Search

Marc J. Amar

Examiner (ID: 13699, Phone: (571)272-9948 , Office: P/3741 )

Most Active Art Unit
3741
Art Unit(s)
3741
Total Applications
481
Issued Applications
342
Pending Applications
52
Abandoned Applications
95

Applications

Application numberTitle of the applicationFiling DateStatus
Array ( [id] => 11178513 [patent_doc_number] => 09410500 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2016-08-09 [patent_title] => 'Movable cascade turbojet thrust reverser having translatable reverser cowl causing variation in jet nozzle' [patent_app_type] => utility [patent_app_number] => 14/173464 [patent_app_country] => US [patent_app_date] => 2014-02-05 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 5 [patent_figures_cnt] => 10 [patent_no_of_words] => 3504 [patent_no_of_claims] => 6 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 258 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14173464 [rel_patent_id] =>[rel_patent_doc_number] =>)
14/173464
Movable cascade turbojet thrust reverser having translatable reverser cowl causing variation in jet nozzle Feb 4, 2014 Issued
Array ( [id] => 9652915 [patent_doc_number] => 20140223919 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2014-08-14 [patent_title] => 'FLEXIBLE LINER HANGER' [patent_app_type] => utility [patent_app_number] => 14/172183 [patent_app_country] => US [patent_app_date] => 2014-02-04 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 6 [patent_figures_cnt] => 6 [patent_no_of_words] => 3397 [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] => 14172183 [rel_patent_id] =>[rel_patent_doc_number] =>)
14/172183
FLEXIBLE LINER HANGER Feb 3, 2014 Abandoned
Array ( [id] => 13917595 [patent_doc_number] => 10202906 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2019-02-12 [patent_title] => Two-shaft gas turbine [patent_app_type] => utility [patent_app_number] => 14/155813 [patent_app_country] => US [patent_app_date] => 2014-01-15 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 5 [patent_figures_cnt] => 10 [patent_no_of_words] => 8375 [patent_no_of_claims] => 3 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 270 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14155813 [rel_patent_id] =>[rel_patent_doc_number] =>)
14/155813
Two-shaft gas turbine Jan 14, 2014 Issued
Array ( [id] => 11576304 [patent_doc_number] => 09631554 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2017-04-25 [patent_title] => 'Electrostatic charge control inlet particle separator system' [patent_app_type] => utility [patent_app_number] => 14/154428 [patent_app_country] => US [patent_app_date] => 2014-01-14 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 4 [patent_figures_cnt] => 6 [patent_no_of_words] => 3635 [patent_no_of_claims] => 13 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 278 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14154428 [rel_patent_id] =>[rel_patent_doc_number] =>)
14/154428
Electrostatic charge control inlet particle separator system Jan 13, 2014 Issued
Array ( [id] => 11829373 [patent_doc_number] => 09726110 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2017-08-08 [patent_title] => 'Aircraft propulsion system fan case comprising thrust reversing assembly' [patent_app_type] => utility [patent_app_number] => 14/090595 [patent_app_country] => US [patent_app_date] => 2013-11-26 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 3 [patent_figures_cnt] => 3 [patent_no_of_words] => 3160 [patent_no_of_claims] => 11 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 243 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14090595 [rel_patent_id] =>[rel_patent_doc_number] =>)
14/090595
Aircraft propulsion system fan case comprising thrust reversing assembly Nov 25, 2013 Issued
Array ( [id] => 9359218 [patent_doc_number] => 20140069090 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2014-03-13 [patent_title] => 'PRIME MOVER WITH RECOVERED ENERGY DRIVEN COMPRESSION OF THE WORKING FLUID' [patent_app_type] => utility [patent_app_number] => 14/082221 [patent_app_country] => US [patent_app_date] => 2013-11-18 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 2 [patent_figures_cnt] => 2 [patent_no_of_words] => 3543 [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] => 14082221 [rel_patent_id] =>[rel_patent_doc_number] =>)
14/082221
PRIME MOVER WITH RECOVERED ENERGY DRIVEN COMPRESSION OF THE WORKING FLUID Nov 17, 2013 Abandoned
Array ( [id] => 11810066 [patent_doc_number] => 09714627 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2017-07-25 [patent_title] => 'Mounting of aircraft propulsion system outer sleeve and inner structure to pylon with distinct hinges' [patent_app_type] => utility [patent_app_number] => 14/081125 [patent_app_country] => US [patent_app_date] => 2013-11-15 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 6 [patent_figures_cnt] => 7 [patent_no_of_words] => 2997 [patent_no_of_claims] => 12 [patent_no_of_ind_claims] => 2 [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] => 14081125 [rel_patent_id] =>[rel_patent_doc_number] =>)
14/081125
Mounting of aircraft propulsion system outer sleeve and inner structure to pylon with distinct hinges Nov 14, 2013 Issued
Array ( [id] => 11774221 [patent_doc_number] => 09383107 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2016-07-05 [patent_title] => 'Dual fuel nozzle tip assembly with impingement cooled nozzle tip' [patent_app_type] => utility [patent_app_number] => 14/077557 [patent_app_country] => US [patent_app_date] => 2013-11-12 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 6 [patent_figures_cnt] => 10 [patent_no_of_words] => 5707 [patent_no_of_claims] => 18 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 185 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14077557 [rel_patent_id] =>[rel_patent_doc_number] =>)
14/077557
Dual fuel nozzle tip assembly with impingement cooled nozzle tip Nov 11, 2013 Issued
Array ( [id] => 10243563 [patent_doc_number] => 20150128558 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2015-05-14 [patent_title] => 'SOLAR FIRED COMBINED CYCLE WITH SUPERCRITICAL TURBINE' [patent_app_type] => utility [patent_app_number] => 14/076727 [patent_app_country] => US [patent_app_date] => 2013-11-11 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 7 [patent_figures_cnt] => 7 [patent_no_of_words] => 8660 [patent_no_of_claims] => 16 [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] => 14076727 [rel_patent_id] =>[rel_patent_doc_number] =>)
14/076727
SOLAR FIRED COMBINED CYCLE WITH SUPERCRITICAL TURBINE Nov 10, 2013 Abandoned
Array ( [id] => 10236893 [patent_doc_number] => 20150121887 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2015-05-07 [patent_title] => 'AUTOMATED CONTROL OF PART-SPEED GAS TURBINE OPERATION' [patent_app_type] => utility [patent_app_number] => 14/071127 [patent_app_country] => US [patent_app_date] => 2013-11-04 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 7 [patent_figures_cnt] => 7 [patent_no_of_words] => 3277 [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] => 14071127 [rel_patent_id] =>[rel_patent_doc_number] =>)
14/071127
AUTOMATED CONTROL OF PART-SPEED GAS TURBINE OPERATION Nov 3, 2013 Abandoned
Array ( [id] => 10229001 [patent_doc_number] => 20150113993 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2015-04-30 [patent_title] => 'GAS TURBINE ENGINES HAVING FUEL INJECTOR SHROUDS WITH INTERIOR RIBS' [patent_app_type] => utility [patent_app_number] => 14/067377 [patent_app_country] => US [patent_app_date] => 2013-10-30 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 10 [patent_figures_cnt] => 10 [patent_no_of_words] => 6998 [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] => 14067377 [rel_patent_id] =>[rel_patent_doc_number] =>)
14/067377
Gas turbine engines having fuel injector shrouds with interior ribs Oct 29, 2013 Issued
Array ( [id] => 9564590 [patent_doc_number] => 20140182303 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2014-07-03 [patent_title] => 'SYSTEM AND METHOD FOR A TURBINE COMBUSTOR' [patent_app_type] => utility [patent_app_number] => 14/067726 [patent_app_country] => US [patent_app_date] => 2013-10-30 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 18 [patent_figures_cnt] => 18 [patent_no_of_words] => 25056 [patent_no_of_claims] => 34 [patent_no_of_ind_claims] => 17 [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] => 14067726 [rel_patent_id] =>[rel_patent_doc_number] =>)
14/067726
System and method for a turbine combustor Oct 29, 2013 Issued
Array ( [id] => 11845123 [patent_doc_number] => 09732672 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2017-08-15 [patent_title] => 'Method and system for gas turbine power augmentation using steam injection' [patent_app_type] => utility [patent_app_number] => 14/064815 [patent_app_country] => US [patent_app_date] => 2013-10-28 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 4 [patent_figures_cnt] => 4 [patent_no_of_words] => 5353 [patent_no_of_claims] => 20 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 152 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14064815 [rel_patent_id] =>[rel_patent_doc_number] =>)
14/064815
Method and system for gas turbine power augmentation using steam injection Oct 27, 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 [patent_figures_cnt] => 5 [patent_no_of_words] => 4932 [patent_no_of_claims] => 6 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 193 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14060094 [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] => 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 [patent_no_of_words] => 3161 [patent_no_of_claims] => 12 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 191 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [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] => 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 [patent_drawing_sheets_cnt] => 7 [patent_figures_cnt] => 11 [patent_no_of_words] => 5532 [patent_no_of_claims] => 15 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 210 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14055106 [rel_patent_id] =>[rel_patent_doc_number] =>)
14/055106
Locking spacer assembly Oct 15, 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 [patent_figures_cnt] => 10 [patent_no_of_words] => 5201 [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] => 14055091 [rel_patent_id] =>[rel_patent_doc_number] =>)
14/055091
Locking spacer assembly inserted between rotor blades Oct 15, 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 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 12 [patent_figures_cnt] => 12 [patent_no_of_words] => 7754 [patent_no_of_claims] => 12 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 224 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14048252 [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] => 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 [patent_app_date] => 2013-10-08 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 12 [patent_figures_cnt] => 12 [patent_no_of_words] => 8900 [patent_no_of_claims] => 15 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 182 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14048272 [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] => 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 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 10 [patent_figures_cnt] => 10 [patent_no_of_words] => 5922 [patent_no_of_claims] => 31 [patent_no_of_ind_claims] => 5 [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] => 14038070 [rel_patent_id] =>[rel_patent_doc_number] =>)
14/038070
METHOD OF OPERATING A MULTI-STAGE FLAMESHEET COMBUSTOR Sep 25, 2013 Abandoned
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