
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] => 9201086
[patent_doc_number] => 20140000263
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2014-01-02
[patent_title] => 'MULTI-PREMIXER FUEL NOZZLE SUPPORT SYSTEM'
[patent_app_type] => utility
[patent_app_number] => 14/015322
[patent_app_country] => US
[patent_app_date] => 2013-08-30
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 7
[patent_figures_cnt] => 7
[patent_no_of_words] => 5579
[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] => 14015322
[rel_patent_id] =>[rel_patent_doc_number] =>) 14/015322 | Multi-premixer fuel nozzle support system | Aug 29, 2013 | Issued |
Array
(
[id] => 11685452
[patent_doc_number] => 09683489
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2017-06-20
[patent_title] => 'System and method for preventing ice crystal accretion in gas turbine engines'
[patent_app_type] => utility
[patent_app_number] => 14/014560
[patent_app_country] => US
[patent_app_date] => 2013-08-30
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 3
[patent_no_of_words] => 3478
[patent_no_of_claims] => 13
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 103
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14014560
[rel_patent_id] =>[rel_patent_doc_number] =>) 14/014560 | System and method for preventing ice crystal accretion in gas turbine engines | Aug 29, 2013 | Issued |
Array
(
[id] => 9962524
[patent_doc_number] => 09010125
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2015-04-21
[patent_title] => 'Regeneratively cooled transition duct with transversely buffered impingement nozzles'
[patent_app_type] => utility
[patent_app_number] => 13/956405
[patent_app_country] => US
[patent_app_date] => 2013-08-01
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 2
[patent_figures_cnt] => 2
[patent_no_of_words] => 2511
[patent_no_of_claims] => 17
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 220
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13956405
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/956405 | Regeneratively cooled transition duct with transversely buffered impingement nozzles | Jul 31, 2013 | Issued |
Array
(
[id] => 11923283
[patent_doc_number] => 09790855
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2017-10-17
[patent_title] => 'Apparatus and method for providing damper liquid in a gas turbine engine'
[patent_app_type] => utility
[patent_app_number] => 13/955385
[patent_app_country] => US
[patent_app_date] => 2013-07-31
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 2
[patent_figures_cnt] => 2
[patent_no_of_words] => 2221
[patent_no_of_claims] => 19
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 123
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13955385
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/955385 | Apparatus and method for providing damper liquid in a gas turbine engine | Jul 30, 2013 | Issued |
Array
(
[id] => 9276618
[patent_doc_number] => 20140026586
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2014-01-30
[patent_title] => 'REHEAT BURNER AND METHOD OF MIXING FUEL/CARRIER AIR FLOW WITHIN A REHEAT BURNER'
[patent_app_type] => utility
[patent_app_number] => 13/951507
[patent_app_country] => US
[patent_app_date] => 2013-07-26
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
[patent_figures_cnt] => 5
[patent_no_of_words] => 3171
[patent_no_of_claims] => 13
[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] => 13951507
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/951507 | Reheat burner and method of mixing fuel/carrier air flow within a reheat burner | Jul 25, 2013 | Issued |
Array
(
[id] => 11225744
[patent_doc_number] => 09453460
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2016-09-27
[patent_title] => 'Mixing element for gas turbine units with flue gas recirculation'
[patent_app_type] => utility
[patent_app_number] => 13/948296
[patent_app_country] => US
[patent_app_date] => 2013-07-23
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 12
[patent_figures_cnt] => 7
[patent_no_of_words] => 4473
[patent_no_of_claims] => 20
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 151
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13948296
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/948296 | Mixing element for gas turbine units with flue gas recirculation | Jul 22, 2013 | Issued |
Array
(
[id] => 9265487
[patent_doc_number] => 20140020403
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2014-01-23
[patent_title] => 'SEALING DEVICE, AXIAL TURBINE AND POWER PLANT'
[patent_app_type] => utility
[patent_app_number] => 13/944201
[patent_app_country] => US
[patent_app_date] => 2013-07-17
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 12
[patent_figures_cnt] => 12
[patent_no_of_words] => 6750
[patent_no_of_claims] => 10
[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] => 13944201
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/944201 | SEALING DEVICE, AXIAL TURBINE AND POWER PLANT | Jul 16, 2013 | Abandoned |
Array
(
[id] => 9748138
[patent_doc_number] => 08839601
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2014-09-23
[patent_title] => 'Door for thrust reverser of an aircraft nacelle'
[patent_app_type] => utility
[patent_app_number] => 13/941946
[patent_app_country] => US
[patent_app_date] => 2013-07-15
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 6
[patent_no_of_words] => 3529
[patent_no_of_claims] => 4
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 230
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13941946
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/941946 | Door for thrust reverser of an aircraft nacelle | Jul 14, 2013 | Issued |
Array
(
[id] => 9218984
[patent_doc_number] => 20140013759
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2014-01-16
[patent_title] => 'PREMIX BURNER OF THE MULTI-CONE TYPE FOR A GAS TURBINE'
[patent_app_type] => utility
[patent_app_number] => 13/937502
[patent_app_country] => US
[patent_app_date] => 2013-07-09
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
[patent_figures_cnt] => 5
[patent_no_of_words] => 2145
[patent_no_of_claims] => 9
[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] => 13937502
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/937502 | Premix burner of the multi-cone type for a gas turbine | Jul 8, 2013 | Issued |
Array
(
[id] => 9333277
[patent_doc_number] => 20140060059
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2014-03-06
[patent_title] => 'FUEL DELIVERY SYSTEM WITH A CAVITY COUPLED FUEL INJECTOR'
[patent_app_type] => utility
[patent_app_number] => 13/936836
[patent_app_country] => US
[patent_app_date] => 2013-07-08
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 7
[patent_figures_cnt] => 7
[patent_no_of_words] => 3400
[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] => 13936836
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/936836 | Fuel delivery system with a cavity coupled fuel injector | Jul 7, 2013 | Issued |
Array
(
[id] => 9795630
[patent_doc_number] => 20150007574
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2015-01-08
[patent_title] => 'SYSTEMS AND METHODS FOR CONTROL OF A GAS TURBINE'
[patent_app_type] => utility
[patent_app_number] => 13/937078
[patent_app_country] => US
[patent_app_date] => 2013-07-08
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 4
[patent_no_of_words] => 4530
[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] => 13937078
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/937078 | Systems and methods for control of operating life of a gas turbine | Jul 7, 2013 | Issued |
Array
(
[id] => 11238173
[patent_doc_number] => 09464809
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2016-10-11
[patent_title] => 'Gas turbine combustor and operating method for gas turbine combustor'
[patent_app_type] => utility
[patent_app_number] => 13/933227
[patent_app_country] => US
[patent_app_date] => 2013-07-02
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 9
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[patent_no_of_words] => 7011
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[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13933227
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/933227 | Gas turbine combustor and operating method for gas turbine combustor | Jul 1, 2013 | Issued |
Array
(
[id] => 10970473
[patent_doc_number] => 20140373506
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2014-12-25
[patent_title] => 'REVERSE SCISSOR THRIST REVERSER FOR A TURBINE ENGINE'
[patent_app_type] => utility
[patent_app_number] => 13/921877
[patent_app_country] => US
[patent_app_date] => 2013-06-19
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 8
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[patent_no_of_words] => 3909
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[patent_current_assignee] =>[type] => publication
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13921877
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/921877 | Reverse scissor thrust reverser for a turbine engine | Jun 18, 2013 | Issued |
Array
(
[id] => 11198902
[patent_doc_number] => 09429105
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2016-08-30
[patent_title] => 'Rocket vehicle with integrated attitude control and thrust vectoring'
[patent_app_type] => utility
[patent_app_number] => 13/912837
[patent_app_country] => US
[patent_app_date] => 2013-06-07
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
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[patent_no_of_words] => 2798
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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] => 13912837
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/912837 | Rocket vehicle with integrated attitude control and thrust vectoring | Jun 6, 2013 | Issued |
Array
(
[id] => 10949776
[patent_doc_number] => 20140352797
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2014-12-04
[patent_title] => 'AIRCRAFT JET ENGINE'
[patent_app_type] => utility
[patent_app_number] => 13/909772
[patent_app_country] => US
[patent_app_date] => 2013-06-04
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
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[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13909772
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/909772 | AIRCRAFT JET ENGINE | Jun 3, 2013 | Abandoned |
Array
(
[id] => 11191264
[patent_doc_number] => 09422063
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2016-08-23
[patent_title] => 'Cooled cooling air system for a gas turbine'
[patent_app_type] => utility
[patent_app_number] => 13/907187
[patent_app_country] => US
[patent_app_date] => 2013-05-31
[patent_effective_date] => 0000-00-00
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[patent_no_of_words] => 4134
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[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13907187
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/907187 | Cooled cooling air system for a gas turbine | May 30, 2013 | Issued |
Array
(
[id] => 9063503
[patent_doc_number] => 20130255259
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2013-10-03
[patent_title] => 'POWER RECOVERY FOR USE IN START-UP OR RE-START OF A PURE TEREPHTHALIC ACID PRODUCTION PROCESS'
[patent_app_type] => utility
[patent_app_number] => 13/901666
[patent_app_country] => US
[patent_app_date] => 2013-05-24
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
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[patent_no_of_words] => 5767
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[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13901666
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/901666 | POWER RECOVERY FOR USE IN START-UP OR RE-START OF A PURE TEREPHTHALIC ACID PRODUCTION PROCESS | May 23, 2013 | Abandoned |
Array
(
[id] => 10407395
[patent_doc_number] => 20150292404
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2015-10-15
[patent_title] => 'PROCESS AND EQUIPMENT FOR COAL GASIFICATION, AND POWER GENERATION SYSTEM AND POWER GENERATION PROCESS THEREOF'
[patent_app_type] => utility
[patent_app_number] => 14/373181
[patent_app_country] => US
[patent_app_date] => 2013-05-22
[patent_effective_date] => 0000-00-00
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[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14373181
[rel_patent_id] =>[rel_patent_doc_number] =>) 14/373181 | Process and equipment for coal gasification, and power generation system and power generation process thereof | May 21, 2013 | Issued |
Array
(
[id] => 10942271
[patent_doc_number] => 20140345292
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2014-11-27
[patent_title] => 'RETURN FLUID AIR COOLER SYSTEM FOR TURBINE COOLING WITH OPTIONAL POWER EXTRACTION'
[patent_app_type] => utility
[patent_app_number] => 13/900189
[patent_app_country] => US
[patent_app_date] => 2013-05-22
[patent_effective_date] => 0000-00-00
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[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13900189
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/900189 | Return fluid air cooler system for turbine cooling with optional power extraction | May 21, 2013 | Issued |
Array
(
[id] => 9157454
[patent_doc_number] => 20130305731
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2013-11-21
[patent_title] => 'METHODS AND APPARATUS FOR PROVIDING FLUIDIC INSERTS INTO AN EXHAUST STREAM TO REDUCE JET NOISE FROM A NOZZLE'
[patent_app_type] => utility
[patent_app_number] => 13/894050
[patent_app_country] => US
[patent_app_date] => 2013-05-14
[patent_effective_date] => 0000-00-00
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[patent_current_assignee] =>[type] => publication
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13894050
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/894050 | METHODS AND APPARATUS FOR PROVIDING FLUIDIC INSERTS INTO AN EXHAUST STREAM TO REDUCE JET NOISE FROM A NOZZLE | May 13, 2013 | Abandoned |