Search

Marc J. Amar

Examiner (ID: 8940, Phone: (571)272-9948 , Office: P/3741 )

Most Active Art Unit
3741
Art Unit(s)
3741
Total Applications
475
Issued Applications
338
Pending Applications
60
Abandoned Applications
92

Applications

Application numberTitle of the applicationFiling DateStatus
Array ( [id] => 18743772 [patent_doc_number] => 20230352760 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2023-11-02 [patent_title] => ELECTRICAL HEATING SYSTEM FOR HYBRID POWERPLANT ELECTRICAL POWER SOURCE [patent_app_type] => utility [patent_app_number] => 17/733408 [patent_app_country] => US [patent_app_date] => 2022-04-29 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 0 [patent_figures_cnt] => 0 [patent_no_of_words] => 4071 [patent_no_of_claims] => 0 [patent_no_of_ind_claims] => -17 [patent_words_short_claim] => 39 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 17733408 [rel_patent_id] =>[rel_patent_doc_number] =>)
17/733408
ELECTRICAL HEATING SYSTEM FOR HYBRID POWERPLANT ELECTRICAL POWER SOURCE Apr 28, 2022 Pending
Array ( [id] => 17989908 [patent_doc_number] => 20220355945 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2022-11-10 [patent_title] => ASSEMBLY OF A PRIMARY STRUCTURE OF AN AIRCRAFT PYLON AND A REAR ENGINE ATTACHMENT COMPRISING AT LEAST ONE LATERAL FASTENING ELEMENT AND AIRCRAFT COMPRISING AT LEAST ONE SUCH ASSEMBLY [patent_app_type] => utility [patent_app_number] => 17/733065 [patent_app_country] => US [patent_app_date] => 2022-04-29 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 0 [patent_figures_cnt] => 0 [patent_no_of_words] => 5351 [patent_no_of_claims] => 0 [patent_no_of_ind_claims] => -8 [patent_words_short_claim] => 208 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 17733065 [rel_patent_id] =>[rel_patent_doc_number] =>)
17/733065
ASSEMBLY OF A PRIMARY STRUCTURE OF AN AIRCRAFT PYLON AND A REAR ENGINE ATTACHMENT COMPRISING AT LEAST ONE LATERAL FASTENING ELEMENT AND AIRCRAFT COMPRISING AT LEAST ONE SUCH ASSEMBLY Apr 28, 2022 Abandoned
Array ( [id] => 18122549 [patent_doc_number] => 20230008152 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2023-01-12 [patent_title] => METAL-BASED FUEL AND FUEL DELIVERY SYSTEMS [patent_app_type] => utility [patent_app_number] => 17/728510 [patent_app_country] => US [patent_app_date] => 2022-04-25 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 0 [patent_figures_cnt] => 0 [patent_no_of_words] => 6846 [patent_no_of_claims] => 0 [patent_no_of_ind_claims] => -17 [patent_words_short_claim] => 43 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 17728510 [rel_patent_id] =>[rel_patent_doc_number] =>)
17/728510
METAL-BASED FUEL AND FUEL DELIVERY SYSTEMS Apr 24, 2022 Pending
Array ( [id] => 17959713 [patent_doc_number] => 20220340293 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2022-10-27 [patent_title] => DEVICE FOR CONNECTING AN AIRCRAFT ENGINE AND A PRIMARY STRUCTURE OF AN AIRCRAFT PYLON COMPRISING A RUDDER AND A SYSTEM FOR LIMITING THE DISPLACEMENT OF THE RUDDER INCORPORATING A DOUBLE STOP, AIRCRAFT COMPRISING SUCH A DEVICE [patent_app_type] => utility [patent_app_number] => 17/725641 [patent_app_country] => US [patent_app_date] => 2022-04-21 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 0 [patent_figures_cnt] => 0 [patent_no_of_words] => 4270 [patent_no_of_claims] => 0 [patent_no_of_ind_claims] => -8 [patent_words_short_claim] => 401 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 17725641 [rel_patent_id] =>[rel_patent_doc_number] =>)
17/725641
Device for connecting an aircraft engine and a primary structure of an aircraft pylon comprising a rudder and a system for limiting the displacement of the rudder incorporating a double stop, aircraft comprising such a device Apr 20, 2022 Issued
Array ( [id] => 17930553 [patent_doc_number] => 20220325678 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2022-10-13 [patent_title] => LOBED MIXER NOZZLES FOR SUPERSONIC AND SUBSONIC AIRCRAFT, AND ASSOCIATED SYSTEMS AND METHODS [patent_app_type] => utility [patent_app_number] => 17/715450 [patent_app_country] => US [patent_app_date] => 2022-04-07 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 0 [patent_figures_cnt] => 0 [patent_no_of_words] => 5750 [patent_no_of_claims] => 0 [patent_no_of_ind_claims] => -24 [patent_words_short_claim] => 105 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 17715450 [rel_patent_id] =>[rel_patent_doc_number] =>)
17/715450
LOBED MIXER NOZZLES FOR SUPERSONIC AND SUBSONIC AIRCRAFT, AND ASSOCIATED SYSTEMS AND METHODS Apr 6, 2022 Abandoned
Array ( [id] => 17735443 [patent_doc_number] => 20220220902 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2022-07-14 [patent_title] => AIRCRAFT BLEED AIR SYSTEMS AND METHODS [patent_app_type] => utility [patent_app_number] => 17/711445 [patent_app_country] => US [patent_app_date] => 2022-04-01 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 0 [patent_figures_cnt] => 0 [patent_no_of_words] => 8112 [patent_no_of_claims] => 0 [patent_no_of_ind_claims] => -10 [patent_words_short_claim] => 241 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 17711445 [rel_patent_id] =>[rel_patent_doc_number] =>)
17/711445
AIRCRAFT BLEED AIR SYSTEMS AND METHODS Mar 31, 2022 Abandoned
Array ( [id] => 18605272 [patent_doc_number] => 11746728 [patent_country] => US [patent_kind] => B1 [patent_issue_date] => 2023-09-05 [patent_title] => Propulsion system with grooved inert rods for reactive wire [patent_app_type] => utility [patent_app_number] => 17/709700 [patent_app_country] => US [patent_app_date] => 2022-03-31 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 5 [patent_figures_cnt] => 11 [patent_no_of_words] => 2687 [patent_no_of_claims] => 19 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 54 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 17709700 [rel_patent_id] =>[rel_patent_doc_number] =>)
17/709700
Propulsion system with grooved inert rods for reactive wire Mar 30, 2022 Issued
Array ( [id] => 17946764 [patent_doc_number] => 20220333783 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2022-10-20 [patent_title] => Hydrogen-Fueled Combustor for Gas Turbines [patent_app_type] => utility [patent_app_number] => 17/688503 [patent_app_country] => US [patent_app_date] => 2022-03-07 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 0 [patent_figures_cnt] => 0 [patent_no_of_words] => 4454 [patent_no_of_claims] => 0 [patent_no_of_ind_claims] => -16 [patent_words_short_claim] => 31 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 17688503 [rel_patent_id] =>[rel_patent_doc_number] =>)
17/688503
Hydrogen-Fueled Combustor for Gas Turbines Mar 6, 2022 Abandoned
Array ( [id] => 18478715 [patent_doc_number] => 11692448 [patent_country] => US [patent_kind] => B1 [patent_issue_date] => 2023-07-04 [patent_title] => Passive valve assembly for a nozzle of a gas turbine engine [patent_app_type] => utility [patent_app_number] => 17/686871 [patent_app_country] => US [patent_app_date] => 2022-03-04 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 18 [patent_figures_cnt] => 30 [patent_no_of_words] => 13091 [patent_no_of_claims] => 20 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 95 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 17686871 [rel_patent_id] =>[rel_patent_doc_number] =>)
17/686871
Passive valve assembly for a nozzle of a gas turbine engine Mar 3, 2022 Issued
Array ( [id] => 18350365 [patent_doc_number] => 20230138476 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2023-05-04 [patent_title] => HYBRID ELECTRIC SINGLE ENGINE DESCENT RESTART [patent_app_type] => utility [patent_app_number] => 17/586326 [patent_app_country] => US [patent_app_date] => 2022-01-27 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 0 [patent_figures_cnt] => 0 [patent_no_of_words] => 6971 [patent_no_of_claims] => 0 [patent_no_of_ind_claims] => -8 [patent_words_short_claim] => 2 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 17586326 [rel_patent_id] =>[rel_patent_doc_number] =>)
17/586326
HYBRID ELECTRIC SINGLE ENGINE DESCENT RESTART Jan 26, 2022 Pending
Array ( [id] => 17688670 [patent_doc_number] => 20220195962 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2022-06-23 [patent_title] => SYSTEMS AND METHODS FOR EXPANDING AN OPERATING SPEED RANGE OF A HIGH SPEED FLIGHT VEHICLE [patent_app_type] => utility [patent_app_number] => 17/539719 [patent_app_country] => US [patent_app_date] => 2021-12-01 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 0 [patent_figures_cnt] => 0 [patent_no_of_words] => 7302 [patent_no_of_claims] => 0 [patent_no_of_ind_claims] => -17 [patent_words_short_claim] => 115 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 17539719 [rel_patent_id] =>[rel_patent_doc_number] =>)
17/539719
SYSTEMS AND METHODS FOR EXPANDING AN OPERATING SPEED RANGE OF A HIGH SPEED FLIGHT VEHICLE Nov 30, 2021 Abandoned
Array ( [id] => 18406432 [patent_doc_number] => 20230167783 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2023-06-01 [patent_title] => PROPULSION SYSTEM FOR A GAS TURBINE ENGINE [patent_app_type] => utility [patent_app_number] => 17/539401 [patent_app_country] => US [patent_app_date] => 2021-12-01 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 0 [patent_figures_cnt] => 0 [patent_no_of_words] => 7915 [patent_no_of_claims] => 0 [patent_no_of_ind_claims] => -15 [patent_words_short_claim] => 2 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 17539401 [rel_patent_id] =>[rel_patent_doc_number] =>)
17/539401
PROPULSION SYSTEM FOR A GAS TURBINE ENGINE Nov 30, 2021 Abandoned
Array ( [id] => 18665934 [patent_doc_number] => 11772809 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2023-10-03 [patent_title] => Fuselage for an aircraft with fuselage-integrated tailplane [patent_app_type] => utility [patent_app_number] => 17/535995 [patent_app_country] => US [patent_app_date] => 2021-11-27 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 6 [patent_figures_cnt] => 11 [patent_no_of_words] => 6057 [patent_no_of_claims] => 9 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 397 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 17535995 [rel_patent_id] =>[rel_patent_doc_number] =>)
17/535995
Fuselage for an aircraft with fuselage-integrated tailplane Nov 26, 2021 Issued
Array ( [id] => 17735441 [patent_doc_number] => 20220220900 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2022-07-14 [patent_title] => Automated Initiation of Starter Motor Operation for Starting an Aircraft Engine [patent_app_type] => utility [patent_app_number] => 17/533009 [patent_app_country] => US [patent_app_date] => 2021-11-22 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 0 [patent_figures_cnt] => 0 [patent_no_of_words] => 7010 [patent_no_of_claims] => 0 [patent_no_of_ind_claims] => -24 [patent_words_short_claim] => 62 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 17533009 [rel_patent_id] =>[rel_patent_doc_number] =>)
17/533009
Automated Initiation of Starter Motor Operation for Starting an Aircraft Engine Nov 21, 2021 Abandoned
Array ( [id] => 18102982 [patent_doc_number] => 11542863 [patent_country] => US [patent_kind] => B1 [patent_issue_date] => 2023-01-03 [patent_title] => Method and device to improve the performance of a power plant integrated with a thermal energy storage system [patent_app_type] => utility [patent_app_number] => 17/455099 [patent_app_country] => US [patent_app_date] => 2021-11-16 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 7 [patent_figures_cnt] => 7 [patent_no_of_words] => 2443 [patent_no_of_claims] => 16 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 187 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 17455099 [rel_patent_id] =>[rel_patent_doc_number] =>)
17/455099
Method and device to improve the performance of a power plant integrated with a thermal energy storage system Nov 15, 2021 Issued
Array ( [id] => 18375601 [patent_doc_number] => 20230150681 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2023-05-18 [patent_title] => GAS TURBINE ENGINE NOISE REDUCTION [patent_app_type] => utility [patent_app_number] => 17/526383 [patent_app_country] => US [patent_app_date] => 2021-11-15 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 0 [patent_figures_cnt] => 0 [patent_no_of_words] => 10728 [patent_no_of_claims] => 0 [patent_no_of_ind_claims] => -17 [patent_words_short_claim] => 95 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 17526383 [rel_patent_id] =>[rel_patent_doc_number] =>)
17/526383
GAS TURBINE ENGINE NOISE REDUCTION Nov 14, 2021 Pending
Array ( [id] => 18972919 [patent_doc_number] => 20240053011 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2024-02-15 [patent_title] => GUIDING ARRAY [patent_app_type] => utility [patent_app_number] => 18/035803 [patent_app_country] => US [patent_app_date] => 2021-11-09 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 0 [patent_figures_cnt] => 0 [patent_no_of_words] => 6733 [patent_no_of_claims] => 0 [patent_no_of_ind_claims] => -26 [patent_words_short_claim] => 2 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 18035803 [rel_patent_id] =>[rel_patent_doc_number] =>)
18/035803
GUIDING ARRAY Nov 8, 2021 Abandoned
Array ( [id] => 18845409 [patent_doc_number] => 20230407813 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2023-12-21 [patent_title] => ASSEMBLY FOR A TURBOMACHINE [patent_app_type] => utility [patent_app_number] => 18/251860 [patent_app_country] => US [patent_app_date] => 2021-11-03 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 0 [patent_figures_cnt] => 0 [patent_no_of_words] => 3053 [patent_no_of_claims] => 0 [patent_no_of_ind_claims] => -11 [patent_words_short_claim] => 120 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 18251860 [rel_patent_id] =>[rel_patent_doc_number] =>)
18/251860
ASSEMBLY FOR A TURBOMACHINE Nov 2, 2021 Pending
Array ( [id] => 17562861 [patent_doc_number] => 20220127010 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2022-04-28 [patent_title] => BRACED-PYLON ARCHITECTURE FOR MOUNTING AN ENGINE TO AN AIRCRAFT [patent_app_type] => utility [patent_app_number] => 17/509113 [patent_app_country] => US [patent_app_date] => 2021-10-25 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 0 [patent_figures_cnt] => 0 [patent_no_of_words] => 3886 [patent_no_of_claims] => 0 [patent_no_of_ind_claims] => -8 [patent_words_short_claim] => 218 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 17509113 [rel_patent_id] =>[rel_patent_doc_number] =>)
17/509113
Braced-pylon architecture for mounting an engine to an aircraft Oct 24, 2021 Issued
Array ( [id] => 18845348 [patent_doc_number] => 20230407752 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2023-12-21 [patent_title] => GAS TURBINE STATIONARY BLADE AND GAS TURBINE [patent_app_type] => utility [patent_app_number] => 18/036058 [patent_app_country] => US [patent_app_date] => 2021-10-15 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 0 [patent_figures_cnt] => 0 [patent_no_of_words] => 24225 [patent_no_of_claims] => 0 [patent_no_of_ind_claims] => -13 [patent_words_short_claim] => 396 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 18036058 [rel_patent_id] =>[rel_patent_doc_number] =>)
18/036058
Gas turbine stationary blade and gas turbine Oct 14, 2021 Issued
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