
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] => 10602001
[patent_doc_number] => 09322558
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2016-04-26
[patent_title] => 'Combustor apparatus in a gas turbine engine'
[patent_app_type] => utility
[patent_app_number] => 13/928476
[patent_app_country] => US
[patent_app_date] => 2013-06-27
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 8
[patent_figures_cnt] => 10
[patent_no_of_words] => 5974
[patent_no_of_claims] => 16
[patent_no_of_ind_claims] => 4
[patent_words_short_claim] => 335
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13928476
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/928476 | Combustor apparatus in a gas turbine engine | Jun 26, 2013 | Issued |
Array
(
[id] => 10649944
[patent_doc_number] => 09366184
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2016-06-14
[patent_title] => 'Gas turbine engine and method of operating thereof'
[patent_app_type] => utility
[patent_app_number] => 13/920244
[patent_app_country] => US
[patent_app_date] => 2013-06-18
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
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[patent_no_of_words] => 6635
[patent_no_of_claims] => 21
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[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13920244
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/920244 | Gas turbine engine and method of operating thereof | Jun 17, 2013 | Issued |
Array
(
[id] => 10236890
[patent_doc_number] => 20150121883
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2015-05-07
[patent_title] => 'FLUID CONDUIT'
[patent_app_type] => utility
[patent_app_number] => 14/407400
[patent_app_country] => US
[patent_app_date] => 2013-06-14
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 9
[patent_figures_cnt] => 9
[patent_no_of_words] => 2537
[patent_no_of_claims] => 15
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 0
[patent_maintenance] => 1
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[patent_current_assignee] =>[type] => publication
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14407400
[rel_patent_id] =>[rel_patent_doc_number] =>) 14/407400 | Two flow path fuel conduit of a gas turbine engine | Jun 13, 2013 | Issued |
Array
(
[id] => 9666581
[patent_doc_number] => 20140230444
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2014-08-21
[patent_title] => 'System and Method for Reducing Back Pressure in a Gas Turbine System'
[patent_app_type] => utility
[patent_app_number] => 13/901518
[patent_app_country] => US
[patent_app_date] => 2013-05-23
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
[patent_figures_cnt] => 5
[patent_no_of_words] => 5050
[patent_no_of_claims] => 20
[patent_no_of_ind_claims] => 3
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[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13901518
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/901518 | System and method for reducing back pressure in a gas turbine system | May 22, 2013 | Issued |
Array
(
[id] => 13169261
[patent_doc_number] => 10100737
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2018-10-16
[patent_title] => Impingement cooling arrangement having a snap-in plate
[patent_app_type] => utility
[patent_app_number] => 13/895831
[patent_app_country] => US
[patent_app_date] => 2013-05-16
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 2
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[patent_no_of_words] => 3243
[patent_no_of_claims] => 9
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[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13895831
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/895831 | Impingement cooling arrangement having a snap-in plate | May 15, 2013 | Issued |
Array
(
[id] => 11464468
[patent_doc_number] => 09581089
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2017-02-28
[patent_title] => 'Gas dosage control for gas engine'
[patent_app_type] => utility
[patent_app_number] => 13/891807
[patent_app_country] => US
[patent_app_date] => 2013-05-10
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
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[patent_no_of_words] => 6132
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[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13891807
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/891807 | Gas dosage control for gas engine | May 9, 2013 | Issued |
Array
(
[id] => 10928616
[patent_doc_number] => 20140331637
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2014-11-13
[patent_title] => 'TURBINE ENGINE SHUTDOWN TEMPERATURE CONTROL SYSTEM WITH AN ELONGATED EJECTOR'
[patent_app_type] => utility
[patent_app_number] => 13/890297
[patent_app_country] => US
[patent_app_date] => 2013-05-09
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 4
[patent_no_of_words] => 2851
[patent_no_of_claims] => 20
[patent_no_of_ind_claims] => 3
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[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13890297
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/890297 | Turbine engine shutdown temperature control system with an elongated ejector | May 8, 2013 | Issued |
Array
(
[id] => 10902119
[patent_doc_number] => 20140305130
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2014-10-16
[patent_title] => 'AIRCRAFT ENVIRONMENTAL CONTROL SYSTEM INLET FLOW CONTROL'
[patent_app_type] => utility
[patent_app_number] => 13/859978
[patent_app_country] => US
[patent_app_date] => 2013-04-10
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 3
[patent_no_of_words] => 3390
[patent_no_of_claims] => 16
[patent_no_of_ind_claims] => 3
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[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13859978
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/859978 | Aircraft environmental control system inlet flow control | Apr 9, 2013 | Issued |
Array
(
[id] => 9766601
[patent_doc_number] => 20140290261
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2014-10-02
[patent_title] => 'COMPENSATION FOR GAS TURBINE ENGINE FUEL VALVE CHARACTERISTICS'
[patent_app_type] => utility
[patent_app_number] => 13/852691
[patent_app_country] => US
[patent_app_date] => 2013-03-28
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
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[patent_no_of_words] => 4432
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[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13852691
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/852691 | COMPENSATION FOR GAS TURBINE ENGINE FUEL VALVE CHARACTERISTICS | Mar 27, 2013 | Abandoned |
Array
(
[id] => 9715216
[patent_doc_number] => 20140250914
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2014-09-11
[patent_title] => 'Starter Motor Shared Lubrication System'
[patent_app_type] => utility
[patent_app_number] => 13/792567
[patent_app_country] => US
[patent_app_date] => 2013-03-11
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
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[patent_no_of_words] => 1581
[patent_no_of_claims] => 20
[patent_no_of_ind_claims] => 2
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[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13792567
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/792567 | Starter Motor Shared Lubrication System | Mar 10, 2013 | Abandoned |
Array
(
[id] => 11874133
[patent_doc_number] => 09745896
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2017-08-29
[patent_title] => 'Systems and methods to control combustion dynamic frequencies based on a compressor discharge temperature'
[patent_app_type] => utility
[patent_app_number] => 13/777724
[patent_app_country] => US
[patent_app_date] => 2013-02-26
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 1
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[patent_no_of_words] => 2498
[patent_no_of_claims] => 18
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[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13777724
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/777724 | Systems and methods to control combustion dynamic frequencies based on a compressor discharge temperature | Feb 25, 2013 | Issued |
Array
(
[id] => 9265480
[patent_doc_number] => 20140020396
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2014-01-23
[patent_title] => 'METHOD OF AUTOMATICALLY REGULATING AN AIRCRAFT POWER PLANT, A DEVICE, AND AN AIRCRAFT'
[patent_app_type] => utility
[patent_app_number] => 13/753690
[patent_app_country] => US
[patent_app_date] => 2013-01-30
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 2
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[patent_current_assignee] =>[type] => publication
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13753690
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/753690 | Method of automatically regulating aircraft power plant gas generator and free turbine speeds as a function of heating, electricity generation, noise emission, and fuel consumption | Jan 29, 2013 | Issued |
Array
(
[id] => 9459241
[patent_doc_number] => 20140123666
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2014-05-08
[patent_title] => 'System to Improve Gas Turbine Output and Hot Gas Path Component Life Utilizing Humid Air for Nozzle Over Cooling'
[patent_app_type] => utility
[patent_app_number] => 13/751675
[patent_app_country] => US
[patent_app_date] => 2013-01-28
[patent_effective_date] => 0000-00-00
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[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13751675
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/751675 | System to Improve Gas Turbine Output and Hot Gas Path Component Life Utilizing Humid Air for Nozzle Over Cooling | Jan 27, 2013 | Abandoned |
Array
(
[id] => 9681265
[patent_doc_number] => 20140238027
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2014-08-28
[patent_title] => 'THERMALLY COMPLIANT DUAL WALL LINER FOR A GAS TURBINE ENGINE'
[patent_app_type] => utility
[patent_app_number] => 13/725114
[patent_app_country] => US
[patent_app_date] => 2012-12-21
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 10
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[patent_no_of_words] => 2424
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[patent_current_assignee] =>[type] => publication
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13725114
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/725114 | THERMALLY COMPLIANT DUAL WALL LINER FOR A GAS TURBINE ENGINE | Dec 20, 2012 | Abandoned |
Array
(
[id] => 10908146
[patent_doc_number] => 20140311161
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2014-10-23
[patent_title] => 'METHOD FOR CREATING A CONNECTING ELEMENT POSITIONED BETWEEN TWO COMPONENTS OF A STRUCTURE, CONNECTING ELEMENT AND BYPASS TURBOJET ENGINE COMPRISING SUCH A CONNECTING ELEMENT'
[patent_app_type] => utility
[patent_app_number] => 14/362267
[patent_app_country] => US
[patent_app_date] => 2012-12-10
[patent_effective_date] => 0000-00-00
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[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14362267
[rel_patent_id] =>[rel_patent_doc_number] =>) 14/362267 | METHOD FOR CREATING A CONNECTING ELEMENT POSITIONED BETWEEN TWO COMPONENTS OF A STRUCTURE, CONNECTING ELEMENT AND BYPASS TURBOJET ENGINE COMPRISING SUCH A CONNECTING ELEMENT | Dec 9, 2012 | Abandoned |
Array
(
[id] => 9459231
[patent_doc_number] => 20140123656
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2014-05-08
[patent_title] => 'MODULAR DROP-IN TRANSITION ASSEMBLY FOR INDUSTRIAL GAS TURBINE AND METHOD FOR INSTALLATION'
[patent_app_type] => utility
[patent_app_number] => 13/672878
[patent_app_country] => US
[patent_app_date] => 2012-11-09
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 13
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[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13672878
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/672878 | Modular drop-in transition assembly for industrial gas turbine and method for installation | Nov 8, 2012 | Issued |
Array
(
[id] => 9201059
[patent_doc_number] => 20140000236
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2014-01-02
[patent_title] => 'COMBUSTOR'
[patent_app_type] => utility
[patent_app_number] => 13/670834
[patent_app_country] => US
[patent_app_date] => 2012-11-07
[patent_effective_date] => 0000-00-00
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[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13670834
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/670834 | COMBUSTOR | Nov 6, 2012 | Abandoned |
Array
(
[id] => 10071193
[patent_doc_number] => 09109541
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[patent_kind] => B2
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[patent_title] => 'Lock for a translating sleeve of a nacelle'
[patent_app_type] => utility
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[rel_patent_id] =>[rel_patent_doc_number] =>) 13/664993 | Lock for a translating sleeve of a nacelle | Oct 30, 2012 | Issued |
Array
(
[id] => 13038581
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[patent_kind] => B2
[patent_issue_date] => 2018-08-07
[patent_title] => Gas turbine system with injection water pressurization passage
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[patent_app_number] => 14/355774
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[rel_patent_id] =>[rel_patent_doc_number] =>) 14/355774 | Gas turbine system with injection water pressurization passage | Oct 28, 2012 | Issued |
Array
(
[id] => 9637888
[patent_doc_number] => 20140215998
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[patent_kind] => A1
[patent_issue_date] => 2014-08-07
[patent_title] => 'GAS TURBINE ENGINES WITH IMPROVED COMPRESSOR BLADES'
[patent_app_type] => utility
[patent_app_number] => 13/662287
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[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13662287
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/662287 | GAS TURBINE ENGINES WITH IMPROVED COMPRESSOR BLADES | Oct 25, 2012 | Abandoned |