
Frederick C. Nicolas
Examiner (ID: 17365, Phone: (571)272-4931 , Office: P/3754 )
| Most Active Art Unit | 3754 |
| Art Unit(s) | 3754 |
| Total Applications | 2465 |
| Issued Applications | 1847 |
| Pending Applications | 211 |
| Abandoned Applications | 435 |
Applications
| Application number | Title of the application | Filing Date | Status |
|---|---|---|---|
Array
(
[id] => 10367720
[patent_doc_number] => 20150252724
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[patent_kind] => A1
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[patent_title] => 'SYSTEM AND METHOD FOR HIGH EFFICIENCY POWER GENERATION USING A CARBON DIOXIDE CIRCULATING WORKING FLUID'
[patent_app_type] => utility
[patent_app_number] => 14/717134
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Array
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[patent_issue_date] => 2016-02-04
[patent_title] => 'Magnetic Gas Engine and Method of Extracting Work'
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Array
(
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[patent_title] => 'DEVICE AND METHOD FOR STARTING AN AUXILIARY POWER UNIT'
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Array
(
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[patent_title] => 'Method and apparatus for isolating inactive fuel passages'
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Array
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[patent_title] => Hybrid air blast fuel nozzle
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[patent_title] => 'Igniter position for a combustor of a gas turbine engine'
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[patent_title] => 'TURBINE ENGINE WITH A COMBUSTION CHAMBER OUTER FLANGE OF SANDWICH TYPE'
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[rel_patent_id] =>[rel_patent_doc_number] =>) 14/629840 | Turbine engine with a combustion chamber outer flange of sandwich type | Feb 23, 2015 | Issued |
Array
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[patent_title] => Methods of forming flexible structures for a rocket motor assembly, related flexible structures, and related assemblies including the flexible structures
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[patent_app_number] => 14/629297
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Array
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[patent_title] => Geared axial multistage expander device, system and method
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Array
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[patent_title] => 'THERMALLY EXPANDABLE TRANSITION PIECE'
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Array
(
[id] => 17976130
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[patent_title] => Fuel control device, combustor, gas turbine, control method, and program
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Array
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[patent_title] => 'Method and apparatus for controlling gas turbine combustor'
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Array
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[rel_patent_id] =>[rel_patent_doc_number] =>) 14/618801 | Aircraft system with fuel-to-fuel heat exchanger | Feb 9, 2015 | Issued |
Array
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[patent_title] => 'Cooling passages for a mid-turbine frame'
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[patent_title] => Fuel injector including tandem vanes for injecting alternate fuels in a gas turbine
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[rel_patent_id] =>[rel_patent_doc_number] =>) 14/597510 | Gas turbine engine with distributed fans | Jan 14, 2015 | Issued |