
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] => 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 |