Search

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 numberTitle of the applicationFiling DateStatus
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 [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] => 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 [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] => 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 [patent_figures_cnt] => 6 [patent_no_of_words] => 6408 [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] => 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 [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] => 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 [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] => 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 [patent_figures_cnt] => 5 [patent_no_of_words] => 5125 [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] => 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 [patent_figures_cnt] => 6 [patent_no_of_words] => 9275 [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] => 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 [patent_figures_cnt] => 3 [patent_no_of_words] => 5148 [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] => 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 [patent_figures_cnt] => 9 [patent_no_of_words] => 4883 [patent_no_of_claims] => 19 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 146 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 12979028 [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 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 4 [patent_figures_cnt] => 4 [patent_no_of_words] => 5299 [patent_no_of_claims] => 19 [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] => 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 [patent_drawing_sheets_cnt] => 10 [patent_figures_cnt] => 10 [patent_no_of_words] => 3978 [patent_no_of_claims] => 10 [patent_no_of_ind_claims] => 7 [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] => 13516683 [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 [patent_drawing_sheets_cnt] => 14 [patent_figures_cnt] => 14 [patent_no_of_words] => 7461 [patent_no_of_claims] => 31 [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] => 12956191 [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 [patent_app_date] => 2010-11-22 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 2 [patent_figures_cnt] => 2 [patent_no_of_words] => 3676 [patent_no_of_claims] => 21 [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] => publications/A1/0154/20110154830.pdf [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 ( [id] => 8190285 [patent_doc_number] => 20120117941 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2012-05-17 [patent_title] => 'FLIGHT VEHICLES INCLUDING ELECTRICALLY-INTERCONNECTIVE SUPPORT STRUCTURES AND METHODS FOR THE MANUFACTURE THEREOF' [patent_app_type] => utility [patent_app_number] => 12/945440 [patent_app_country] => US [patent_app_date] => 2010-11-12 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 8 [patent_figures_cnt] => 8 [patent_no_of_words] => 6765 [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] => publications/A1/0117/20120117941.pdf [firstpage_image] =>[orig_patent_app_number] => 12945440 [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 [patent_doc_number] => 20120111012 [patent_country] => US [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 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 5 [patent_figures_cnt] => 5 [patent_no_of_words] => 3602 [patent_no_of_claims] => 21 [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] => publications/A1/0111/20120111012.pdf [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
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