
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] => 15754995
[patent_doc_number] => 10619598
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2020-04-14
[patent_title] => Nacelle for an aircraft engine with variable section nozzle
[patent_app_type] => utility
[patent_app_number] => 15/093805
[patent_app_country] => US
[patent_app_date] => 2016-04-08
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
[patent_figures_cnt] => 16
[patent_no_of_words] => 4860
[patent_no_of_claims] => 11
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 336
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 15093805
[rel_patent_id] =>[rel_patent_doc_number] =>) 15/093805 | Nacelle for an aircraft engine with variable section nozzle | Apr 7, 2016 | Issued |
Array
(
[id] => 15667645
[patent_doc_number] => 10598044
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2020-03-24
[patent_title] => Oil jet for turbine engine with housing including sealing membrane
[patent_app_type] => utility
[patent_app_number] => 15/563036
[patent_app_country] => US
[patent_app_date] => 2016-03-31
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 1
[patent_figures_cnt] => 4
[patent_no_of_words] => 2247
[patent_no_of_claims] => 11
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 142
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 15563036
[rel_patent_id] =>[rel_patent_doc_number] =>) 15/563036 | Oil jet for turbine engine with housing including sealing membrane | Mar 30, 2016 | Issued |
Array
(
[id] => 11091948
[patent_doc_number] => 20160288916
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2016-10-06
[patent_title] => 'ENGINE COWLING OF AN AIRCRAFT GAS TURBINE'
[patent_app_type] => utility
[patent_app_number] => 15/087228
[patent_app_country] => US
[patent_app_date] => 2016-03-31
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 4
[patent_no_of_words] => 2249
[patent_no_of_claims] => 10
[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] => 15087228
[rel_patent_id] =>[rel_patent_doc_number] =>) 15/087228 | Engine cowling of an aircraft gas turbine | Mar 30, 2016 | Issued |
Array
(
[id] => 16329139
[patent_doc_number] => 20200300105
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2020-09-24
[patent_title] => GAS TURBINE ENGINE, CORRESPONDING SEAL SECTION AND INTEGRATED EXIT PIECE
[patent_app_type] => utility
[patent_app_number] => 16/088204
[patent_app_country] => US
[patent_app_date] => 2016-03-25
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 0
[patent_figures_cnt] => 0
[patent_no_of_words] => 2773
[patent_no_of_claims] => 0
[patent_no_of_ind_claims] => -17
[patent_words_short_claim] => 133
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 16088204
[rel_patent_id] =>[rel_patent_doc_number] =>) 16/088204 | GAS TURBINE ENGINE, CORRESPONDING SEAL SECTION AND INTEGRATED EXIT PIECE | Mar 24, 2016 | Abandoned |
Array
(
[id] => 14423995
[patent_doc_number] => 10316793
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2019-06-11
[patent_title] => Thrust reverser track beam with integrated actuator fitting
[patent_app_type] => utility
[patent_app_number] => 15/068010
[patent_app_country] => US
[patent_app_date] => 2016-03-11
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 7
[patent_figures_cnt] => 9
[patent_no_of_words] => 3366
[patent_no_of_claims] => 9
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 100
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 15068010
[rel_patent_id] =>[rel_patent_doc_number] =>) 15/068010 | Thrust reverser track beam with integrated actuator fitting | Mar 10, 2016 | Issued |
Array
(
[id] => 10823358
[patent_doc_number] => 20160169523
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2016-06-16
[patent_title] => 'FUEL INJECTION DEVICE FOR GAS TURBINE'
[patent_app_type] => utility
[patent_app_number] => 15/051993
[patent_app_country] => US
[patent_app_date] => 2016-02-24
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 8
[patent_figures_cnt] => 8
[patent_no_of_words] => 5070
[patent_no_of_claims] => 7
[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] => 15051993
[rel_patent_id] =>[rel_patent_doc_number] =>) 15/051993 | Fuel injection device for gas turbine | Feb 23, 2016 | Issued |
Array
(
[id] => 14612581
[patent_doc_number] => 10358980
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2019-07-23
[patent_title] => Fuel supply apparatus for aircraft engine
[patent_app_type] => utility
[patent_app_number] => 15/050800
[patent_app_country] => US
[patent_app_date] => 2016-02-23
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 6
[patent_figures_cnt] => 6
[patent_no_of_words] => 7637
[patent_no_of_claims] => 3
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 197
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 15050800
[rel_patent_id] =>[rel_patent_doc_number] =>) 15/050800 | Fuel supply apparatus for aircraft engine | Feb 22, 2016 | Issued |
Array
(
[id] => 17556869
[patent_doc_number] => 11313559
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2022-04-26
[patent_title] => Method and device for flame stabilization in a burner system of a stationary combustion engine
[patent_app_type] => utility
[patent_app_number] => 15/050244
[patent_app_country] => US
[patent_app_date] => 2016-02-22
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
[patent_figures_cnt] => 17
[patent_no_of_words] => 5507
[patent_no_of_claims] => 11
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 163
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 15050244
[rel_patent_id] =>[rel_patent_doc_number] =>) 15/050244 | Method and device for flame stabilization in a burner system of a stationary combustion engine | Feb 21, 2016 | Issued |
Array
(
[id] => 11048272
[patent_doc_number] => 20160245230
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2016-08-25
[patent_title] => 'ENGINE COWLING OF A GAS TURBINE WITH THRUST-REVERSING DEVICE AND CROSS-SECTIONALLY ADJUSTABLE OUTLET NOZZLE'
[patent_app_type] => utility
[patent_app_number] => 15/047257
[patent_app_country] => US
[patent_app_date] => 2016-02-18
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 4
[patent_no_of_words] => 2873
[patent_no_of_claims] => 6
[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] => 15047257
[rel_patent_id] =>[rel_patent_doc_number] =>) 15/047257 | Engine cowling of a gas turbine with thrust-reversing device and cross-sectionally adjustable outlet nozzle | Feb 17, 2016 | Issued |
Array
(
[id] => 11937144
[patent_doc_number] => 20170241294
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2017-08-24
[patent_title] => 'EXHAUST SYSTEM FOR GAS TURBINE ENGINE'
[patent_app_type] => utility
[patent_app_number] => 15/046946
[patent_app_country] => US
[patent_app_date] => 2016-02-18
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 4
[patent_no_of_words] => 4373
[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] => 15046946
[rel_patent_id] =>[rel_patent_doc_number] =>) 15/046946 | EXHAUST SYSTEM FOR GAS TURBINE ENGINE | Feb 17, 2016 | Abandoned |
Array
(
[id] => 14032791
[patent_doc_number] => 10228140
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2019-03-12
[patent_title] => Gas-only cartridge for a premix fuel nozzle
[patent_app_type] => utility
[patent_app_number] => 15/046482
[patent_app_country] => US
[patent_app_date] => 2016-02-18
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 6
[patent_figures_cnt] => 9
[patent_no_of_words] => 4619
[patent_no_of_claims] => 12
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 189
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 15046482
[rel_patent_id] =>[rel_patent_doc_number] =>) 15/046482 | Gas-only cartridge for a premix fuel nozzle | Feb 17, 2016 | Issued |
Array
(
[id] => 15228891
[patent_doc_number] => 10502160
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2019-12-10
[patent_title] => Reverse thrust engine
[patent_app_type] => utility
[patent_app_number] => 15/018893
[patent_app_country] => US
[patent_app_date] => 2016-02-09
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 3
[patent_no_of_words] => 4060
[patent_no_of_claims] => 20
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 165
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 15018893
[rel_patent_id] =>[rel_patent_doc_number] =>) 15/018893 | Reverse thrust engine | Feb 8, 2016 | Issued |
Array
(
[id] => 11055055
[patent_doc_number] => 20160252017
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2016-09-01
[patent_title] => 'METHOD FOR CONTROLLING THE OPERATION OF A GAS TURBINE WITH SEQUENTIAL COMBUSTION'
[patent_app_type] => utility
[patent_app_number] => 15/006480
[patent_app_country] => US
[patent_app_date] => 2016-01-26
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 2
[patent_figures_cnt] => 2
[patent_no_of_words] => 2517
[patent_no_of_claims] => 14
[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] => 15006480
[rel_patent_id] =>[rel_patent_doc_number] =>) 15/006480 | METHOD FOR CONTROLLING THE OPERATION OF A GAS TURBINE WITH SEQUENTIAL COMBUSTION | Jan 25, 2016 | Abandoned |
Array
(
[id] => 14520413
[patent_doc_number] => 10337454
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2019-07-02
[patent_title] => Thrust reverser with asymmetric vane geometry
[patent_app_type] => utility
[patent_app_number] => 15/005357
[patent_app_country] => US
[patent_app_date] => 2016-01-25
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 11
[patent_figures_cnt] => 12
[patent_no_of_words] => 5595
[patent_no_of_claims] => 8
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 225
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 15005357
[rel_patent_id] =>[rel_patent_doc_number] =>) 15/005357 | Thrust reverser with asymmetric vane geometry | Jan 24, 2016 | Issued |
Array
(
[id] => 15009753
[patent_doc_number] => 10451002
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2019-10-22
[patent_title] => Translating cowl thrust reverser that prevents unintended door rotation
[patent_app_type] => utility
[patent_app_number] => 15/004020
[patent_app_country] => US
[patent_app_date] => 2016-01-22
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 6
[patent_figures_cnt] => 11
[patent_no_of_words] => 3999
[patent_no_of_claims] => 11
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 343
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 15004020
[rel_patent_id] =>[rel_patent_doc_number] =>) 15/004020 | Translating cowl thrust reverser that prevents unintended door rotation | Jan 21, 2016 | Issued |
Array
(
[id] => 16430366
[patent_doc_number] => 10830445
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2020-11-10
[patent_title] => Liquid fuel nozzles for dual fuel combustors
[patent_app_type] => utility
[patent_app_number] => 15/780496
[patent_app_country] => US
[patent_app_date] => 2015-12-30
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 5
[patent_no_of_words] => 2305
[patent_no_of_claims] => 20
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 186
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 15780496
[rel_patent_id] =>[rel_patent_doc_number] =>) 15/780496 | Liquid fuel nozzles for dual fuel combustors | Dec 29, 2015 | Issued |
Array
(
[id] => 11277601
[patent_doc_number] => 09494078
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2016-11-15
[patent_title] => 'Prime mover with recovered energy driven compression of the working fluid'
[patent_app_type] => utility
[patent_app_number] => 14/972166
[patent_app_country] => US
[patent_app_date] => 2015-12-17
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 7
[patent_figures_cnt] => 8
[patent_no_of_words] => 5665
[patent_no_of_claims] => 18
[patent_no_of_ind_claims] => 4
[patent_words_short_claim] => 251
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14972166
[rel_patent_id] =>[rel_patent_doc_number] =>) 14/972166 | Prime mover with recovered energy driven compression of the working fluid | Dec 16, 2015 | Issued |
Array
(
[id] => 10738019
[patent_doc_number] => 20160084169
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2016-03-24
[patent_title] => 'METHOD OF OPERATING A MULTI-STAGE FLAMESHEET COMBUSTOR'
[patent_app_type] => utility
[patent_app_number] => 14/956048
[patent_app_country] => US
[patent_app_date] => 2015-12-01
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 13
[patent_figures_cnt] => 13
[patent_no_of_words] => 9564
[patent_no_of_claims] => 25
[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] => 14956048
[rel_patent_id] =>[rel_patent_doc_number] =>) 14/956048 | Method of operating a multi-stage flamesheet combustor | Nov 30, 2015 | Issued |
Array
(
[id] => 14295719
[patent_doc_number] => 10287978
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2019-05-14
[patent_title] => Method of increasing the safety of a power plant, and a power plant suitable for implementing the method
[patent_app_type] => utility
[patent_app_number] => 14/931066
[patent_app_country] => US
[patent_app_date] => 2015-11-03
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 4
[patent_no_of_words] => 6630
[patent_no_of_claims] => 20
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 104
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14931066
[rel_patent_id] =>[rel_patent_doc_number] =>) 14/931066 | Method of increasing the safety of a power plant, and a power plant suitable for implementing the method | Nov 2, 2015 | Issued |
Array
(
[id] => 10777437
[patent_doc_number] => 20160123593
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2016-05-05
[patent_title] => 'CAN COMBUSTION CHAMBER'
[patent_app_type] => utility
[patent_app_number] => 14/928433
[patent_app_country] => US
[patent_app_date] => 2015-10-30
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 4
[patent_no_of_words] => 1235
[patent_no_of_claims] => 9
[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] => 14928433
[rel_patent_id] =>[rel_patent_doc_number] =>) 14/928433 | Can combustion chamber | Oct 29, 2015 | Issued |