
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] => 9666538
[patent_doc_number] => 20140230401
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2014-08-21
[patent_title] => 'CYCLE TURBINE ENGINE POWER SYSTEM'
[patent_app_type] => utility
[patent_app_number] => 14/013255
[patent_app_country] => US
[patent_app_date] => 2013-08-29
[patent_effective_date] => 0000-00-00
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[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14013255
[rel_patent_id] =>[rel_patent_doc_number] =>) 14/013255 | Semi-closed cycle turbine power system to produce saleable CO | Aug 28, 2013 | Issued |
Array
(
[id] => 9666540
[patent_doc_number] => 20140230403
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2014-08-21
[patent_title] => 'GAS TURBINE ENGINE SHAFT BEARING CONFIGURATION'
[patent_app_type] => utility
[patent_app_number] => 14/012576
[patent_app_country] => US
[patent_app_date] => 2013-08-28
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[rel_patent_id] =>[rel_patent_doc_number] =>) 14/012576 | Gas turbine engine shaft bearing configuration | Aug 27, 2013 | Issued |
Array
(
[id] => 9326787
[patent_doc_number] => 20140053569
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2014-02-27
[patent_title] => 'METHOD FOR MIXING A DILUTION AIR IN A SEQUENTIAL COMBUSTION SYSTEM OF A GAS TURBINE'
[patent_app_type] => utility
[patent_app_number] => 13/974523
[patent_app_country] => US
[patent_app_date] => 2013-08-23
[patent_effective_date] => 0000-00-00
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Array
(
[id] => 13888927
[patent_doc_number] => 10197010
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2019-02-05
[patent_title] => Long-duct, mixed-flow nozzle system for a turbofan engine
[patent_app_type] => utility
[patent_app_number] => 13/964706
[patent_app_country] => US
[patent_app_date] => 2013-08-12
[patent_effective_date] => 0000-00-00
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[rel_patent_id] =>[rel_patent_doc_number] =>) 13/964706 | Long-duct, mixed-flow nozzle system for a turbofan engine | Aug 11, 2013 | Issued |
Array
(
[id] => 9276617
[patent_doc_number] => 20140026585
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[patent_kind] => A1
[patent_issue_date] => 2014-01-30
[patent_title] => 'CERAMIC-TO-METAL TURBINE VOLUTE ATTACHMENT FOR A GAS TURBINE ENGINE'
[patent_app_type] => utility
[patent_app_number] => 13/949781
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[rel_patent_id] =>[rel_patent_doc_number] =>) 13/949781 | Ceramic-to-metal turbine volute attachment for a gas turbine engine | Jul 23, 2013 | Issued |
Array
(
[id] => 9838366
[patent_doc_number] => 20150030446
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2015-01-29
[patent_title] => 'NACELLE FOR AN AIRCRAFT BYPASS TURBOJET ENGINE'
[patent_app_type] => utility
[patent_app_number] => 13/946316
[patent_app_country] => US
[patent_app_date] => 2013-07-19
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[rel_patent_id] =>[rel_patent_doc_number] =>) 13/946316 | NACELLE FOR AN AIRCRAFT BYPASS TURBOJET ENGINE | Jul 18, 2013 | Abandoned |
Array
(
[id] => 9838364
[patent_doc_number] => 20150030445
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2015-01-29
[patent_title] => 'NACELLE FOR AN AIRCRAFT BYPASS TURBOJET ENGINE'
[patent_app_type] => utility
[patent_app_number] => 13/945023
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[rel_patent_id] =>[rel_patent_doc_number] =>) 13/945023 | NACELLE FOR AN AIRCRAFT BYPASS TURBOJET ENGINE | Jul 17, 2013 | Abandoned |
Array
(
[id] => 9103292
[patent_doc_number] => 20130276423
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2013-10-24
[patent_title] => 'GAS TURBINE'
[patent_app_type] => utility
[patent_app_number] => 13/923884
[patent_app_country] => US
[patent_app_date] => 2013-06-21
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[rel_patent_id] =>[rel_patent_doc_number] =>) 13/923884 | Gas turbine | Jun 20, 2013 | Issued |
Array
(
[id] => 9187737
[patent_doc_number] => 20130327052
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2013-12-12
[patent_title] => 'EXHAUST SYSTEM FOR GAS TURBINES'
[patent_app_type] => utility
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[rel_patent_id] =>[rel_patent_doc_number] =>) 13/916396 | EXHAUST SYSTEM FOR GAS TURBINES | Jun 11, 2013 | Abandoned |
Array
(
[id] => 9187739
[patent_doc_number] => 20130327054
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2013-12-12
[patent_title] => 'HYBRID SLINGER COMBUSTION SYSTEM'
[patent_app_type] => utility
[patent_app_number] => 13/915990
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[rel_patent_id] =>[rel_patent_doc_number] =>) 13/915990 | Hybrid slinger combustion system | Jun 11, 2013 | Issued |
Array
(
[id] => 14552523
[patent_doc_number] => 10344710
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[patent_kind] => B2
[patent_issue_date] => 2019-07-09
[patent_title] => Engine with a thrust reverser lockout mechanism
[patent_app_type] => utility
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[rel_patent_id] =>[rel_patent_doc_number] =>) 14/888811 | Engine with a thrust reverser lockout mechanism | Jun 6, 2013 | Issued |
Array
(
[id] => 10163114
[patent_doc_number] => 09194333
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[patent_title] => 'Turbopump'
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Array
(
[id] => 9170436
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Array
(
[id] => 9078040
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[patent_title] => 'HELICAL CROSS FLOW (HCF) PULSE DETONATION ENGINE'
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[rel_patent_id] =>[rel_patent_doc_number] =>) 13/886030 | Helical cross flow (HCF) pulse detonation engine | May 1, 2013 | Issued |
Array
(
[id] => 11657806
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[patent_title] => 'Turbojet engine nacelle with variable ventilation outlet cross section'
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[rel_patent_id] =>[rel_patent_doc_number] =>) 13/870369 | Turbojet engine nacelle with variable ventilation outlet cross section | Apr 24, 2013 | Issued |
Array
(
[id] => 12608376
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[patent_title] => High Stiffness Shape Memory Alloy Actuated Aerostructure
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[rel_patent_id] =>[rel_patent_doc_number] =>) 13/855721 | High stiffness shape memory alloy actuated aerostructure | Apr 2, 2013 | Issued |
Array
(
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Array
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Array
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Array
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