
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] => 15948047
[patent_doc_number] => 10661910
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[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
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Array
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[patent_issue_date] => 2018-09-25
[patent_title] => Aircraft comprising a turbine engine incorporated into the rear fuselage with variable supply
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Array
(
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[patent_title] => 'COMBUSTOR ANTI-SURGE RETENTION SYSTEM'
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Array
(
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[patent_title] => 'METHOD AND SYSTEM FOR SOAK-BACK MITIGATION BY ACTIVE COOLING'
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Array
(
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[patent_title] => 'POWER SYSTEM FOR AIRCRAFT PARALLEL HYBRID GAS TURBINE ELECTRIC PROPULSION SYSTEM'
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Array
(
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[patent_title] => Flow control system for a rocket engine with parallel fuel passage network
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Array
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Array
(
[id] => 12119485
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Array
(
[id] => 12982060
[patent_doc_number] => 20170342943
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[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
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[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
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[patent_issue_date] => 2018-04-26
[patent_title] => Rocket Engine Ignition System
[patent_app_type] => utility
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Array
(
[id] => 13494607
[patent_doc_number] => 20180298846
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[patent_title] => Liquid Propellant Chemical Rocket Engine Reactor Thermal Management System
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Array
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[id] => 11980185
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Array
(
[id] => 14666409
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Array
(
[id] => 15851883
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[patent_title] => Rocket thruster nozzle with connectors and brace
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Array
(
[id] => 16337051
[patent_doc_number] => 10787998
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[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
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Array
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[patent_issue_date] => 2018-03-15
[patent_title] => 'PROPELLANT INJECTOR ALLOWING PROPELLANT TO BE DISCHARGED WHILE ENSURING UNIFORM INJECTION'
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[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
(
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Array
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[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 |