
Carlos A. Rivera
Examiner (ID: 56, Phone: (571)270-5697 , Office: P/3741 )
| Most Active Art Unit | 3741 |
| Art Unit(s) | 3741, 4168, 4100, 3723 |
| Total Applications | 629 |
| Issued Applications | 447 |
| Pending Applications | 80 |
| Abandoned Applications | 131 |
Applications
| Application number | Title of the application | Filing Date | Status |
|---|---|---|---|
Array
(
[id] => 11865803
[patent_doc_number] => 20170233089
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2017-08-17
[patent_title] => 'SYSTEM AND METHOD FOR STARTING THE ENGINES OF A TWIN-ENGINE AIRCRAFT'
[patent_app_type] => utility
[patent_app_number] => 15/434284
[patent_app_country] => US
[patent_app_date] => 2017-02-16
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 3
[patent_no_of_words] => 3756
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[patent_current_assignee] =>[type] => publication
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[rel_patent_id] =>[rel_patent_doc_number] =>) 15/434284 | System and method for starting the engines of a twin-engine aircraft | Feb 15, 2017 | Issued |
Array
(
[id] => 13359423
[patent_doc_number] => 20180231251
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2018-08-16
[patent_title] => COMBUSTOR LINER PANEL SHELL INTERFACE FOR A GAS TURBINE ENGINE COMBUSTOR
[patent_app_type] => utility
[patent_app_number] => 15/432098
[patent_app_country] => US
[patent_app_date] => 2017-02-14
[patent_effective_date] => 0000-00-00
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[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 15432098
[rel_patent_id] =>[rel_patent_doc_number] =>) 15/432098 | Combustor liner panel shell interface for a gas turbine engine combustor | Feb 13, 2017 | Issued |
Array
(
[id] => 15979251
[patent_doc_number] => 10669941
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2020-06-02
[patent_title] => Gas turbine cooling system, gas turbine facility including the same, and control device and control method of gas turbine cooling system
[patent_app_type] => utility
[patent_app_number] => 15/777767
[patent_app_country] => US
[patent_app_date] => 2016-12-06
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[patent_drawing_sheets_cnt] => 9
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[rel_patent_id] =>[rel_patent_doc_number] =>) 15/777767 | Gas turbine cooling system, gas turbine facility including the same, and control device and control method of gas turbine cooling system | Dec 5, 2016 | Issued |
Array
(
[id] => 13577839
[patent_doc_number] => 20180340468
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2018-11-29
[patent_title] => GAS TURBINE AND COMPONENT-TEMPERATURE ADJUSTMENT METHOD THEREFOR
[patent_app_type] => utility
[patent_app_number] => 15/778122
[patent_app_country] => US
[patent_app_date] => 2016-11-25
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 0
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[rel_patent_id] =>[rel_patent_doc_number] =>) 15/778122 | Gas turbine and component-temperature adjustment method therefor | Nov 24, 2016 | Issued |
Array
(
[id] => 13591641
[patent_doc_number] => 20180347369
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2018-12-06
[patent_title] => FLOW PASSAGE FORMING PLATE, FLOW PASSAGE FORMING MEMBER ASSEMBLY AND VANE INCLUDING THE SAME, GAS TURBINE, MANUFACTURING METHOD OF FLOW PASSAGE FORMING PLATE, AND MODIFICATION METHOD OF FLOW PASSAGE FORMING PLATE
[patent_app_type] => utility
[patent_app_number] => 15/778522
[patent_app_country] => US
[patent_app_date] => 2016-11-17
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 0
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[patent_no_of_words] => 17896
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[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 15778522
[rel_patent_id] =>[rel_patent_doc_number] =>) 15/778522 | Flow passage forming plate, flow passage forming member assembly and vane including the same, gas turbine, manufacturing method of flow passage forming plate, and modification method of flow passage forming plate | Nov 16, 2016 | Issued |
Array
(
[id] => 12731065
[patent_doc_number] => 20180135522
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2018-05-17
[patent_title] => GAS TURBINE ENGINE ACCESSORIES ARRANGEMENT
[patent_app_type] => utility
[patent_app_number] => 15/351803
[patent_app_country] => US
[patent_app_date] => 2016-11-15
[patent_effective_date] => 0000-00-00
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[rel_patent_id] =>[rel_patent_doc_number] =>) 15/351803 | Gas turbine engine accessories arrangement | Nov 14, 2016 | Issued |
Array
(
[id] => 14854227
[patent_doc_number] => 10415832
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2019-09-17
[patent_title] => Multi-swirler fuel/air mixer with centralized fuel injection
[patent_app_type] => utility
[patent_app_number] => 15/339463
[patent_app_country] => US
[patent_app_date] => 2016-10-31
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 12
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[rel_patent_id] =>[rel_patent_doc_number] =>) 15/339463 | Multi-swirler fuel/air mixer with centralized fuel injection | Oct 30, 2016 | Issued |
Array
(
[id] => 11604920
[patent_doc_number] => 20170122222
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2017-05-04
[patent_title] => 'System and Method for Determining Fuel Splits for a Gas Turbine'
[patent_app_type] => utility
[patent_app_number] => 15/296222
[patent_app_country] => US
[patent_app_date] => 2016-10-18
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
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[rel_patent_id] =>[rel_patent_doc_number] =>) 15/296222 | System and Method for Determining Fuel Splits for a Gas Turbine | Oct 17, 2016 | Abandoned |
Array
(
[id] => 16029707
[patent_doc_number] => 10677264
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2020-06-09
[patent_title] => Supersonic single-stage turbofan engine
[patent_app_type] => utility
[patent_app_number] => 15/293368
[patent_app_country] => US
[patent_app_date] => 2016-10-14
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[rel_patent_id] =>[rel_patent_doc_number] =>) 15/293368 | Supersonic single-stage turbofan engine | Oct 13, 2016 | Issued |
Array
(
[id] => 16030111
[patent_doc_number] => 10677466
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2020-06-09
[patent_title] => Combustor inlet flow conditioner
[patent_app_type] => utility
[patent_app_number] => 15/292485
[patent_app_country] => US
[patent_app_date] => 2016-10-13
[patent_effective_date] => 0000-00-00
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[rel_patent_id] =>[rel_patent_doc_number] =>) 15/292485 | Combustor inlet flow conditioner | Oct 12, 2016 | Issued |
Array
(
[id] => 11994661
[patent_doc_number] => 20170298816
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2017-10-19
[patent_title] => 'GAS TURBINE ENGINE'
[patent_app_type] => utility
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[rel_patent_id] =>[rel_patent_doc_number] =>) 15/292852 | GAS TURBINE ENGINE | Oct 12, 2016 | Abandoned |
Array
(
[id] => 11628074
[patent_doc_number] => 20170138263
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2017-05-18
[patent_title] => 'AIR INLET DUCT HAVING A PARTICLE SEPARATOR AND AN AGGLOMERATOR FOR A GAS TURBINE ENGINE'
[patent_app_type] => utility
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[rel_patent_id] =>[rel_patent_doc_number] =>) 15/292676 | Air-inlet duct having a particle separator and an agglomerator for a gas turbine engine | Oct 12, 2016 | Issued |
Array
(
[id] => 12642972
[patent_doc_number] => 20180106155
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[patent_kind] => A1
[patent_issue_date] => 2018-04-19
[patent_title] => TRANSITION DUCT FORMED OF A PLURALITY OF SEGMENTS
[patent_app_type] => utility
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[rel_patent_id] =>[rel_patent_doc_number] =>) 15/292390 | TRANSITION DUCT FORMED OF A PLURALITY OF SEGMENTS | Oct 12, 2016 | Abandoned |
Array
(
[id] => 14763359
[patent_doc_number] => 10393068
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[patent_issue_date] => 2019-08-27
[patent_title] => Shafting arrangement for a gas turbine engine
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Array
(
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[patent_title] => Efficient, low pressure ratio propulsor for gas turbine engines
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Array
(
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[patent_title] => 'EFFICIENT, LOW PRESSURE RATIO PROPULSOR FOR GAS TURBINE ENGINES'
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Array
(
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Array
(
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[patent_title] => Variable area fan nozzle with wall thickness distribution
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Array
(
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Array
(
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[patent_title] => Turbomachine diffuser including flow mixing lobes and method
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[rel_patent_id] =>[rel_patent_doc_number] =>) 15/159850 | Turbomachine diffuser including flow mixing lobes and method | May 19, 2016 | Issued |