
Marc J. Amar
Examiner (ID: 17142, Phone: (571)272-9948 , Office: P/3741 )
| Most Active Art Unit | 3741 |
| Art Unit(s) | 3741 |
| Total Applications | 488 |
| Issued Applications | 346 |
| Pending Applications | 52 |
| Abandoned Applications | 95 |
Applications
| Application number | Title of the application | Filing Date | Status |
|---|---|---|---|
Array
(
[id] => 11244384
[patent_doc_number] => 09470422
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2016-10-18
[patent_title] => 'Gas turbine structural mounting arrangement between combustion gas duct annular chamber and turbine vane carrier'
[patent_app_type] => utility
[patent_app_number] => 14/059521
[patent_app_country] => US
[patent_app_date] => 2013-10-22
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 7
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[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14059521
[rel_patent_id] =>[rel_patent_doc_number] =>) 14/059521 | Gas turbine structural mounting arrangement between combustion gas duct annular chamber and turbine vane carrier | Oct 21, 2013 | Issued |
Array
(
[id] => 13252267
[patent_doc_number] => 10138817
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2018-11-27
[patent_title] => Gas turbine engine geared compressor with first and second input rotors
[patent_app_type] => utility
[patent_app_number] => 14/060094
[patent_app_country] => US
[patent_app_date] => 2013-10-22
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
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[rel_patent_id] =>[rel_patent_doc_number] =>) 14/060094 | Gas turbine engine geared compressor with first and second input rotors | Oct 21, 2013 | Issued |
Array
(
[id] => 10216355
[patent_doc_number] => 20150101347
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2015-04-16
[patent_title] => 'LOCKING SPACER ASSEMBLY'
[patent_app_type] => utility
[patent_app_number] => 14/055091
[patent_app_country] => US
[patent_app_date] => 2013-10-16
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 10
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[rel_patent_id] =>[rel_patent_doc_number] =>) 14/055091 | Locking spacer assembly inserted between rotor blades | Oct 15, 2013 | Issued |
Array
(
[id] => 11319732
[patent_doc_number] => 09518471
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2016-12-13
[patent_title] => 'Locking spacer assembly'
[patent_app_type] => utility
[patent_app_number] => 14/055106
[patent_app_country] => US
[patent_app_date] => 2013-10-16
[patent_effective_date] => 0000-00-00
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[rel_patent_id] =>[rel_patent_doc_number] =>) 14/055106 | Locking spacer assembly | Oct 15, 2013 | Issued |
Array
(
[id] => 10116628
[patent_doc_number] => 09151502
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2015-10-06
[patent_title] => 'System and method for reducing modal coupling of combustion dynamics'
[patent_app_type] => utility
[patent_app_number] => 14/048272
[patent_app_country] => US
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[rel_patent_id] =>[rel_patent_doc_number] =>) 14/048272 | System and method for reducing modal coupling of combustion dynamics | Oct 7, 2013 | Issued |
Array
(
[id] => 10529582
[patent_doc_number] => 09255711
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2016-02-09
[patent_title] => 'System for reducing combustion dynamics by varying fuel flow axial distances'
[patent_app_type] => utility
[patent_app_number] => 14/048252
[patent_app_country] => US
[patent_app_date] => 2013-10-08
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[rel_patent_id] =>[rel_patent_doc_number] =>) 14/048252 | System for reducing combustion dynamics by varying fuel flow axial distances | Oct 7, 2013 | Issued |
Array
(
[id] => 10299858
[patent_doc_number] => 20150184858
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2015-07-02
[patent_title] => 'METHOD OF OPERATING A MULTI-STAGE FLAMESHEET COMBUSTOR'
[patent_app_type] => utility
[patent_app_number] => 14/038070
[patent_app_country] => US
[patent_app_date] => 2013-09-26
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[rel_patent_id] =>[rel_patent_doc_number] =>) 14/038070 | METHOD OF OPERATING A MULTI-STAGE FLAMESHEET COMBUSTOR | Sep 25, 2013 | Abandoned |
Array
(
[id] => 10197813
[patent_doc_number] => 20150082799
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2015-03-26
[patent_title] => 'High Efficiency Hydrogen Turbine'
[patent_app_type] => utility
[patent_app_number] => 14/034551
[patent_app_country] => US
[patent_app_date] => 2013-09-24
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 2
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[patent_no_of_words] => 534
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[rel_patent_id] =>[rel_patent_doc_number] =>) 14/034551 | High Efficiency Hydrogen Turbine | Sep 23, 2013 | Abandoned |
Array
(
[id] => 10097725
[patent_doc_number] => 09134029
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2015-09-15
[patent_title] => 'Radial midframe baffle for can-annular combustor arrangement having tangentially oriented combustor cans'
[patent_app_type] => utility
[patent_app_number] => 14/024892
[patent_app_country] => US
[patent_app_date] => 2013-09-12
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[rel_patent_id] =>[rel_patent_doc_number] =>) 14/024892 | Radial midframe baffle for can-annular combustor arrangement having tangentially oriented combustor cans | Sep 11, 2013 | Issued |
Array
(
[id] => 9904152
[patent_doc_number] => 20150059352
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2015-03-05
[patent_title] => 'DUAL FUEL COMBUSTOR FOR A GAS TURBINE ENGINE'
[patent_app_type] => utility
[patent_app_number] => 14/017509
[patent_app_country] => US
[patent_app_date] => 2013-09-04
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
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[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14017509
[rel_patent_id] =>[rel_patent_doc_number] =>) 14/017509 | Dual fuel combustor for a gas turbine engine including a toroidal injection manifold with inner and outer sleeves | Sep 3, 2013 | Issued |
Array
(
[id] => 11881345
[patent_doc_number] => 09752509
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2017-09-05
[patent_title] => 'Method for controlling coupling of shafts between a first machine and a second machine using rotation speeds and angles'
[patent_app_type] => utility
[patent_app_number] => 14/010669
[patent_app_country] => US
[patent_app_date] => 2013-08-27
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[rel_patent_id] =>[rel_patent_doc_number] =>) 14/010669 | Method for controlling coupling of shafts between a first machine and a second machine using rotation speeds and angles | Aug 26, 2013 | Issued |
Array
(
[id] => 10326417
[patent_doc_number] => 20150211421
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2015-07-30
[patent_title] => 'METHOD AND SYSTEM FOR STARTING AN AIRCRAFT TURBOENGINE'
[patent_app_type] => utility
[patent_app_number] => 14/426310
[patent_app_country] => US
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[rel_patent_id] =>[rel_patent_doc_number] =>) 14/426310 | Method and system for starting an aircraft turboengine | Aug 26, 2013 | Issued |
Array
(
[id] => 11994669
[patent_doc_number] => 20170298824
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2017-10-19
[patent_title] => 'Gas-turbine combustion chamber with impingement-cooled bolts of the combustion\nchamber tiles'
[patent_app_type] => utility
[patent_app_number] => 13/971328
[patent_app_country] => US
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[rel_patent_id] =>[rel_patent_doc_number] =>) 13/971328 | Gas-turbine combustion chamber with impingement-cooled bolts of the combustion chamber tiles | Aug 19, 2013 | Issued |
Array
(
[id] => 9892169
[patent_doc_number] => 20150047368
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2015-02-19
[patent_title] => 'SYSTEMS AND METHODS FOR CONTROLLING GAS TURBINES'
[patent_app_type] => utility
[patent_app_number] => 13/965863
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[rel_patent_id] =>[rel_patent_doc_number] =>) 13/965863 | SYSTEMS AND METHODS FOR CONTROLLING GAS TURBINES | Aug 12, 2013 | Abandoned |
Array
(
[id] => 9860550
[patent_doc_number] => 20150040567
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2015-02-12
[patent_title] => 'Systems and Methods for Reducing or Limiting One or More Flows Between a Hot Gas Path and a Wheel Space of a Turbine'
[patent_app_type] => utility
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[rel_patent_id] =>[rel_patent_doc_number] =>) 13/962244 | Systems and Methods for Reducing or Limiting One or More Flows Between a Hot Gas Path and a Wheel Space of a Turbine | Aug 7, 2013 | Abandoned |
Array
(
[id] => 9860518
[patent_doc_number] => 20150040535
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2015-02-12
[patent_title] => 'INLET PARTICLE SEPARATOR SYSTEM WITH HUB AND/OR SHROUD SUCTION'
[patent_app_type] => utility
[patent_app_number] => 13/961284
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[rel_patent_id] =>[rel_patent_doc_number] =>) 13/961284 | Inlet particle separator system with flow passage through hub and/or shroud | Aug 6, 2013 | Issued |
Array
(
[id] => 9860554
[patent_doc_number] => 20150040571
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2015-02-12
[patent_title] => 'METHOD FOR FUEL SPLIT CONTROL TO A GAS TURBINE USING A MODIFIED TURBINE FIRING TEMPERATURE'
[patent_app_type] => utility
[patent_app_number] => 13/960907
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Array
(
[id] => 9277568
[patent_doc_number] => 20140027536
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[patent_issue_date] => 2014-01-30
[patent_title] => 'TRANSLATING CASCADES'
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[rel_patent_id] =>[rel_patent_doc_number] =>) 13/949952 | Translating sleeve thrust reverser with movable cascade | Jul 23, 2013 | Issued |
Array
(
[id] => 9835045
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[rel_patent_id] =>[rel_patent_doc_number] =>) 13/949640 | SYSTEM FOR PROVIDING FUEL TO A COMBUSTOR | Jul 23, 2013 | Abandoned |
Array
(
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[rel_patent_id] =>[rel_patent_doc_number] =>) 13/932157 | System and method for reducing emissions via solvent injection | Jun 30, 2013 | Issued |