Search

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 numberTitle of the applicationFiling DateStatus
Array ( [id] => 15948047 [patent_doc_number] => 10661910 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2020-05-26 [patent_title] => Aircraft comprising a turbine engine incorporated into the rear fuselage comprising a system for blocking the fans [patent_app_type] => utility [patent_app_number] => 15/745661 [patent_app_country] => US [patent_app_date] => 2016-07-21 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 2 [patent_figures_cnt] => 4 [patent_no_of_words] => 4328 [patent_no_of_claims] => 28 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 283 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 15745661 [rel_patent_id] =>[rel_patent_doc_number] =>)
15/745661
Aircraft comprising a turbine engine incorporated into the rear fuselage comprising a system for blocking the fans Jul 20, 2016 Issued
Array ( [id] => 13128233 [patent_doc_number] => 10082040 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2018-09-25 [patent_title] => Aircraft comprising a turbine engine incorporated into the rear fuselage with variable supply [patent_app_type] => utility [patent_app_number] => 15/745704 [patent_app_country] => US [patent_app_date] => 2016-07-21 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 4 [patent_figures_cnt] => 10 [patent_no_of_words] => 7154 [patent_no_of_claims] => 17 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 168 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 15745704 [rel_patent_id] =>[rel_patent_doc_number] =>)
15/745704
Aircraft comprising a turbine engine incorporated into the rear fuselage with variable supply Jul 20, 2016 Issued
Array ( [id] => 12139177 [patent_doc_number] => 20180017260 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2018-01-18 [patent_title] => 'COMBUSTOR ANTI-SURGE RETENTION SYSTEM' [patent_app_type] => utility [patent_app_number] => 15/210090 [patent_app_country] => US [patent_app_date] => 2016-07-14 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 4 [patent_figures_cnt] => 4 [patent_no_of_words] => 2960 [patent_no_of_claims] => 15 [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] => 15210090 [rel_patent_id] =>[rel_patent_doc_number] =>)
15/210090
COMBUSTOR ANTI-SURGE RETENTION SYSTEM Jul 13, 2016 Abandoned
Array ( [id] => 12138850 [patent_doc_number] => 20180016933 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2018-01-18 [patent_title] => 'METHOD AND SYSTEM FOR SOAK-BACK MITIGATION BY ACTIVE COOLING' [patent_app_type] => utility [patent_app_number] => 15/207640 [patent_app_country] => US [patent_app_date] => 2016-07-12 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 7 [patent_figures_cnt] => 7 [patent_no_of_words] => 4988 [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] => 15207640 [rel_patent_id] =>[rel_patent_doc_number] =>)
15/207640
METHOD AND SYSTEM FOR SOAK-BACK MITIGATION BY ACTIVE COOLING Jul 11, 2016 Abandoned
Array ( [id] => 12119523 [patent_doc_number] => 20180003109 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2018-01-04 [patent_title] => 'POWER SYSTEM FOR AIRCRAFT PARALLEL HYBRID GAS TURBINE ELECTRIC PROPULSION SYSTEM' [patent_app_type] => utility [patent_app_number] => 15/200240 [patent_app_country] => US [patent_app_date] => 2016-07-01 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 3 [patent_figures_cnt] => 3 [patent_no_of_words] => 3501 [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] => 15200240 [rel_patent_id] =>[rel_patent_doc_number] =>)
15/200240
Power system for aircraft parallel hybrid gas turbine electric propulsion system Jun 30, 2016 Issued
Array ( [id] => 16445488 [patent_doc_number] => 10837406 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2020-11-17 [patent_title] => Flow control system for a rocket engine with parallel fuel passage network [patent_app_type] => utility [patent_app_number] => 15/580070 [patent_app_country] => US [patent_app_date] => 2016-07-01 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 2 [patent_figures_cnt] => 2 [patent_no_of_words] => 3455 [patent_no_of_claims] => 14 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 225 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 15580070 [rel_patent_id] =>[rel_patent_doc_number] =>)
15/580070
Flow control system for a rocket engine with parallel fuel passage network Jun 30, 2016 Issued
Array ( [id] => 12119486 [patent_doc_number] => 20180003072 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2018-01-04 [patent_title] => 'DESCENT OPERATION FOR AN AIRCRAFT PARALLEL HYBRID GAS TURBINE ELECTRIC PROPULSION SYSTEM' [patent_app_type] => utility [patent_app_number] => 15/200149 [patent_app_country] => US [patent_app_date] => 2016-07-01 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 2 [patent_figures_cnt] => 2 [patent_no_of_words] => 3787 [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] =>[firstpage_image] =>[orig_patent_app_number] => 15200149 [rel_patent_id] =>[rel_patent_doc_number] =>)
15/200149
Descent operation for an aircraft parallel hybrid gas turbine electric propulsion system Jun 30, 2016 Issued
Array ( [id] => 12119485 [patent_doc_number] => 20180003071 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2018-01-04 [patent_title] => 'HIGH EFFICIENCY AIRCRAFT PARALLEL HYBRID GAS TURBINE ELECTRIC PROPULSION SYSTEM' [patent_app_type] => utility [patent_app_number] => 15/200128 [patent_app_country] => US [patent_app_date] => 2016-07-01 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 3 [patent_figures_cnt] => 3 [patent_no_of_words] => 3235 [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] => 15200128 [rel_patent_id] =>[rel_patent_doc_number] =>)
15/200128
HIGH EFFICIENCY AIRCRAFT PARALLEL HYBRID GAS TURBINE ELECTRIC PROPULSION SYSTEM Jun 30, 2016 Issued
Array ( [id] => 12982060 [patent_doc_number] => 20170342943 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2017-11-30 [patent_title] => METHODS, SYSTEMS AND APPARATUSES FOR COMBUSTIBLE LEAD FOR HIGH TRIPLE POINT PROPELLANTS [patent_app_type] => utility [patent_app_number] => 15/166558 [patent_app_country] => US [patent_app_date] => 2016-05-27 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 0 [patent_figures_cnt] => 0 [patent_no_of_words] => 6385 [patent_no_of_claims] => 0 [patent_no_of_ind_claims] => -18 [patent_words_short_claim] => 75 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 15166558 [rel_patent_id] =>[rel_patent_doc_number] =>)
15/166558
Methods, systems and apparatuses for combustible lead for high triple point propellants May 26, 2016 Issued
Array ( [id] => 12662386 [patent_doc_number] => 20180112628 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2018-04-26 [patent_title] => Rocket Engine Ignition System [patent_app_type] => utility [patent_app_number] => 15/572440 [patent_app_country] => US [patent_app_date] => 2016-05-09 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 0 [patent_figures_cnt] => 0 [patent_no_of_words] => 5246 [patent_no_of_claims] => 0 [patent_no_of_ind_claims] => -11 [patent_words_short_claim] => 90 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 15572440 [rel_patent_id] =>[rel_patent_doc_number] =>)
15/572440
Rocket Engine Ignition System May 8, 2016 Abandoned
Array ( [id] => 13494607 [patent_doc_number] => 20180298846 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2018-10-18 [patent_title] => Liquid Propellant Chemical Rocket Engine Reactor Thermal Management System [patent_app_type] => utility [patent_app_number] => 15/566362 [patent_app_country] => US [patent_app_date] => 2016-04-14 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 0 [patent_figures_cnt] => 0 [patent_no_of_words] => 4525 [patent_no_of_claims] => 0 [patent_no_of_ind_claims] => -14 [patent_words_short_claim] => 122 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 15566362 [rel_patent_id] =>[rel_patent_doc_number] =>)
15/566362
Liquid Propellant Chemical Rocket Engine Reactor Thermal Management System Apr 13, 2016 Abandoned
Array ( [id] => 11980185 [patent_doc_number] => 20170284339 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2017-10-05 [patent_title] => 'THRUSTER WITH SEGMENTED PROPELLANT' [patent_app_type] => utility [patent_app_number] => 15/091245 [patent_app_country] => US [patent_app_date] => 2016-04-05 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 4 [patent_figures_cnt] => 4 [patent_no_of_words] => 5829 [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] => 15091245 [rel_patent_id] =>[rel_patent_doc_number] =>)
15/091245
THRUSTER WITH SEGMENTED PROPELLANT Apr 4, 2016 Abandoned
Array ( [id] => 14666409 [patent_doc_number] => 10371099 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2019-08-06 [patent_title] => Spark plug and associated propellant ignition system [patent_app_type] => utility [patent_app_number] => 15/091192 [patent_app_country] => US [patent_app_date] => 2016-04-05 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 3 [patent_figures_cnt] => 5 [patent_no_of_words] => 3339 [patent_no_of_claims] => 20 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 154 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 15091192 [rel_patent_id] =>[rel_patent_doc_number] =>)
15/091192
Spark plug and associated propellant ignition system Apr 4, 2016 Issued
Array ( [id] => 15851883 [patent_doc_number] => 10641212 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2020-05-05 [patent_title] => Rocket thruster nozzle with connectors and brace [patent_app_type] => utility [patent_app_number] => 15/554344 [patent_app_country] => US [patent_app_date] => 2016-03-11 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 1 [patent_figures_cnt] => 5 [patent_no_of_words] => 1947 [patent_no_of_claims] => 14 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 133 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 15554344 [rel_patent_id] =>[rel_patent_doc_number] =>)
15/554344
Rocket thruster nozzle with connectors and brace Mar 10, 2016 Issued
Array ( [id] => 16337051 [patent_doc_number] => 10787998 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2020-09-29 [patent_title] => Cooling mechanism of combustion chamber, rocket engine having cooling mechanism, and method of manufacturing cooling mechanism [patent_app_type] => utility [patent_app_number] => 15/556461 [patent_app_country] => US [patent_app_date] => 2016-03-09 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 24 [patent_figures_cnt] => 35 [patent_no_of_words] => 14256 [patent_no_of_claims] => 18 [patent_no_of_ind_claims] => 5 [patent_words_short_claim] => 320 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 15556461 [rel_patent_id] =>[rel_patent_doc_number] =>)
15/556461
Cooling mechanism of combustion chamber, rocket engine having cooling mechanism, and method of manufacturing cooling mechanism Mar 8, 2016 Issued
Array ( [id] => 12240602 [patent_doc_number] => 20180073465 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2018-03-15 [patent_title] => 'PROPELLANT INJECTOR ALLOWING PROPELLANT TO BE DISCHARGED WHILE ENSURING UNIFORM INJECTION' [patent_app_type] => utility [patent_app_number] => 15/554464 [patent_app_country] => US [patent_app_date] => 2016-03-02 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 4 [patent_figures_cnt] => 4 [patent_no_of_words] => 2414 [patent_no_of_claims] => 8 [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] => 15554464 [rel_patent_id] =>[rel_patent_doc_number] =>)
15/554464
Propellant injector allowing propellant to be discharged while ensuring uniform injection Mar 1, 2016 Issued
Array ( [id] => 12152249 [patent_doc_number] => 20180023513 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2018-01-25 [patent_title] => 'ROCKET ENGINE AND IGNITION SYSTEM' [patent_app_type] => utility [patent_app_number] => 15/547995 [patent_app_country] => US [patent_app_date] => 2016-02-19 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 11 [patent_figures_cnt] => 11 [patent_no_of_words] => 7793 [patent_no_of_claims] => 11 [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] => 15547995 [rel_patent_id] =>[rel_patent_doc_number] =>)
15/547995
ROCKET ENGINE AND IGNITION SYSTEM Feb 18, 2016 Abandoned
Array ( [id] => 12220018 [patent_doc_number] => 20180058378 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2018-03-01 [patent_title] => 'PRESSURIZATION DEVICE FOR A LIQUID-OXYGEN TANK OF A ROCKET ENGINE' [patent_app_type] => utility [patent_app_number] => 15/550208 [patent_app_country] => US [patent_app_date] => 2016-02-09 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 3 [patent_figures_cnt] => 3 [patent_no_of_words] => 3540 [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] => 15550208 [rel_patent_id] =>[rel_patent_doc_number] =>)
15/550208
PRESSURIZATION DEVICE FOR A LIQUID-OXYGEN TANK OF A ROCKET ENGINE Feb 8, 2016 Abandoned
Array ( [id] => 11729974 [patent_doc_number] => 20170191417 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2017-07-06 [patent_title] => 'ENGINE COMPONENT ASSEMBLY' [patent_app_type] => utility [patent_app_number] => 14/989290 [patent_app_country] => US [patent_app_date] => 2016-01-06 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 9 [patent_figures_cnt] => 9 [patent_no_of_words] => 4675 [patent_no_of_claims] => 57 [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] => 14989290 [rel_patent_id] =>[rel_patent_doc_number] =>)
14/989290
ENGINE COMPONENT ASSEMBLY Jan 5, 2016 Abandoned
Array ( [id] => 16415180 [patent_doc_number] => 10823060 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2020-11-03 [patent_title] => Gas turbine engine with short inlet, acoustic treatment and anti-icing features [patent_app_type] => utility [patent_app_number] => 14/974169 [patent_app_country] => US [patent_app_date] => 2015-12-18 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 3 [patent_figures_cnt] => 6 [patent_no_of_words] => 3541 [patent_no_of_claims] => 5 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 307 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14974169 [rel_patent_id] =>[rel_patent_doc_number] =>)
14/974169
Gas turbine engine with short inlet, acoustic treatment and anti-icing features Dec 17, 2015 Issued
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