
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] => 9681262
[patent_doc_number] => 20140238024
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2014-08-28
[patent_title] => 'RICH BURN, QUICK MIX, LEAN BURN COMBUSTOR'
[patent_app_type] => utility
[patent_app_number] => 13/777179
[patent_app_country] => US
[patent_app_date] => 2013-02-26
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 6
[patent_figures_cnt] => 6
[patent_no_of_words] => 4483
[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] => 13777179
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/777179 | Rich burn, quick mix, lean burn combustor | Feb 25, 2013 | Issued |
Array
(
[id] => 9685093
[patent_doc_number] => 20140241856
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2014-08-28
[patent_title] => 'GAS TURBINE ENGINE SYSTEMS INVOLVING TIP FANS'
[patent_app_type] => utility
[patent_app_number] => 13/777723
[patent_app_country] => US
[patent_app_date] => 2013-02-26
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 3
[patent_no_of_words] => 2658
[patent_no_of_claims] => 10
[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] => 13777723
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/777723 | GAS TURBINE ENGINE SYSTEMS INVOLVING TIP FANS | Feb 25, 2013 | Abandoned |
Array
(
[id] => 10205822
[patent_doc_number] => 20150090810
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2015-04-02
[patent_title] => 'THRUST REVERSER HYDRAULIC ACTUATION SYSTEM WITH SERVO SYNCHRONIZATION'
[patent_app_type] => utility
[patent_app_number] => 13/764538
[patent_app_country] => US
[patent_app_date] => 2013-02-11
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 6
[patent_figures_cnt] => 6
[patent_no_of_words] => 7321
[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] => 13764538
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/764538 | THRUST REVERSER HYDRAULIC ACTUATION SYSTEM WITH SERVO SYNCHRONIZATION | Feb 10, 2013 | Abandoned |
Array
(
[id] => 8979957
[patent_doc_number] => 08511061
[patent_country] => US
[patent_kind] => B1
[patent_issue_date] => 2013-08-20
[patent_title] => 'Gas turbine engine shaft bearing configuration'
[patent_app_type] => utility
[patent_app_number] => 13/762970
[patent_app_country] => US
[patent_app_date] => 2013-02-08
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 2
[patent_figures_cnt] => 2
[patent_no_of_words] => 2837
[patent_no_of_claims] => 15
[patent_no_of_ind_claims] => 4
[patent_words_short_claim] => 153
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13762970
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/762970 | Gas turbine engine shaft bearing configuration | Feb 7, 2013 | Issued |
Array
(
[id] => 10622176
[patent_doc_number] => 09341114
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2016-05-17
[patent_title] => 'Gas power plant'
[patent_app_type] => utility
[patent_app_number] => 14/379439
[patent_app_country] => US
[patent_app_date] => 2013-02-01
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 2
[patent_figures_cnt] => 4
[patent_no_of_words] => 5926
[patent_no_of_claims] => 19
[patent_no_of_ind_claims] => 4
[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] => 14379439
[rel_patent_id] =>[rel_patent_doc_number] =>) 14/379439 | Gas power plant | Jan 31, 2013 | Issued |
Array
(
[id] => 13155159
[patent_doc_number] => 10094295
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2018-10-09
[patent_title] => Gas turbine engine with transmission
[patent_app_type] => utility
[patent_app_number] => 13/754304
[patent_app_country] => US
[patent_app_date] => 2013-01-30
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 8
[patent_figures_cnt] => 8
[patent_no_of_words] => 4259
[patent_no_of_claims] => 15
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 239
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13754304
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/754304 | Gas turbine engine with transmission | Jan 29, 2013 | Issued |
Array
(
[id] => 10492103
[patent_doc_number] => 20150377125
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2015-12-31
[patent_title] => 'REVERSE-FLOW CORE GAS TURBINE ENGINE WITH A PULSE DETONATION SYSTEM'
[patent_app_type] => utility
[patent_app_number] => 14/764186
[patent_app_country] => US
[patent_app_date] => 2013-01-29
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 3
[patent_no_of_words] => 4620
[patent_no_of_claims] => 15
[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] => 14764186
[rel_patent_id] =>[rel_patent_doc_number] =>) 14/764186 | Reverse-flow core gas turbine engine with a pulse detonation system | Jan 28, 2013 | Issued |
Array
(
[id] => 10299593
[patent_doc_number] => 20150184593
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2015-07-02
[patent_title] => 'Gas Turbine Energy Storage and Energy Supplementing Systems And Methods of Making and Using the Same'
[patent_app_type] => utility
[patent_app_number] => 14/357136
[patent_app_country] => US
[patent_app_date] => 2013-01-29
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 6
[patent_figures_cnt] => 6
[patent_no_of_words] => 8696
[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] => 14357136
[rel_patent_id] =>[rel_patent_doc_number] =>) 14/357136 | Gas Turbine Energy Storage and Energy Supplementing Systems And Methods of Making and Using the Same | Jan 28, 2013 | Abandoned |
Array
(
[id] => 11994713
[patent_doc_number] => 20170298868
[patent_country] => US
[patent_kind] => A9
[patent_issue_date] => 2017-10-19
[patent_title] => 'GAS TURBINE ENGINE NOZZLE INCLUDING HOUSING HAVING SCALLOPED ROOT REGIONS'
[patent_app_type] => utility
[patent_app_number] => 13/746277
[patent_app_country] => US
[patent_app_date] => 2013-01-21
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 8
[patent_figures_cnt] => 8
[patent_no_of_words] => 1909
[patent_no_of_claims] => 17
[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] => 13746277
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/746277 | Gas turbine engine nozzle including housing having scalloped root regions | Jan 20, 2013 | Issued |
Array
(
[id] => 11994713
[patent_doc_number] => 20170298868
[patent_country] => US
[patent_kind] => A9
[patent_issue_date] => 2017-10-19
[patent_title] => 'GAS TURBINE ENGINE NOZZLE INCLUDING HOUSING HAVING SCALLOPED ROOT REGIONS'
[patent_app_type] => utility
[patent_app_number] => 13/746277
[patent_app_country] => US
[patent_app_date] => 2013-01-21
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 8
[patent_figures_cnt] => 8
[patent_no_of_words] => 1909
[patent_no_of_claims] => 17
[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] => 13746277
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/746277 | Gas turbine engine nozzle including housing having scalloped root regions | Jan 20, 2013 | Issued |
Array
(
[id] => 10477175
[patent_doc_number] => 20150362192
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2015-12-17
[patent_title] => 'GAS TURBINE ENGINE COMBUSTOR LINER ASSEMBLY WITH CONVERGENT HYPERBOLIC PROFILE'
[patent_app_type] => utility
[patent_app_number] => 14/761559
[patent_app_country] => US
[patent_app_date] => 2013-01-17
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 13
[patent_figures_cnt] => 13
[patent_no_of_words] => 4739
[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] => 14761559
[rel_patent_id] =>[rel_patent_doc_number] =>) 14/761559 | GAS TURBINE ENGINE COMBUSTOR LINER ASSEMBLY WITH CONVERGENT HYPERBOLIC PROFILE | Jan 16, 2013 | Abandoned |
Array
(
[id] => 8817134
[patent_doc_number] => 20130118179
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2013-05-16
[patent_title] => 'POWER PLANT WITH CO2 CAPTURE'
[patent_app_type] => utility
[patent_app_number] => 13/739806
[patent_app_country] => US
[patent_app_date] => 2013-01-11
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 4
[patent_no_of_words] => 5360
[patent_no_of_claims] => 14
[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] => 13739806
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/739806 | POWER PLANT WITH CO2 CAPTURE | Jan 10, 2013 | Abandoned |
Array
(
[id] => 10950378
[patent_doc_number] => 20140353399
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2014-12-04
[patent_title] => 'THRUST REVERSER SYSTEM WITH TRANSLATING-ROTATING BLOCKER DOORS AND METHOD OF OPERATION'
[patent_app_type] => utility
[patent_app_number] => 13/689981
[patent_app_country] => US
[patent_app_date] => 2012-11-30
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 9
[patent_figures_cnt] => 9
[patent_no_of_words] => 4270
[patent_no_of_claims] => 24
[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] => 13689981
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/689981 | Thrust reverser system with translating-rotating blocker doors and method of operation | Nov 29, 2012 | Issued |
Array
(
[id] => 11319796
[patent_doc_number] => 09518535
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2016-12-13
[patent_title] => 'Assembly including a reverse thrust device and system for actuating said device'
[patent_app_type] => utility
[patent_app_number] => 13/691160
[patent_app_country] => US
[patent_app_date] => 2012-11-30
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 10
[patent_no_of_words] => 4852
[patent_no_of_claims] => 9
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 225
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13691160
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/691160 | Assembly including a reverse thrust device and system for actuating said device | Nov 29, 2012 | Issued |
Array
(
[id] => 12254706
[patent_doc_number] => 09926845
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2018-03-27
[patent_title] => 'Combustor and gas turbine'
[patent_app_type] => utility
[patent_app_number] => 13/687587
[patent_app_country] => US
[patent_app_date] => 2012-11-28
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 9
[patent_figures_cnt] => 12
[patent_no_of_words] => 10561
[patent_no_of_claims] => 9
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 301
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13687587
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/687587 | Combustor and gas turbine | Nov 27, 2012 | Issued |
Array
(
[id] => 8915781
[patent_doc_number] => 20130177406
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2013-07-11
[patent_title] => 'GAS TURBINE ENGINE BEARING CHAMBER SEALS'
[patent_app_type] => utility
[patent_app_number] => 13/684356
[patent_app_country] => US
[patent_app_date] => 2012-11-23
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 6
[patent_figures_cnt] => 6
[patent_no_of_words] => 4302
[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] => 13684356
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/684356 | Gas turbine engine bearing chamber seals | Nov 22, 2012 | Issued |
Array
(
[id] => 8912949
[patent_doc_number] => 20130174574
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2013-07-11
[patent_title] => 'GAS TURBINE ENGINE BEARING CHAMBER SEALS'
[patent_app_type] => utility
[patent_app_number] => 13/684342
[patent_app_country] => US
[patent_app_date] => 2012-11-23
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
[patent_figures_cnt] => 5
[patent_no_of_words] => 3263
[patent_no_of_claims] => 16
[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] => 13684342
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/684342 | GAS TURBINE ENGINE BEARING CHAMBER SEALS | Nov 22, 2012 | Abandoned |
Array
(
[id] => 11244381
[patent_doc_number] => 09470419
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2016-10-18
[patent_title] => 'Combustion chamber'
[patent_app_type] => utility
[patent_app_number] => 14/356990
[patent_app_country] => US
[patent_app_date] => 2012-11-22
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 4
[patent_no_of_words] => 1724
[patent_no_of_claims] => 4
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 248
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14356990
[rel_patent_id] =>[rel_patent_doc_number] =>) 14/356990 | Combustion chamber | Nov 21, 2012 | Issued |
Array
(
[id] => 10057770
[patent_doc_number] => 09097119
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2015-08-04
[patent_title] => 'Transitional region for a secondary combustion chamber of a gas turbine'
[patent_app_type] => utility
[patent_app_number] => 13/668274
[patent_app_country] => US
[patent_app_date] => 2012-11-04
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 9
[patent_no_of_words] => 4366
[patent_no_of_claims] => 16
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 226
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13668274
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/668274 | Transitional region for a secondary combustion chamber of a gas turbine | Nov 3, 2012 | Issued |
Array
(
[id] => 9013671
[patent_doc_number] => 20130228635
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2013-09-05
[patent_title] => 'TURBOJET ENGINE NACELLE'
[patent_app_type] => utility
[patent_app_number] => 13/663652
[patent_app_country] => US
[patent_app_date] => 2012-10-30
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 4
[patent_no_of_words] => 4576
[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] =>[firstpage_image] =>[orig_patent_app_number] => 13663652
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/663652 | TURBOJET ENGINE NACELLE | Oct 29, 2012 | Abandoned |