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] => 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] => 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] => 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] => 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] => 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] => 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] => 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
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 [patent_figures_cnt] => 2 [patent_no_of_words] => 534 [patent_no_of_claims] => 4 [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] => 14034551 [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 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 4 [patent_figures_cnt] => 5 [patent_no_of_words] => 2978 [patent_no_of_claims] => 19 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 150 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14024892 [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 [patent_figures_cnt] => 5 [patent_no_of_words] => 5827 [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] => 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 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 6 [patent_figures_cnt] => 8 [patent_no_of_words] => 3691 [patent_no_of_claims] => 14 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 284 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14010669 [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 [patent_app_date] => 2013-08-27 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 3 [patent_figures_cnt] => 3 [patent_no_of_words] => 4392 [patent_no_of_claims] => 9 [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] => 14426310 [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 [patent_app_date] => 2013-08-20 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 4 [patent_figures_cnt] => 4 [patent_no_of_words] => 2615 [patent_no_of_claims] => 11 [patent_no_of_ind_claims] => 1 [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] => 13971328 [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 [patent_app_country] => US [patent_app_date] => 2013-08-13 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 5 [patent_figures_cnt] => 5 [patent_no_of_words] => 3801 [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] => 13965863 [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 [patent_app_number] => 13/962244 [patent_app_country] => US [patent_app_date] => 2013-08-08 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 6 [patent_figures_cnt] => 6 [patent_no_of_words] => 2520 [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] => 13962244 [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 [patent_app_country] => US [patent_app_date] => 2013-08-07 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 7 [patent_figures_cnt] => 7 [patent_no_of_words] => 2877 [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] => 13961284 [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 [patent_app_country] => US [patent_app_date] => 2013-08-07 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 7 [patent_figures_cnt] => 7 [patent_no_of_words] => 5043 [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] => 13960907 [rel_patent_id] =>[rel_patent_doc_number] =>)
13/960907
METHOD FOR FUEL SPLIT CONTROL TO A GAS TURBINE USING A MODIFIED TURBINE FIRING TEMPERATURE Aug 6, 2013 Abandoned
Array ( [id] => 9277568 [patent_doc_number] => 20140027536 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2014-01-30 [patent_title] => 'TRANSLATING CASCADES' [patent_app_type] => utility [patent_app_number] => 13/949952 [patent_app_country] => US [patent_app_date] => 2013-07-24 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 8 [patent_figures_cnt] => 8 [patent_no_of_words] => 4547 [patent_no_of_claims] => 19 [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] => 13949952 [rel_patent_id] =>[rel_patent_doc_number] =>)
13/949952
Translating sleeve thrust reverser with movable cascade Jul 23, 2013 Issued
Array ( [id] => 9835045 [patent_doc_number] => 20150027126 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2015-01-29 [patent_title] => 'SYSTEM FOR PROVIDING FUEL TO A COMBUSTOR' [patent_app_type] => utility [patent_app_number] => 13/949640 [patent_app_country] => US [patent_app_date] => 2013-07-24 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 8 [patent_figures_cnt] => 8 [patent_no_of_words] => 4091 [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] => 13949640 [rel_patent_id] =>[rel_patent_doc_number] =>)
13/949640
SYSTEM FOR PROVIDING FUEL TO A COMBUSTOR Jul 23, 2013 Abandoned
Array ( [id] => 11772689 [patent_doc_number] => 09381462 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2016-07-05 [patent_title] => 'System and method for reducing emissions via solvent injection' [patent_app_type] => utility [patent_app_number] => 13/932157 [patent_app_country] => US [patent_app_date] => 2013-07-01 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 3 [patent_figures_cnt] => 3 [patent_no_of_words] => 3428 [patent_no_of_claims] => 18 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 199 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13932157 [rel_patent_id] =>[rel_patent_doc_number] =>)
13/932157
System and method for reducing emissions via solvent injection Jun 30, 2013 Issued
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