
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] => 10649949
[patent_doc_number] => 09366190
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2016-06-14
[patent_title] => 'Tapered gas turbine engine liquid gallery'
[patent_app_type] => utility
[patent_app_number] => 13/893019
[patent_app_country] => US
[patent_app_date] => 2013-05-13
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 7
[patent_figures_cnt] => 8
[patent_no_of_words] => 6057
[patent_no_of_claims] => 14
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 168
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13893019
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/893019 | Tapered gas turbine engine liquid gallery | May 12, 2013 | Issued |
Array
(
[id] => 10197818
[patent_doc_number] => 20150082804
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2015-03-26
[patent_title] => 'TURBINE ENGINE INCORPORATING THERMOELECTRIC GENERATORS'
[patent_app_type] => utility
[patent_app_number] => 14/396290
[patent_app_country] => US
[patent_app_date] => 2013-04-22
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 2
[patent_figures_cnt] => 2
[patent_no_of_words] => 2144
[patent_no_of_claims] => 5
[patent_no_of_ind_claims] => 2
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[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14396290
[rel_patent_id] =>[rel_patent_doc_number] =>) 14/396290 | Turbine engine incorporating thermoelectric generators | Apr 21, 2013 | Issued |
Array
(
[id] => 9012999
[patent_doc_number] => 20130227963
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2013-09-05
[patent_title] => 'ASSEMBLY FOR ATTACHING THE HANGERS FROM WHICH AN AIRCRAFT PROPULSION UNIT IS SUSPENDED'
[patent_app_type] => utility
[patent_app_number] => 13/862724
[patent_app_country] => US
[patent_app_date] => 2013-04-15
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 3
[patent_no_of_words] => 3588
[patent_no_of_claims] => 10
[patent_no_of_ind_claims] => 1
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[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13862724
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/862724 | Assembly for attaching the hangers from which an aircraft propulsion unit is suspended | Apr 14, 2013 | Issued |
Array
(
[id] => 10649898
[patent_doc_number] => 09366139
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2016-06-14
[patent_title] => 'Repair method of plate member, plate member, combustor, ring segment, and gas turbine'
[patent_app_type] => utility
[patent_app_number] => 13/859240
[patent_app_country] => US
[patent_app_date] => 2013-04-09
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 14
[patent_figures_cnt] => 22
[patent_no_of_words] => 5790
[patent_no_of_claims] => 13
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 187
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13859240
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/859240 | Repair method of plate member, plate member, combustor, ring segment, and gas turbine | Apr 8, 2013 | Issued |
Array
(
[id] => 11192060
[patent_doc_number] => 09422868
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2016-08-23
[patent_title] => 'Simple cycle gas turbomachine system having a fuel conditioning system'
[patent_app_type] => utility
[patent_app_number] => 13/859388
[patent_app_country] => US
[patent_app_date] => 2013-04-09
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 2
[patent_figures_cnt] => 2
[patent_no_of_words] => 2600
[patent_no_of_claims] => 10
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 185
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13859388
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/859388 | Simple cycle gas turbomachine system having a fuel conditioning system | Apr 8, 2013 | Issued |
Array
(
[id] => 10874234
[patent_doc_number] => 08899013
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2014-12-02
[patent_title] => 'Thrust reverser having locking/unlocking cascade vanes'
[patent_app_type] => utility
[patent_app_number] => 13/855947
[patent_app_country] => US
[patent_app_date] => 2013-04-03
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 8
[patent_no_of_words] => 4026
[patent_no_of_claims] => 6
[patent_no_of_ind_claims] => 2
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[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13855947
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/855947 | Thrust reverser having locking/unlocking cascade vanes | Apr 2, 2013 | Issued |
Array
(
[id] => 9104323
[patent_doc_number] => 20130277454
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2013-10-24
[patent_title] => 'AIRCRAFT PROPULSION ASSEMBLY'
[patent_app_type] => utility
[patent_app_number] => 13/856038
[patent_app_country] => US
[patent_app_date] => 2013-04-03
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
[patent_figures_cnt] => 5
[patent_no_of_words] => 4267
[patent_no_of_claims] => 11
[patent_no_of_ind_claims] => 1
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[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13856038
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/856038 | AIRCRAFT PROPULSION ASSEMBLY | Apr 2, 2013 | Abandoned |
Array
(
[id] => 10197822
[patent_doc_number] => 20150082808
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2015-03-26
[patent_title] => 'GAS TURBINE ENGINES WITH TURBINE AIRFOIL COOLING'
[patent_app_type] => utility
[patent_app_number] => 13/855417
[patent_app_country] => US
[patent_app_date] => 2013-04-02
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 9
[patent_figures_cnt] => 9
[patent_no_of_words] => 4512
[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] => 13855417
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/855417 | Gas turbine engines with turbine airfoil cooling | Apr 1, 2013 | Issued |
Array
(
[id] => 9681228
[patent_doc_number] => 20140237990
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2014-08-28
[patent_title] => 'VARIABLE AREA FAN NOZZLE WITH WALL THICKNESS DISTRIBUTION'
[patent_app_type] => utility
[patent_app_number] => 13/834123
[patent_app_country] => US
[patent_app_date] => 2013-03-15
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
[patent_figures_cnt] => 5
[patent_no_of_words] => 4993
[patent_no_of_claims] => 20
[patent_no_of_ind_claims] => 3
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[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13834123
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/834123 | Variable area fan nozzle with wall thickness distribution | Mar 14, 2013 | Issued |
Array
(
[id] => 9795629
[patent_doc_number] => 20150007573
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2015-01-08
[patent_title] => 'ANNULAR-COMBUSTION-CHAMBER BYPASS'
[patent_app_type] => utility
[patent_app_number] => 14/382918
[patent_app_country] => US
[patent_app_date] => 2013-03-15
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 4
[patent_no_of_words] => 1796
[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] => 14382918
[rel_patent_id] =>[rel_patent_doc_number] =>) 14/382918 | ANNULAR-COMBUSTION-CHAMBER BYPASS | Mar 14, 2013 | Abandoned |
Array
(
[id] => 11805528
[patent_doc_number] => 09546557
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2017-01-17
[patent_title] => 'Nozzle, a nozzle hanger, and a ceramic to metal attachment system'
[patent_app_type] => utility
[patent_app_number] => 13/804402
[patent_app_country] => US
[patent_app_date] => 2013-03-14
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 8
[patent_figures_cnt] => 10
[patent_no_of_words] => 2722
[patent_no_of_claims] => 11
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 141
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13804402
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/804402 | Nozzle, a nozzle hanger, and a ceramic to metal attachment system | Mar 13, 2013 | Issued |
Array
(
[id] => 11192061
[patent_doc_number] => 09422869
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2016-08-23
[patent_title] => 'Systems and methods for gas turbine tuning and control'
[patent_app_type] => utility
[patent_app_number] => 13/801259
[patent_app_country] => US
[patent_app_date] => 2013-03-13
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 9
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[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13801259
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/801259 | Systems and methods for gas turbine tuning and control | Mar 12, 2013 | Issued |
Array
(
[id] => 9201061
[patent_doc_number] => 20140000238
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2014-01-02
[patent_title] => 'LOCKING/UNLOCKING DEVICE FOR A THURST REVERSER WITH A SLIDING COVER AND ADAPTIVE NOZZLE FOR AIRCRAFT ENGINE NACELLE'
[patent_app_type] => utility
[patent_app_number] => 13/801813
[patent_app_country] => US
[patent_app_date] => 2013-03-13
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
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[patent_no_of_words] => 3719
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[patent_current_assignee] =>[type] => publication
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13801813
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/801813 | Locking/unlocking device for a thrust reverser with a sliding cover and adaptive nozzle for aircraft engine nacelle | Mar 12, 2013 | Issued |
Array
(
[id] => 10649946
[patent_doc_number] => 09366188
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2016-06-14
[patent_title] => 'Gas turbine sequence purging process'
[patent_app_type] => utility
[patent_app_number] => 13/801525
[patent_app_country] => US
[patent_app_date] => 2013-03-13
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
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[patent_no_of_words] => 2569
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[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13801525
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/801525 | Gas turbine sequence purging process | Mar 12, 2013 | Issued |
Array
(
[id] => 9724566
[patent_doc_number] => 20140260267
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2014-09-18
[patent_title] => 'COMBUSTOR END COVER WITH FUEL PLENUMS'
[patent_app_type] => utility
[patent_app_number] => 13/797883
[patent_app_country] => US
[patent_app_date] => 2013-03-12
[patent_effective_date] => 0000-00-00
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[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13797883
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/797883 | Combustor end cover with fuel plenums | Mar 11, 2013 | Issued |
Array
(
[id] => 9276610
[patent_doc_number] => 20140026578
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2014-01-30
[patent_title] => 'COMBUSTOR NOZZLE ASSEMBLY, COMBUSTOR EQUIPPED WITH THE SAME, AND GAS TURBINE'
[patent_app_type] => utility
[patent_app_number] => 13/796345
[patent_app_country] => US
[patent_app_date] => 2013-03-12
[patent_effective_date] => 0000-00-00
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[patent_current_assignee] =>[type] => publication
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13796345
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/796345 | Combustor nozzle assembly, combustor equipped with the same, and gas turbine | Mar 11, 2013 | Issued |
Array
(
[id] => 9030352
[patent_doc_number] => 20130232990
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2013-09-12
[patent_title] => 'Apparatus for Releasing a Flow Cross Section of a Gas Line'
[patent_app_type] => utility
[patent_app_number] => 13/790872
[patent_app_country] => US
[patent_app_date] => 2013-03-08
[patent_effective_date] => 0000-00-00
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[patent_current_assignee] =>[type] => publication
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13790872
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/790872 | Apparatus for Releasing a Flow Cross Section of a Gas Line | Mar 7, 2013 | Abandoned |
Array
(
[id] => 8912910
[patent_doc_number] => 20130174535
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2013-07-11
[patent_title] => 'FLUSHING THE EXHAUST GAS RECIRCULATION LINES OF A GAS TURBINE'
[patent_app_type] => utility
[patent_app_number] => 13/783911
[patent_app_country] => US
[patent_app_date] => 2013-03-04
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[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13783911
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/783911 | Flushing the exhaust gas recirculation lines of a gas turbine | Mar 3, 2013 | Issued |
Array
(
[id] => 9696833
[patent_doc_number] => 20140246518
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2014-09-04
[patent_title] => 'FUEL NOZZLE WITH DISCRETE JET INNER AIR SWIRLER'
[patent_app_type] => utility
[patent_app_number] => 13/782969
[patent_app_country] => US
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[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13782969
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/782969 | Fuel nozzle with discrete jet inner air swirler | Feb 28, 2013 | Issued |
Array
(
[id] => 9473037
[patent_doc_number] => 20140130500
[patent_country] => US
[patent_kind] => A9
[patent_issue_date] => 2014-05-15
[patent_title] => 'DESIGN AND MANUFACTURING OF AN ADVANCED LOW COST MICRO-TURBINE SYSTEM'
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[patent_app_number] => 13/782429
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[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13782429
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/782429 | DESIGN AND MANUFACTURING OF AN ADVANCED LOW COST MICRO-TURBINE SYSTEM | Feb 28, 2013 | Abandoned |