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] => 8132287 [patent_doc_number] => 20120090694 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2012-04-19 [patent_title] => 'AIRCRAFT NACELLE INCLUDING A REAR FRAME INCLINED TO THE REAR' [patent_app_type] => utility [patent_app_number] => 13/270536 [patent_app_country] => US [patent_app_date] => 2011-10-11 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 5 [patent_figures_cnt] => 5 [patent_no_of_words] => 2419 [patent_no_of_claims] => 12 [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/A1/0090/20120090694.pdf [firstpage_image] =>[orig_patent_app_number] => 13270536 [rel_patent_id] =>[rel_patent_doc_number] =>)
13/270536
Aircraft nacelle including a rear frame inclined to the rear Oct 10, 2011 Issued
Array ( [id] => 8752609 [patent_doc_number] => 20130086913 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2013-04-11 [patent_title] => 'TURBOMACHINE COMBUSTOR ASSEMBLY INCLUDING A COMBUSTION DYNAMICS MITIGATION SYSTEM' [patent_app_type] => utility [patent_app_number] => 13/269090 [patent_app_country] => US [patent_app_date] => 2011-10-07 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 5 [patent_figures_cnt] => 5 [patent_no_of_words] => 2288 [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] => 13269090 [rel_patent_id] =>[rel_patent_doc_number] =>)
13/269090
TURBOMACHINE COMBUSTOR ASSEMBLY INCLUDING A COMBUSTION DYNAMICS MITIGATION SYSTEM Oct 6, 2011 Abandoned
Array ( [id] => 8602833 [patent_doc_number] => 20130008145 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2013-01-10 [patent_title] => 'INTEGRATED ELECTRIC VARIABLE AREA FAN NOZZLE THRUST REVERSAL ACTUATION SYSTEM' [patent_app_type] => utility [patent_app_number] => 13/252305 [patent_app_country] => US [patent_app_date] => 2011-10-04 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 4 [patent_figures_cnt] => 4 [patent_no_of_words] => 3092 [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] => 13252305 [rel_patent_id] =>[rel_patent_doc_number] =>)
13/252305
Integrated electric variable area fan nozzle thrust reversal actuation system Oct 3, 2011 Issued
Array ( [id] => 8438696 [patent_doc_number] => 20120255311 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2012-10-11 [patent_title] => 'COOLING STRUCTURE, GAS TURBINE COMBUSTOR AND MANUFACTURING METHOD OF COOLING STRUCTURE' [patent_app_type] => utility [patent_app_number] => 13/241594 [patent_app_country] => US [patent_app_date] => 2011-09-23 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 10 [patent_figures_cnt] => 10 [patent_no_of_words] => 4982 [patent_no_of_claims] => 8 [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] => 13241594 [rel_patent_id] =>[rel_patent_doc_number] =>)
13/241594
COOLING STRUCTURE, GAS TURBINE COMBUSTOR AND MANUFACTURING METHOD OF COOLING STRUCTURE Sep 22, 2011 Abandoned
Array ( [id] => 10149618 [patent_doc_number] => 09181898 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2015-11-10 [patent_title] => 'Thrust reverser for a gas turbine engine with moveable doors' [patent_app_type] => utility [patent_app_number] => 13/237296 [patent_app_country] => US [patent_app_date] => 2011-09-20 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 6 [patent_figures_cnt] => 6 [patent_no_of_words] => 2455 [patent_no_of_claims] => 24 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 121 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13237296 [rel_patent_id] =>[rel_patent_doc_number] =>)
13/237296
Thrust reverser for a gas turbine engine with moveable doors Sep 19, 2011 Issued
Array ( [id] => 8704282 [patent_doc_number] => 20130061571 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2013-03-14 [patent_title] => 'Laser propelled flight vehicle' [patent_app_type] => utility [patent_app_number] => 13/199992 [patent_app_country] => US [patent_app_date] => 2011-09-14 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 9 [patent_figures_cnt] => 9 [patent_no_of_words] => 4559 [patent_no_of_claims] => 3 [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] => 13199992 [rel_patent_id] =>[rel_patent_doc_number] =>)
13/199992
Laser propelled flight vehicle Sep 13, 2011 Abandoned
Array ( [id] => 11197507 [patent_doc_number] => 09427703 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2016-08-30 [patent_title] => 'CO2 separation and recovery equipment, and a coal gasification combined power plant comprising CO2 separation and recovery equipment' [patent_app_type] => utility [patent_app_number] => 13/877412 [patent_app_country] => US [patent_app_date] => 2011-09-12 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 5 [patent_figures_cnt] => 5 [patent_no_of_words] => 6466 [patent_no_of_claims] => 7 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 336 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13877412 [rel_patent_id] =>[rel_patent_doc_number] =>)
13/877412
CO2 separation and recovery equipment, and a coal gasification combined power plant comprising CO2 separation and recovery equipment Sep 11, 2011 Issued
Array ( [id] => 10142801 [patent_doc_number] => 09175604 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2015-11-03 [patent_title] => 'Gas turbine engine with high and intermediate temperature compressed air zones' [patent_app_type] => utility [patent_app_number] => 13/227769 [patent_app_country] => US [patent_app_date] => 2011-09-08 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 5 [patent_figures_cnt] => 6 [patent_no_of_words] => 1718 [patent_no_of_claims] => 17 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 79 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13227769 [rel_patent_id] =>[rel_patent_doc_number] =>)
13/227769
Gas turbine engine with high and intermediate temperature compressed air zones Sep 7, 2011 Issued
Array ( [id] => 9887128 [patent_doc_number] => 08973371 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2015-03-10 [patent_title] => 'Gas turbine engine with turbine cooling arrangement' [patent_app_type] => utility [patent_app_number] => 13/224894 [patent_app_country] => US [patent_app_date] => 2011-09-02 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 3 [patent_figures_cnt] => 3 [patent_no_of_words] => 3860 [patent_no_of_claims] => 13 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 190 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13224894 [rel_patent_id] =>[rel_patent_doc_number] =>)
13/224894
Gas turbine engine with turbine cooling arrangement Sep 1, 2011 Issued
Array ( [id] => 8396517 [patent_doc_number] => 08266883 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2012-09-18 [patent_title] => 'Power plant start-up method and method of venting the power plant' [patent_app_type] => utility [patent_app_number] => 13/217646 [patent_app_country] => US [patent_app_date] => 2011-08-25 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 2 [patent_figures_cnt] => 2 [patent_no_of_words] => 13184 [patent_no_of_claims] => 20 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 292 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13217646 [rel_patent_id] =>[rel_patent_doc_number] =>)
13/217646
Power plant start-up method and method of venting the power plant Aug 24, 2011 Issued
Array ( [id] => 10156301 [patent_doc_number] => 09188065 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2015-11-17 [patent_title] => 'APU selective cool down cycle' [patent_app_type] => utility [patent_app_number] => 13/197178 [patent_app_country] => US [patent_app_date] => 2011-08-03 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 1 [patent_figures_cnt] => 2 [patent_no_of_words] => 1062 [patent_no_of_claims] => 12 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 131 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13197178 [rel_patent_id] =>[rel_patent_doc_number] =>)
13/197178
APU selective cool down cycle Aug 2, 2011 Issued
Array ( [id] => 10097463 [patent_doc_number] => 09133767 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2015-09-15 [patent_title] => 'Fuel injecting assembly for gas turbine engine including cooling gap between supply structures' [patent_app_type] => utility [patent_app_number] => 13/195915 [patent_app_country] => US [patent_app_date] => 2011-08-02 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 5 [patent_figures_cnt] => 5 [patent_no_of_words] => 4239 [patent_no_of_claims] => 20 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 242 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13195915 [rel_patent_id] =>[rel_patent_doc_number] =>)
13/195915
Fuel injecting assembly for gas turbine engine including cooling gap between supply structures Aug 1, 2011 Issued
Array ( [id] => 10193771 [patent_doc_number] => 09222674 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2015-12-29 [patent_title] => 'Multi-stage amplification vortex mixture for gas turbine engine combustor' [patent_app_type] => utility [patent_app_number] => 13/188451 [patent_app_country] => US [patent_app_date] => 2011-07-21 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 7 [patent_figures_cnt] => 10 [patent_no_of_words] => 3706 [patent_no_of_claims] => 20 [patent_no_of_ind_claims] => 4 [patent_words_short_claim] => 91 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13188451 [rel_patent_id] =>[rel_patent_doc_number] =>)
13/188451
Multi-stage amplification vortex mixture for gas turbine engine combustor Jul 20, 2011 Issued
Array ( [id] => 7748025 [patent_doc_number] => 20120023900 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2012-02-02 [patent_title] => 'AIRCRAFT NACELLE' [patent_app_type] => utility [patent_app_number] => 13/185954 [patent_app_country] => US [patent_app_date] => 2011-07-19 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 3 [patent_figures_cnt] => 3 [patent_no_of_words] => 2487 [patent_no_of_claims] => 8 [patent_no_of_ind_claims] => 5 [patent_words_short_claim] => 0 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] => publications/A1/0023/20120023900.pdf [firstpage_image] =>[orig_patent_app_number] => 13185954 [rel_patent_id] =>[rel_patent_doc_number] =>)
13/185954
Pivoting door for thrust reverser with stable intermediate position Jul 18, 2011 Issued
Array ( [id] => 10649945 [patent_doc_number] => 09366186 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2016-06-14 [patent_title] => 'Lateral turbojet improved in order to limit the deformation thereof' [patent_app_type] => utility [patent_app_number] => 13/813071 [patent_app_country] => US [patent_app_date] => 2011-07-15 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 3 [patent_figures_cnt] => 7 [patent_no_of_words] => 2206 [patent_no_of_claims] => 13 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 164 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13813071 [rel_patent_id] =>[rel_patent_doc_number] =>)
13/813071
Lateral turbojet improved in order to limit the deformation thereof Jul 14, 2011 Issued
Array ( [id] => 8752604 [patent_doc_number] => 20130086908 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2013-04-11 [patent_title] => 'GAS TURBINE COMBUSTION CHAMBER ARRANGEMENT OF AXIAL TYPE OF CONSTRUCTION' [patent_app_type] => utility [patent_app_number] => 13/704972 [patent_app_country] => US [patent_app_date] => 2011-06-15 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 4 [patent_figures_cnt] => 4 [patent_no_of_words] => 2652 [patent_no_of_claims] => 20 [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] => 13704972 [rel_patent_id] =>[rel_patent_doc_number] =>)
13/704972
Gas turbine combustion chamber arrangement of axial type of construction Jun 14, 2011 Issued
Array ( [id] => 9920406 [patent_doc_number] => 08978353 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2015-03-17 [patent_title] => 'Systems and methods for using an endothermic fuel with a high heat sink capacity for aircraft waste heat rejection' [patent_app_type] => utility [patent_app_number] => 13/118800 [patent_app_country] => US [patent_app_date] => 2011-05-31 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 1 [patent_figures_cnt] => 2 [patent_no_of_words] => 6119 [patent_no_of_claims] => 20 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 159 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13118800 [rel_patent_id] =>[rel_patent_doc_number] =>)
13/118800
Systems and methods for using an endothermic fuel with a high heat sink capacity for aircraft waste heat rejection May 30, 2011 Issued
Array ( [id] => 10114930 [patent_doc_number] => 09149795 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2015-10-06 [patent_title] => 'Corrosion resistant catalysts for decomposition of liquid monopropellants' [patent_app_type] => utility [patent_app_number] => 13/115814 [patent_app_country] => US [patent_app_date] => 2011-05-25 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 2 [patent_figures_cnt] => 4 [patent_no_of_words] => 4360 [patent_no_of_claims] => 6 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 61 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13115814 [rel_patent_id] =>[rel_patent_doc_number] =>)
13/115814
Corrosion resistant catalysts for decomposition of liquid monopropellants May 24, 2011 Issued
Array ( [id] => 10104417 [patent_doc_number] => 09140193 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2015-09-22 [patent_title] => 'Gas turbine igniter with structure to reduce radial movement of igniter rod' [patent_app_type] => utility [patent_app_number] => 13/099507 [patent_app_country] => US [patent_app_date] => 2011-05-03 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 4 [patent_figures_cnt] => 10 [patent_no_of_words] => 2317 [patent_no_of_claims] => 10 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 87 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13099507 [rel_patent_id] =>[rel_patent_doc_number] =>)
13/099507
Gas turbine igniter with structure to reduce radial movement of igniter rod May 2, 2011 Issued
Array ( [id] => 9830171 [patent_doc_number] => 08938978 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2015-01-27 [patent_title] => 'Gas turbine engine combustor with lobed, three dimensional contouring' [patent_app_type] => utility [patent_app_number] => 13/099938 [patent_app_country] => US [patent_app_date] => 2011-05-03 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 5 [patent_figures_cnt] => 6 [patent_no_of_words] => 1971 [patent_no_of_claims] => 14 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 94 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13099938 [rel_patent_id] =>[rel_patent_doc_number] =>)
13/099938
Gas turbine engine combustor with lobed, three dimensional contouring May 2, 2011 Issued
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