
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] => 11472376
[patent_doc_number] => 20170059159
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2017-03-02
[patent_title] => 'CMC COMBUSTOR SHELL WITH INTEGRAL CHUTES'
[patent_app_type] => utility
[patent_app_number] => 14/834605
[patent_app_country] => US
[patent_app_date] => 2015-08-25
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Array
(
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[patent_doc_number] => 20170051680
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2017-02-23
[patent_title] => 'AIRFLOW INJECTION NOZZLE FOR A GAS TURBINE ENGINE'
[patent_app_type] => utility
[patent_app_number] => 14/828544
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[patent_app_date] => 2015-08-18
[patent_effective_date] => 0000-00-00
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Array
(
[id] => 11457764
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[patent_kind] => A1
[patent_issue_date] => 2017-02-23
[patent_title] => 'POWER SYSTEM AND METHODS OF ASSEMBLING THE SAME'
[patent_app_type] => utility
[patent_app_number] => 14/829411
[patent_app_country] => US
[patent_app_date] => 2015-08-18
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[patent_drawing_sheets_cnt] => 6
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Array
(
[id] => 11396085
[patent_doc_number] => 20170016620
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2017-01-19
[patent_title] => 'COMBUSTOR ASSEMBLY FOR USE IN A GAS TURBINE ENGINE AND METHOD OF ASSEMBLING'
[patent_app_type] => utility
[patent_app_number] => 14/801962
[patent_app_country] => US
[patent_app_date] => 2015-07-17
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
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[rel_patent_id] =>[rel_patent_doc_number] =>) 14/801962 | Combustor assembly for use in a gas turbine engine and method of assembling | Jul 16, 2015 | Issued |
Array
(
[id] => 12159661
[patent_doc_number] => 20180030927
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2018-02-01
[patent_title] => 'PROPELLANT GRAIN FOR A SOLID ROCKET MOTOR'
[patent_app_type] => utility
[patent_app_number] => 15/550690
[patent_app_country] => US
[patent_app_date] => 2015-07-03
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 7
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Array
(
[id] => 10678869
[patent_doc_number] => 20160025014
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2016-01-28
[patent_title] => 'HIGH TEMPERATURE DISK CONDITIONING SYSTEM'
[patent_app_type] => utility
[patent_app_number] => 14/754325
[patent_app_country] => US
[patent_app_date] => 2015-06-29
[patent_effective_date] => 0000-00-00
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[rel_patent_id] =>[rel_patent_doc_number] =>) 14/754325 | High temperature disk conditioning system | Jun 28, 2015 | Issued |
Array
(
[id] => 10492468
[patent_doc_number] => 20150377489
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2015-12-31
[patent_title] => 'INJECTION SYSTEM FOR A TURBINE ENGINE COMBUSTION CHAMBER CONFIGURED FOR DIRECT INJECTION OF TWO COAXIAL FUEL FLOWS'
[patent_app_type] => utility
[patent_app_number] => 14/750347
[patent_app_country] => US
[patent_app_date] => 2015-06-25
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 8
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[rel_patent_id] =>[rel_patent_doc_number] =>) 14/750347 | Injection system for a turbine engine combustion chamber configured for direct injection of two coaxial fuel flows | Jun 24, 2015 | Issued |
Array
(
[id] => 13155125
[patent_doc_number] => 10094277
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2018-10-09
[patent_title] => Gas turbine engine configured for modular assembly/disassembly and method for same
[patent_app_type] => utility
[patent_app_number] => 14/745158
[patent_app_country] => US
[patent_app_date] => 2015-06-19
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[rel_patent_id] =>[rel_patent_doc_number] =>) 14/745158 | Gas turbine engine configured for modular assembly/disassembly and method for same | Jun 18, 2015 | Issued |
Array
(
[id] => 10484106
[patent_doc_number] => 20150369125
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[patent_kind] => A1
[patent_issue_date] => 2015-12-24
[patent_title] => 'METHOD FOR INCREASING THE POWER OF A COMBINED-CYCLE POWER PLANT, AND COMBINED-CYCLE POWER PLANT FOR CONDUCTING SAID METHOD'
[patent_app_type] => utility
[patent_app_number] => 14/741893
[patent_app_country] => US
[patent_app_date] => 2015-06-17
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[rel_patent_id] =>[rel_patent_doc_number] =>) 14/741893 | METHOD FOR INCREASING THE POWER OF A COMBINED-CYCLE POWER PLANT, AND COMBINED-CYCLE POWER PLANT FOR CONDUCTING SAID METHOD | Jun 16, 2015 | Abandoned |
Array
(
[id] => 11291217
[patent_doc_number] => 20160341150
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2016-11-24
[patent_title] => 'Thrust Reverser System and Method with Flow Separation-Inhibiting Blades'
[patent_app_type] => utility
[patent_app_number] => 14/718241
[patent_app_country] => US
[patent_app_date] => 2015-05-21
[patent_effective_date] => 0000-00-00
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[rel_patent_id] =>[rel_patent_doc_number] =>) 14/718241 | Thrust Reverser System and Method with Flow Separation-Inhibiting Blades | May 20, 2015 | Abandoned |
Array
(
[id] => 11291497
[patent_doc_number] => 20160341429
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2016-11-24
[patent_title] => 'GAS TURBINE ENGINE LIQUID FUEL SUPPLY SYSTEM AND METHOD'
[patent_app_type] => utility
[patent_app_number] => 14/717570
[patent_app_country] => US
[patent_app_date] => 2015-05-20
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Array
(
[id] => 13676323
[patent_doc_number] => 20160376895
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[patent_issue_date] => 2016-12-29
[patent_title] => GAS TURBINE ENGINE COMPONENT PLATFORM COOLING
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[rel_patent_id] =>[rel_patent_doc_number] =>) 14/713186 | Gas turbine engine component platform cooling | May 14, 2015 | Issued |
Array
(
[id] => 10655744
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[patent_title] => 'HYDRAULICALLY ACTUATED MECHANICAL LOCK ASSEMBLY'
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[rel_patent_id] =>[rel_patent_doc_number] =>) 14/707518 | Hydraulically actuated mechanical lock assembly | May 7, 2015 | Issued |
Array
(
[id] => 17498189
[patent_doc_number] => 11286887
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[patent_kind] => B2
[patent_issue_date] => 2022-03-29
[patent_title] => Pneumatic circuit breaker based self resetting passive overspeed control valve for turbine pump assembly
[patent_app_type] => utility
[patent_app_number] => 14/695082
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[rel_patent_id] =>[rel_patent_doc_number] =>) 14/695082 | Pneumatic circuit breaker based self resetting passive overspeed control valve for turbine pump assembly | Apr 23, 2015 | Issued |
Array
(
[id] => 12010553
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[patent_title] => 'Premix pilot nozzle'
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[rel_patent_id] =>[rel_patent_doc_number] =>) 14/691864 | Premix pilot nozzle | Apr 20, 2015 | Issued |
Array
(
[id] => 11108316
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[patent_title] => 'SHROUD ASSEMBLY AND SHROUD FOR GAS TURBINE ENGINE'
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Array
(
[id] => 12511464
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[patent_title] => Fuel nozzle with dual-staged main circuit
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Array
(
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Array
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Array
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