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] => 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 [patent_no_of_claims] => 7 [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] => 15434284 [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 [patent_drawing_sheets_cnt] => 0 [patent_figures_cnt] => 0 [patent_no_of_words] => 4757 [patent_no_of_claims] => 0 [patent_no_of_ind_claims] => -17 [patent_words_short_claim] => 14 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [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 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 9 [patent_figures_cnt] => 9 [patent_no_of_words] => 20649 [patent_no_of_claims] => 25 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 341 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 15777767 [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 [patent_figures_cnt] => 0 [patent_no_of_words] => 19864 [patent_no_of_claims] => 0 [patent_no_of_ind_claims] => -12 [patent_words_short_claim] => 2 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 15778122 [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 [patent_figures_cnt] => 0 [patent_no_of_words] => 17896 [patent_no_of_claims] => 0 [patent_no_of_ind_claims] => -15 [patent_words_short_claim] => 109 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [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 [patent_drawing_sheets_cnt] => 0 [patent_figures_cnt] => 0 [patent_no_of_words] => 4880 [patent_no_of_claims] => 0 [patent_no_of_ind_claims] => -17 [patent_words_short_claim] => 76 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 15351803 [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 [patent_figures_cnt] => 13 [patent_no_of_words] => 2868 [patent_no_of_claims] => 20 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 202 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 15339463 [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 [patent_figures_cnt] => 5 [patent_no_of_words] => 8121 [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] => 15296222 [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 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 3 [patent_figures_cnt] => 4 [patent_no_of_words] => 4175 [patent_no_of_claims] => 20 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 145 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 15293368 [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 [patent_drawing_sheets_cnt] => 7 [patent_figures_cnt] => 12 [patent_no_of_words] => 5072 [patent_no_of_claims] => 10 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 304 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 15292485 [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 [patent_app_number] => 15/292852 [patent_app_country] => US [patent_app_date] => 2016-10-13 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 8 [patent_figures_cnt] => 8 [patent_no_of_words] => 5448 [patent_no_of_claims] => 13 [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] => 15292852 [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 [patent_app_number] => 15/292676 [patent_app_country] => US [patent_app_date] => 2016-10-13 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 6 [patent_figures_cnt] => 6 [patent_no_of_words] => 7213 [patent_no_of_claims] => 26 [patent_no_of_ind_claims] => 4 [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] => 15292676 [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 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2018-04-19 [patent_title] => TRANSITION DUCT FORMED OF A PLURALITY OF SEGMENTS [patent_app_type] => utility [patent_app_number] => 15/292390 [patent_app_country] => US [patent_app_date] => 2016-10-13 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 0 [patent_figures_cnt] => 0 [patent_no_of_words] => 3079 [patent_no_of_claims] => 0 [patent_no_of_ind_claims] => -18 [patent_words_short_claim] => 70 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 15292390 [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 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2019-08-27 [patent_title] => Shafting arrangement for a gas turbine engine [patent_app_type] => utility [patent_app_number] => 15/262612 [patent_app_country] => US [patent_app_date] => 2016-09-12 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 4 [patent_figures_cnt] => 7 [patent_no_of_words] => 4336 [patent_no_of_claims] => 16 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 195 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 15262612 [rel_patent_id] =>[rel_patent_doc_number] =>)
15/262612
Shafting arrangement for a gas turbine engine Sep 11, 2016 Issued
Array ( [id] => 14059163 [patent_doc_number] => 10233868 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2019-03-19 [patent_title] => Efficient, low pressure ratio propulsor for gas turbine engines [patent_app_type] => utility [patent_app_number] => 15/252811 [patent_app_country] => US [patent_app_date] => 2016-08-31 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 2 [patent_figures_cnt] => 2 [patent_no_of_words] => 1936 [patent_no_of_claims] => 28 [patent_no_of_ind_claims] => 4 [patent_words_short_claim] => 119 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 15252811 [rel_patent_id] =>[rel_patent_doc_number] =>)
15/252811
Efficient, low pressure ratio propulsor for gas turbine engines Aug 30, 2016 Issued
Array ( [id] => 11350963 [patent_doc_number] => 20160369703 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2016-12-22 [patent_title] => 'EFFICIENT, LOW PRESSURE RATIO PROPULSOR FOR GAS TURBINE ENGINES' [patent_app_type] => utility [patent_app_number] => 15/233142 [patent_app_country] => US [patent_app_date] => 2016-08-10 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 4 [patent_figures_cnt] => 4 [patent_no_of_words] => 4059 [patent_no_of_claims] => 30 [patent_no_of_ind_claims] => 4 [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] => 15233142 [rel_patent_id] =>[rel_patent_doc_number] =>)
15/233142
Efficient, low pressure ratio propulsor for gas turbine engines Aug 9, 2016 Issued
Array ( [id] => 11121645 [patent_doc_number] => 20160318619 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2016-11-03 [patent_title] => 'COOLED COOLING AIR SYSTEM FOR A GAS TURBINE' [patent_app_type] => utility [patent_app_number] => 15/209880 [patent_app_country] => US [patent_app_date] => 2016-07-14 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 11 [patent_figures_cnt] => 11 [patent_no_of_words] => 4138 [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] => 15209880 [rel_patent_id] =>[rel_patent_doc_number] =>)
15/209880
Cooled cooling air system for a gas turbine Jul 13, 2016 Issued
Array ( [id] => 14361503 [patent_doc_number] => 10302042 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2019-05-28 [patent_title] => Variable area fan nozzle with wall thickness distribution [patent_app_type] => utility [patent_app_number] => 15/177657 [patent_app_country] => US [patent_app_date] => 2016-06-09 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 4 [patent_figures_cnt] => 12 [patent_no_of_words] => 4448 [patent_no_of_claims] => 12 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 109 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 15177657 [rel_patent_id] =>[rel_patent_doc_number] =>)
15/177657
Variable area fan nozzle with wall thickness distribution Jun 8, 2016 Issued
Array ( [id] => 12981970 [patent_doc_number] => 20170342910 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2017-11-30 [patent_title] => ATTACHMENT SYSTEM FOR A GAS TURBINE ENGINE [patent_app_type] => utility [patent_app_number] => 15/163747 [patent_app_country] => US [patent_app_date] => 2016-05-25 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 0 [patent_figures_cnt] => 0 [patent_no_of_words] => 5590 [patent_no_of_claims] => 0 [patent_no_of_ind_claims] => -18 [patent_words_short_claim] => 83 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 15163747 [rel_patent_id] =>[rel_patent_doc_number] =>)
15/163747
ATTACHMENT SYSTEM FOR A GAS TURBINE ENGINE May 24, 2016 Abandoned
Array ( [id] => 14552311 [patent_doc_number] => 10344604 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2019-07-09 [patent_title] => Turbomachine diffuser including flow mixing lobes and method [patent_app_type] => utility [patent_app_number] => 15/159850 [patent_app_country] => US [patent_app_date] => 2016-05-20 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 5 [patent_figures_cnt] => 10 [patent_no_of_words] => 2178 [patent_no_of_claims] => 20 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 139 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 15159850 [rel_patent_id] =>[rel_patent_doc_number] =>)
15/159850
Turbomachine diffuser including flow mixing lobes and method May 19, 2016 Issued
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