
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 number | Title of the application | Filing Date | Status |
|---|---|---|---|
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
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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] => 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
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[patent_no_of_words] => 3397
[patent_no_of_claims] => 20
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[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
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[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
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[patent_current_assignee] =>[type] => patent
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[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
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[patent_no_of_words] => 3160
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[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
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[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
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[patent_no_of_words] => 5707
[patent_no_of_claims] => 18
[patent_no_of_ind_claims] => 3
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[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
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[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
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[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
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[patent_no_of_words] => 6998
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[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
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[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
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[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
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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] => 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
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[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
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[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'
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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] => 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
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Array
(
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[patent_title] => 'System and method for reducing modal coupling of combustion dynamics'
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Array
(
[id] => 10299858
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[patent_title] => 'METHOD OF OPERATING A MULTI-STAGE FLAMESHEET COMBUSTOR'
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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 |