] => utility [patent_app_number] => 14/169618 [patent_app_country] => US [patent_app_date] => 2014-01-31 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 5 [patent_figures_cnt] => 5 [patent_no_of_words] => 2156 [patent_no_of_claims] => 15 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 166 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14169618 [rel_patent_id] =>[rel_patent_doc_number] =>)
14/169618
Hybrid slinger combustion system Jan 30, 2014 Issued
Array ( [id] => 10492467 [patent_doc_number] => 20150377490 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2015-12-31 [patent_title] => 'SUPPLEMENTARY LASER FIRING FOR COMBUSTION STABILITY' [patent_app_type] => utility [patent_app_number] => 14/767484 [patent_app_country] => US [patent_app_date] => 2014-01-23 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 3 [patent_figures_cnt] => 3 [patent_no_of_words] => 6184 [patent_no_of_claims] => 12 [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] =>[firstpage_image] =>[orig_patent_app_number] => 14767484 [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 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2014-05-15 [patent_title] => 'GAS TURBINE PLANT WITH EXHAUST GAS RECIRCULATION AND ALSO METHOD FOR OPERATING SUCH A PLANT' [patent_app_type] => utility [patent_app_number] => 14/157982 [patent_app_country] => US [patent_app_date] => 2014-01-17 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 6 [patent_figures_cnt] => 6 [patent_no_of_words] => 7398 [patent_no_of_claims] => 24 [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] =>[firstpage_image] =>[orig_patent_app_number] => 14157982 [rel_patent_id] =>[rel_patent_doc_number] =>)
14/157982
GAS TURBINE PLANT WITH EXHAUST GAS RECIRCULATION AND ALSO METHOD FOR OPERATING SUCH A PLANT Jan 16, 2014 Abandoned
Array ( [id] => 9766598 [patent_doc_number] => 20140290258 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2014-10-02 [patent_title] => 'METHOD FOR THE ARRANGEMENT OF IMPINGEMENT COOLING HOLES AND EFFUSION HOLES IN A COMBUSTION CHAMBER WALL OF A GAS TURBINE' [patent_app_type] => utility [patent_app_number] => 14/134602 [patent_app_country] => US [patent_app_date] => 2013-12-19 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 5 [patent_figures_cnt] => 5 [patent_no_of_words] => 2930 [patent_no_of_claims] => 4 [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] =>[firstpage_image] =>[orig_patent_app_number] => 14134602 [rel_patent_id] =>[rel_patent_doc_number] =>)
14/134602
METHOD FOR THE ARRANGEMENT OF IMPINGEMENT COOLING HOLES AND EFFUSION HOLES IN A COMBUSTION CHAMBER WALL OF A GAS TURBINE Dec 18, 2013 Abandoned
Array ( [id] => 9459242 [patent_doc_number] => 20140123667 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2014-05-08 [patent_title] => 'METHOD AND GAS TURBINE COMBUSTION SYSTEM FOR SAFELY MIXING H2-RICH FUELS WITH AIR' [patent_app_type] => utility [patent_app_number] => 14/096210 [patent_app_country] => US [patent_app_date] => 2013-12-04 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 4 [patent_figures_cnt] => 4 [patent_no_of_words] => 3315 [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] =>[firstpage_image] =>[orig_patent_app_number] => 14096210 [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 ( [id] => 12106891 [patent_doc_number] => 09863367 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2018-01-09 [patent_title] => 'Fan nozzle drive systems that lock thrust reversers' [patent_app_type] => utility [patent_app_number] => 14/070393 [patent_app_country] => US [patent_app_date] => 2013-11-01 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 7 [patent_figures_cnt] => 7 [patent_no_of_words] => 3717 [patent_no_of_claims] => 23 [patent_no_of_ind_claims] => 4 [patent_words_short_claim] => 130 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14070393 [rel_patent_id] =>[rel_patent_doc_number] =>)
14/070393
Fan nozzle drive systems that lock thrust reversers Oct 31, 2013 Issued
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