Search

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 numberTitle of the applicationFiling DateStatus
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 [patent_figures_cnt] => 9 [patent_no_of_words] => 6635 [patent_no_of_claims] => 21 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 124 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [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 [patent_no_of_assignments] => 0 [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 [patent_words_short_claim] => 0 [patent_maintenance] => 1 [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 [patent_figures_cnt] => 3 [patent_no_of_words] => 3243 [patent_no_of_claims] => 9 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 183 [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 [patent_figures_cnt] => 5 [patent_no_of_words] => 6132 [patent_no_of_claims] => 19 [patent_no_of_ind_claims] => 4 [patent_words_short_claim] => 159 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [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 [patent_words_short_claim] => 0 [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 [patent_words_short_claim] => 0 [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 [patent_figures_cnt] => 4 [patent_no_of_words] => 4432 [patent_no_of_claims] => 20 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 0 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [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 [patent_figures_cnt] => 5 [patent_no_of_words] => 1581 [patent_no_of_claims] => 20 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 0 [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 [patent_figures_cnt] => 1 [patent_no_of_words] => 2498 [patent_no_of_claims] => 18 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 106 [patent_maintenance] => 1 [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 [patent_figures_cnt] => 2 [patent_no_of_words] => 5570 [patent_no_of_claims] => 15 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 0 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [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 [patent_drawing_sheets_cnt] => 7 [patent_figures_cnt] => 7 [patent_no_of_words] => 4394 [patent_no_of_claims] => 20 [patent_no_of_ind_claims] => 4 [patent_words_short_claim] => 0 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [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 [patent_figures_cnt] => 10 [patent_no_of_words] => 2424 [patent_no_of_claims] => 20 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 0 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [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 [patent_drawing_sheets_cnt] => 5 [patent_figures_cnt] => 5 [patent_no_of_words] => 4570 [patent_no_of_claims] => 12 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 0 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [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 [patent_figures_cnt] => 13 [patent_no_of_words] => 4951 [patent_no_of_claims] => 19 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 0 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [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 [patent_drawing_sheets_cnt] => 3 [patent_figures_cnt] => 3 [patent_no_of_words] => 1842 [patent_no_of_claims] => 16 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 0 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [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 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2015-08-18 [patent_title] => 'Lock for a translating sleeve of a nacelle' [patent_app_type] => utility [patent_app_number] => 13/664993 [patent_app_country] => US [patent_app_date] => 2012-10-31 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 12 [patent_figures_cnt] => 18 [patent_no_of_words] => 5395 [patent_no_of_claims] => 20 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 135 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13664993 [rel_patent_id] =>[rel_patent_doc_number] =>)
13/664993
Lock for a translating sleeve of a nacelle Oct 30, 2012 Issued
Array ( [id] => 13038581 [patent_doc_number] => 10041417 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2018-08-07 [patent_title] => Gas turbine system with injection water pressurization passage [patent_app_type] => utility [patent_app_number] => 14/355774 [patent_app_country] => US [patent_app_date] => 2012-10-29 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 6 [patent_figures_cnt] => 13 [patent_no_of_words] => 4807 [patent_no_of_claims] => 5 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 146 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14355774 [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 [patent_country] => US [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 [patent_app_country] => US [patent_app_date] => 2012-10-26 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 6 [patent_figures_cnt] => 6 [patent_no_of_words] => 2995 [patent_no_of_claims] => 20 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 0 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [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
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