
Cary Michael Robinson
Examiner (ID: 2649, Phone: (571)270-3316 , Office: P/2923 )
| Most Active Art Unit | 2923 |
| Art Unit(s) | 2954, 2923 |
| Total Applications | 1373 |
| Issued Applications | 1343 |
| Pending Applications | 5 |
| Abandoned Applications | 23 |
Applications
| Application number | Title of the application | Filing Date | Status |
|---|---|---|---|
Array
(
[id] => 15103507
[patent_doc_number] => 10473060
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2019-11-12
[patent_title] => Method and system for a gas turbine engine air ventilation purge circuit
[patent_app_type] => utility
[patent_app_number] => 14/966513
[patent_app_country] => US
[patent_app_date] => 2015-12-11
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
[patent_figures_cnt] => 10
[patent_no_of_words] => 5564
[patent_no_of_claims] => 20
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 250
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14966513
[rel_patent_id] =>[rel_patent_doc_number] =>) 14/966513 | Method and system for a gas turbine engine air ventilation purge circuit | Dec 10, 2015 | Issued |
Array
(
[id] => 11691723
[patent_doc_number] => 20170167438
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2017-06-15
[patent_title] => 'Gas Turbine Engine'
[patent_app_type] => utility
[patent_app_number] => 14/966007
[patent_app_country] => US
[patent_app_date] => 2015-12-11
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 3
[patent_no_of_words] => 4119
[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] => 14966007
[rel_patent_id] =>[rel_patent_doc_number] =>) 14/966007 | Gas Turbine Engine | Dec 10, 2015 | Abandoned |
Array
(
[id] => 15884065
[patent_doc_number] => 10648365
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2020-05-12
[patent_title] => Gas turbine engine bearing sump and lubricant drain line from cooling passage
[patent_app_type] => utility
[patent_app_number] => 14/962217
[patent_app_country] => US
[patent_app_date] => 2015-12-08
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 4
[patent_no_of_words] => 4864
[patent_no_of_claims] => 16
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 184
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14962217
[rel_patent_id] =>[rel_patent_doc_number] =>) 14/962217 | Gas turbine engine bearing sump and lubricant drain line from cooling passage | Dec 7, 2015 | Issued |
Array
(
[id] => 11670842
[patent_doc_number] => 20170159563
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2017-06-08
[patent_title] => 'METHOD AND SYSTEM FOR PRE-COOLER EXHAUST ENERGY RECOVERY'
[patent_app_type] => utility
[patent_app_number] => 14/961057
[patent_app_country] => US
[patent_app_date] => 2015-12-07
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
[patent_figures_cnt] => 5
[patent_no_of_words] => 3460
[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] =>[firstpage_image] =>[orig_patent_app_number] => 14961057
[rel_patent_id] =>[rel_patent_doc_number] =>) 14/961057 | METHOD AND SYSTEM FOR PRE-COOLER EXHAUST ENERGY RECOVERY | Dec 6, 2015 | Abandoned |
Array
(
[id] => 11956778
[patent_doc_number] => 20170260929
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2017-09-14
[patent_title] => 'DEVICE AND LOCKING OF A FUELING DEVICE'
[patent_app_type] => utility
[patent_app_number] => 15/529836
[patent_app_country] => US
[patent_app_date] => 2015-11-23
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 6
[patent_figures_cnt] => 6
[patent_no_of_words] => 2623
[patent_no_of_claims] => 8
[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] => 15529836
[rel_patent_id] =>[rel_patent_doc_number] =>) 15/529836 | Device and locking of a fueling device | Nov 22, 2015 | Issued |
Array
(
[id] => 10814599
[patent_doc_number] => 20160160758
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2016-06-09
[patent_title] => 'GAS TURBINE ENGINE NACELLE ANTI-ICING SYSTEM'
[patent_app_type] => utility
[patent_app_number] => 14/947174
[patent_app_country] => US
[patent_app_date] => 2015-11-20
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
[patent_figures_cnt] => 5
[patent_no_of_words] => 3084
[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] => 14947174
[rel_patent_id] =>[rel_patent_doc_number] =>) 14/947174 | GAS TURBINE ENGINE NACELLE ANTI-ICING SYSTEM | Nov 19, 2015 | Abandoned |
Array
(
[id] => 10800309
[patent_doc_number] => 20160146466
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2016-05-26
[patent_title] => 'LOBE LANCE FOR A GAS TURBINE COMBUSTOR'
[patent_app_type] => utility
[patent_app_number] => 14/947386
[patent_app_country] => US
[patent_app_date] => 2015-11-20
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 3
[patent_no_of_words] => 3657
[patent_no_of_claims] => 14
[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] => 14947386
[rel_patent_id] =>[rel_patent_doc_number] =>) 14/947386 | Lobe lance for a gas turbine combustor | Nov 19, 2015 | Issued |
Array
(
[id] => 10792368
[patent_doc_number] => 20160138524
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2016-05-19
[patent_title] => 'Monopropellant Driven Hydraulic Pressure Supply'
[patent_app_type] => utility
[patent_app_number] => 14/942780
[patent_app_country] => US
[patent_app_date] => 2015-11-16
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
[patent_figures_cnt] => 5
[patent_no_of_words] => 2109
[patent_no_of_claims] => 16
[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] => 14942780
[rel_patent_id] =>[rel_patent_doc_number] =>) 14/942780 | Monopropellant driven hydraulic pressure supply | Nov 15, 2015 | Issued |
Array
(
[id] => 11628122
[patent_doc_number] => 20170138310
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2017-05-18
[patent_title] => 'AEROSPIKE ROCKET MOTOR ASSEMBLY'
[patent_app_type] => utility
[patent_app_number] => 14/938952
[patent_app_country] => US
[patent_app_date] => 2015-11-12
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 7
[patent_figures_cnt] => 7
[patent_no_of_words] => 3905
[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] => 14938952
[rel_patent_id] =>[rel_patent_doc_number] =>) 14/938952 | Aerospike rocket motor assembly | Nov 11, 2015 | Issued |
Array
(
[id] => 11620400
[patent_doc_number] => 20170130587
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2017-05-11
[patent_title] => 'LAST STAGE AIRFOIL DESIGN FOR OPTIMAL DIFFUSER PERFORMANCE'
[patent_app_type] => utility
[patent_app_number] => 14/936253
[patent_app_country] => US
[patent_app_date] => 2015-11-09
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 10
[patent_figures_cnt] => 10
[patent_no_of_words] => 5869
[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] => 14936253
[rel_patent_id] =>[rel_patent_doc_number] =>) 14/936253 | LAST STAGE AIRFOIL DESIGN FOR OPTIMAL DIFFUSER PERFORMANCE | Nov 8, 2015 | Abandoned |
Array
(
[id] => 11604957
[patent_doc_number] => 20170122259
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2017-05-04
[patent_title] => 'SOLID ROCKET MOTORS INCLUDING FLIGHT TERMINATION SYSTEMS, AND RELATED MULTI-STAGE SOLID ROCKET MOTOR ASSEMBLIES AND METHODS'
[patent_app_type] => utility
[patent_app_number] => 14/932895
[patent_app_country] => US
[patent_app_date] => 2015-11-04
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 6
[patent_figures_cnt] => 6
[patent_no_of_words] => 12823
[patent_no_of_claims] => 28
[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] => 14932895
[rel_patent_id] =>[rel_patent_doc_number] =>) 14/932895 | Solid rocket motors including flight termination systems, and related multi-stage solid rocket motor assemblies and methods | Nov 3, 2015 | Issued |
Array
(
[id] => 10701162
[patent_doc_number] => 20160047310
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2016-02-18
[patent_title] => 'HEAT STORAGE MECHANISM OF HEAT EXCHANGER'
[patent_app_type] => utility
[patent_app_number] => 14/926721
[patent_app_country] => US
[patent_app_date] => 2015-10-29
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
[patent_figures_cnt] => 5
[patent_no_of_words] => 3490
[patent_no_of_claims] => 6
[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] => 14926721
[rel_patent_id] =>[rel_patent_doc_number] =>) 14/926721 | Heat storage mechanism of heat exchanger | Oct 28, 2015 | Issued |
Array
(
[id] => 10769645
[patent_doc_number] => 20160115801
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2016-04-28
[patent_title] => 'MULTI-PIECE TURBINE AIRFOIL'
[patent_app_type] => utility
[patent_app_number] => 14/887847
[patent_app_country] => US
[patent_app_date] => 2015-10-20
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 4
[patent_no_of_words] => 4793
[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] => 14887847
[rel_patent_id] =>[rel_patent_doc_number] =>) 14/887847 | Multi-piece turbine airfoil | Oct 19, 2015 | Issued |
Array
(
[id] => 10762978
[patent_doc_number] => 20160109133
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2016-04-21
[patent_title] => 'GAS TURBINE ENGINE FUEL SYSTEM'
[patent_app_type] => utility
[patent_app_number] => 14/876352
[patent_app_country] => US
[patent_app_date] => 2015-10-06
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 6
[patent_figures_cnt] => 6
[patent_no_of_words] => 8523
[patent_no_of_claims] => 16
[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] => 14876352
[rel_patent_id] =>[rel_patent_doc_number] =>) 14/876352 | GAS TURBINE ENGINE FUEL SYSTEM | Oct 5, 2015 | Abandoned |
Array
(
[id] => 11543143
[patent_doc_number] => 20170096968
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2017-04-06
[patent_title] => 'SOLID PROPELLANT GRAIN'
[patent_app_type] => utility
[patent_app_number] => 14/873522
[patent_app_country] => US
[patent_app_date] => 2015-10-02
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 4
[patent_no_of_words] => 1980
[patent_no_of_claims] => 17
[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] => 14873522
[rel_patent_id] =>[rel_patent_doc_number] =>) 14/873522 | Solid propellant grain | Oct 1, 2015 | Issued |
Array
(
[id] => 15575369
[patent_doc_number] => 10578056
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2020-03-03
[patent_title] => Spacecraft nozzle comprising an improved deployment system
[patent_app_type] => utility
[patent_app_number] => 15/516829
[patent_app_country] => US
[patent_app_date] => 2015-10-02
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 6
[patent_no_of_words] => 3654
[patent_no_of_claims] => 6
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 430
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 15516829
[rel_patent_id] =>[rel_patent_doc_number] =>) 15/516829 | Spacecraft nozzle comprising an improved deployment system | Oct 1, 2015 | Issued |
Array
(
[id] => 10751174
[patent_doc_number] => 20160097325
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2016-04-07
[patent_title] => 'COOLED COMPONENT'
[patent_app_type] => utility
[patent_app_number] => 14/858535
[patent_app_country] => US
[patent_app_date] => 2015-09-18
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 8
[patent_figures_cnt] => 8
[patent_no_of_words] => 8170
[patent_no_of_claims] => 22
[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] => 14858535
[rel_patent_id] =>[rel_patent_doc_number] =>) 14/858535 | Cooled component | Sep 17, 2015 | Issued |
Array
(
[id] => 11004968
[patent_doc_number] => 20160201918
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2016-07-14
[patent_title] => 'SMALL ARRAYED SWIRLER SYSTEM FOR REDUCED EMISSIONS AND NOISE'
[patent_app_type] => utility
[patent_app_number] => 14/857439
[patent_app_country] => US
[patent_app_date] => 2015-09-17
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
[patent_figures_cnt] => 5
[patent_no_of_words] => 4106
[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] => 14857439
[rel_patent_id] =>[rel_patent_doc_number] =>) 14/857439 | SMALL ARRAYED SWIRLER SYSTEM FOR REDUCED EMISSIONS AND NOISE | Sep 16, 2015 | Abandoned |
Array
(
[id] => 14247255
[patent_doc_number] => 10273821
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2019-04-30
[patent_title] => Advanced stationary sealing cooled cross-section for axial retention of ceramic matrix composite shrouds
[patent_app_type] => utility
[patent_app_number] => 14/850383
[patent_app_country] => US
[patent_app_date] => 2015-09-10
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 8
[patent_no_of_words] => 5513
[patent_no_of_claims] => 15
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 207
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14850383
[rel_patent_id] =>[rel_patent_doc_number] =>) 14/850383 | Advanced stationary sealing cooled cross-section for axial retention of ceramic matrix composite shrouds | Sep 9, 2015 | Issued |
Array
(
[id] => 13344461
[patent_doc_number] => 20180223770
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2018-08-09
[patent_title] => ROCKET MOTOR WITH ENERGETIC GRAIN HAVING MICRO-VOIDS
[patent_app_type] => utility
[patent_app_number] => 15/506480
[patent_app_country] => US
[patent_app_date] => 2015-09-10
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 0
[patent_figures_cnt] => 0
[patent_no_of_words] => 4854
[patent_no_of_claims] => 0
[patent_no_of_ind_claims] => -17
[patent_words_short_claim] => 85
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 15506480
[rel_patent_id] =>[rel_patent_doc_number] =>) 15/506480 | ROCKET MOTOR WITH ENERGETIC GRAIN HAVING MICRO-VOIDS | Sep 9, 2015 | Abandoned |