
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] => 8449713
[patent_doc_number] => 20120260659
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2012-10-18
[patent_title] => 'INTERFACE BETWEEN A COMBUSTOR BASKET AND A TRANSITION OF A GAS TURBINE ENGINE'
[patent_app_type] => utility
[patent_app_number] => 13/088507
[patent_app_country] => US
[patent_app_date] => 2011-04-18
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
[patent_figures_cnt] => 5
[patent_no_of_words] => 3600
[patent_no_of_claims] => 19
[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] => 13088507
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/088507 | Interface between a combustor basket and a transition of a gas turbine engine | Apr 17, 2011 | Issued |
Array
(
[id] => 11800186
[patent_doc_number] => 09541007
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2017-01-10
[patent_title] => 'Coupling shaft for gas turbine fan drive gear system'
[patent_app_type] => utility
[patent_app_number] => 13/087446
[patent_app_country] => US
[patent_app_date] => 2011-04-15
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 4
[patent_no_of_words] => 1964
[patent_no_of_claims] => 17
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 106
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13087446
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/087446 | Coupling shaft for gas turbine fan drive gear system | Apr 14, 2011 | Issued |
Array
(
[id] => 8449714
[patent_doc_number] => 20120260660
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2012-10-18
[patent_title] => 'Stoichiometric Exhaust Gas Recirculation Combustor'
[patent_app_type] => utility
[patent_app_number] => 13/087463
[patent_app_country] => US
[patent_app_date] => 2011-04-15
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 2
[patent_figures_cnt] => 2
[patent_no_of_words] => 2074
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[patent_current_assignee] =>[type] => publication
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13087463
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/087463 | Stoichiometric exhaust gas recirculation combustor with extraction port for cooling air | Apr 14, 2011 | Issued |
Array
(
[id] => 8401918
[patent_doc_number] => 20120233978
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2012-09-20
[patent_title] => 'APPARATUS FOR STARTING UP COMBINED CYCLE POWER SYSTEMS AND METHOD FOR ASSEMBLING SAME'
[patent_app_type] => utility
[patent_app_number] => 13/051661
[patent_app_country] => US
[patent_app_date] => 2011-03-18
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 6
[patent_figures_cnt] => 6
[patent_no_of_words] => 5461
[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] => 13051661
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/051661 | Apparatus for starting up combined cycle power systems and method for assembling same | Mar 17, 2011 | Issued |
Array
(
[id] => 8343612
[patent_doc_number] => 20120204534
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2012-08-16
[patent_title] => 'SYSTEM AND METHOD FOR DAMPING PRESSURE OSCILLATIONS WITHIN A PULSE DETONATION ENGINE'
[patent_app_type] => utility
[patent_app_number] => 13/028099
[patent_app_country] => US
[patent_app_date] => 2011-02-15
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
[patent_figures_cnt] => 5
[patent_no_of_words] => 6977
[patent_no_of_claims] => 20
[patent_no_of_ind_claims] => 3
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[patent_maintenance] => 1
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[patent_current_assignee] =>[type] => publication
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13028099
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/028099 | SYSTEM AND METHOD FOR DAMPING PRESSURE OSCILLATIONS WITHIN A PULSE DETONATION ENGINE | Feb 14, 2011 | Abandoned |
Array
(
[id] => 8332111
[patent_doc_number] => 20120198811
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2012-08-09
[patent_title] => 'POWER GENERATION SYSTEM AND METHODS FOR MONITORING OPERATION OF SAME'
[patent_app_type] => utility
[patent_app_number] => 13/024014
[patent_app_country] => US
[patent_app_date] => 2011-02-09
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 6
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[patent_no_of_words] => 6408
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[patent_current_assignee] =>[type] => publication
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13024014
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/024014 | Power generation system and methods for monitoring operation of same | Feb 8, 2011 | Issued |
Array
(
[id] => 9872668
[patent_doc_number] => 08959927
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2015-02-24
[patent_title] => 'Pitot tube with increased particle separation for a compressor bleed system of a gas turbine engine'
[patent_app_type] => utility
[patent_app_number] => 13/017146
[patent_app_country] => US
[patent_app_date] => 2011-01-31
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 3
[patent_no_of_words] => 2455
[patent_no_of_claims] => 17
[patent_no_of_ind_claims] => 4
[patent_words_short_claim] => 102
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13017146
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/017146 | Pitot tube with increased particle separation for a compressor bleed system of a gas turbine engine | Jan 30, 2011 | Issued |
Array
(
[id] => 5953986
[patent_doc_number] => 20110179796
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2011-07-28
[patent_title] => 'HELMHOLTZ DAMPER FOR A COMBUSTOR OF A GAS TURBINE AND A METHOD FOR INSTALLING THE HELMHOLTZ DAMPER'
[patent_app_type] => utility
[patent_app_number] => 13/015640
[patent_app_country] => US
[patent_app_date] => 2011-01-28
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
[patent_figures_cnt] => 5
[patent_no_of_words] => 2669
[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] => publications/A1/0179/20110179796.pdf
[firstpage_image] =>[orig_patent_app_number] => 13015640
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/015640 | Helmholtz damper for a combustor of a gas turbine and a method for installing the helmholtz damper | Jan 27, 2011 | Issued |
Array
(
[id] => 8320134
[patent_doc_number] => 20120192546
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2012-08-02
[patent_title] => 'Catalytic Converter for a Pulse Detonation Turbine Engine'
[patent_app_type] => utility
[patent_app_number] => 13/015617
[patent_app_country] => US
[patent_app_date] => 2011-01-28
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 4
[patent_no_of_words] => 2420
[patent_no_of_claims] => 20
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[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13015617
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/015617 | Catalytic Converter for a Pulse Detonation Turbine Engine | Jan 27, 2011 | Abandoned |
Array
(
[id] => 8309243
[patent_doc_number] => 20120186264
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2012-07-26
[patent_title] => 'GAS TURBINE COMBUSTOR'
[patent_app_type] => utility
[patent_app_number] => 13/012254
[patent_app_country] => US
[patent_app_date] => 2011-01-24
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 6
[patent_figures_cnt] => 6
[patent_no_of_words] => 5120
[patent_no_of_claims] => 13
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[patent_maintenance] => 1
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[patent_current_assignee] =>[type] => publication
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13012254
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/012254 | Gas turbine combustor with liner air admission holes associated with interspersed main and pilot swirler assemblies | Jan 23, 2011 | Issued |
Array
(
[id] => 8298314
[patent_doc_number] => 20120180873
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2012-07-19
[patent_title] => 'METHOD FOR REPLICATING A PRESSURE CONTROL VALVE WITH ADJUSTABLE RESPONSE CHARACTERISTIC'
[patent_app_type] => utility
[patent_app_number] => 13/007295
[patent_app_country] => US
[patent_app_date] => 2011-01-14
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
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[patent_no_of_words] => 5125
[patent_no_of_claims] => 20
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[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13007295
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/007295 | METHOD FOR REPLICATING A PRESSURE CONTROL VALVE WITH ADJUSTABLE RESPONSE CHARACTERISTIC | Jan 13, 2011 | Abandoned |
Array
(
[id] => 8286263
[patent_doc_number] => 20120174590
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2012-07-12
[patent_title] => 'SYSTEM AND METHOD FOR CONTROLLING COMBUSTOR OPERATING CONDITIONS BASED ON FLAME DETECTION'
[patent_app_type] => utility
[patent_app_number] => 12/986227
[patent_app_country] => US
[patent_app_date] => 2011-01-07
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 6
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[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 12986227
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/986227 | System and method for controlling combustor operating conditions based on flame detection | Jan 6, 2011 | Issued |
Array
(
[id] => 8177771
[patent_doc_number] => 20120111024
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2012-05-10
[patent_title] => 'GAS TURBINE ENGINE AND HIGH SPEED ROLLING ELEMENT BEARING'
[patent_app_type] => utility
[patent_app_number] => 12/981010
[patent_app_country] => US
[patent_app_date] => 2010-12-29
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
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[pdf_file] => publications/A1/0111/20120111024.pdf
[firstpage_image] =>[orig_patent_app_number] => 12981010
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/981010 | Gas turbine engine and high speed rolling element bearing | Dec 28, 2010 | Issued |
Array
(
[id] => 10886480
[patent_doc_number] => 08910465
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2014-12-16
[patent_title] => 'Gas turbine engine and heat exchange system'
[patent_app_type] => utility
[patent_app_number] => 12/979028
[patent_app_country] => US
[patent_app_date] => 2010-12-27
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 7
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[rel_patent_id] =>[rel_patent_doc_number] =>) 12/979028 | Gas turbine engine and heat exchange system | Dec 26, 2010 | Issued |
Array
(
[id] => 8247573
[patent_doc_number] => 20120151895
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2012-06-21
[patent_title] => 'HOT GAS PATH COMPONENT COOLING FOR HYBRID PULSE DETONATION COMBUSTION SYSTEMS'
[patent_app_type] => utility
[patent_app_number] => 12/974031
[patent_app_country] => US
[patent_app_date] => 2010-12-21
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[pdf_file] => publications/A1/0151/20120151895.pdf
[firstpage_image] =>[orig_patent_app_number] => 12974031
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/974031 | HOT GAS PATH COMPONENT COOLING FOR HYBRID PULSE DETONATION COMBUSTION SYSTEMS | Dec 20, 2010 | Abandoned |
Array
(
[id] => 8959591
[patent_doc_number] => 20130199193
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2013-08-08
[patent_title] => 'TUNGSTEN CARBIDE INSERTS AND METHOD'
[patent_app_type] => utility
[patent_app_number] => 13/516683
[patent_app_country] => US
[patent_app_date] => 2010-12-09
[patent_effective_date] => 0000-00-00
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[rel_patent_id] =>[rel_patent_doc_number] =>) 13/516683 | TUNGSTEN CARBIDE INSERTS AND METHOD | Dec 8, 2010 | Abandoned |
Array
(
[id] => 8215297
[patent_doc_number] => 20120131926
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2012-05-31
[patent_title] => 'ADVANCED LASER IGNITION SYSTEMS FOR GAS TURBINES INCLUDING AIRCRAFT ENGINES'
[patent_app_type] => utility
[patent_app_number] => 12/956191
[patent_app_country] => US
[patent_app_date] => 2010-11-30
[patent_effective_date] => 0000-00-00
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[rel_patent_id] =>[rel_patent_doc_number] =>) 12/956191 | Advanced laser ignition systems for gas turbines including aircraft engines | Nov 29, 2010 | Issued |
Array
(
[id] => 6150487
[patent_doc_number] => 20110154830
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2011-06-30
[patent_title] => 'GAS TURBINE ENGINE SURGE MARGIN BLEED POWER RECUPERATION'
[patent_app_type] => utility
[patent_app_number] => 12/951274
[patent_app_country] => US
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[firstpage_image] =>[orig_patent_app_number] => 12951274
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/951274 | Gas turbine engine surge margin bleed power recuperation | Nov 21, 2010 | Issued |
Array
(
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[patent_title] => 'FLIGHT VEHICLES INCLUDING ELECTRICALLY-INTERCONNECTIVE SUPPORT STRUCTURES AND METHODS FOR THE MANUFACTURE THEREOF'
[patent_app_type] => utility
[patent_app_number] => 12/945440
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[rel_patent_id] =>[rel_patent_doc_number] =>) 12/945440 | Flight vehicles including electrically-interconnective support structures and methods for the manufacture thereof | Nov 11, 2010 | Issued |
Array
(
[id] => 8177760
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[patent_kind] => A1
[patent_issue_date] => 2012-05-10
[patent_title] => 'Ultra low emissions gas turbine combustor'
[patent_app_type] => utility
[patent_app_number] => 12/926322
[patent_app_country] => US
[patent_app_date] => 2010-11-09
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[firstpage_image] =>[orig_patent_app_number] => 12926322
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/926322 | Ultra low emissions gas turbine combustor | Nov 8, 2010 | Issued |