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] => 19150962 [patent_doc_number] => 11975857 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2024-05-07 [patent_title] => Front engine attachment system for an aircraft engine, which has a compact structure [patent_app_type] => utility [patent_app_number] => 17/899673 [patent_app_country] => US [patent_app_date] => 2022-08-31 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 5 [patent_figures_cnt] => 6 [patent_no_of_words] => 2304 [patent_no_of_claims] => 4 [patent_no_of_ind_claims] => 1 [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] => 17899673 [rel_patent_id] =>[rel_patent_doc_number] =>)
17/899673
Front engine attachment system for an aircraft engine, which has a compact structure Aug 30, 2022 Issued
Array ( [id] => 18576141 [patent_doc_number] => 11732659 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2023-08-22 [patent_title] => Controlling soot [patent_app_type] => utility [patent_app_number] => 17/896467 [patent_app_country] => US [patent_app_date] => 2022-08-26 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 14 [patent_figures_cnt] => 20 [patent_no_of_words] => 10718 [patent_no_of_claims] => 19 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 139 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 17896467 [rel_patent_id] =>[rel_patent_doc_number] =>)
17/896467
Controlling soot Aug 25, 2022 Issued
Array ( [id] => 18709916 [patent_doc_number] => 20230332538 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2023-10-19 [patent_title] => COMBUSTION SYSTEM, PARTICLE SEPARATOR AND FEED SYSTEM FOR COMBINED HEAT AND POWER SYSTEM [patent_app_type] => utility [patent_app_number] => 17/886869 [patent_app_country] => US [patent_app_date] => 2022-08-12 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 0 [patent_figures_cnt] => 0 [patent_no_of_words] => 11892 [patent_no_of_claims] => 0 [patent_no_of_ind_claims] => -11 [patent_words_short_claim] => 68 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 17886869 [rel_patent_id] =>[rel_patent_doc_number] =>)
17/886869
COMBUSTION SYSTEM, PARTICLE SEPARATOR AND FEED SYSTEM FOR COMBINED HEAT AND POWER SYSTEM Aug 11, 2022 Pending
Array ( [id] => 18879931 [patent_doc_number] => 20240003300 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2024-01-04 [patent_title] => IN-FLIGHT ENGINE RE-START [patent_app_type] => utility [patent_app_number] => 17/856550 [patent_app_country] => US [patent_app_date] => 2022-07-01 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 0 [patent_figures_cnt] => 0 [patent_no_of_words] => 4826 [patent_no_of_claims] => 0 [patent_no_of_ind_claims] => -17 [patent_words_short_claim] => 87 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 17856550 [rel_patent_id] =>[rel_patent_doc_number] =>)
17/856550
In-flight engine re-start Jun 30, 2022 Issued
Array ( [id] => 19180789 [patent_doc_number] => 11987370 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2024-05-21 [patent_title] => Aircraft propulsion assembly comprising a front engine mount which comprises a transverse beam which is partially positioned opposite a front transverse reinforcement of a primary structure of a strut [patent_app_type] => utility [patent_app_number] => 17/849882 [patent_app_country] => US [patent_app_date] => 2022-06-27 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 3 [patent_figures_cnt] => 10 [patent_no_of_words] => 3839 [patent_no_of_claims] => 9 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 356 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 17849882 [rel_patent_id] =>[rel_patent_doc_number] =>)
17/849882
Aircraft propulsion assembly comprising a front engine mount which comprises a transverse beam which is partially positioned opposite a front transverse reinforcement of a primary structure of a strut Jun 26, 2022 Issued
Array ( [id] => 18461259 [patent_doc_number] => 11685541 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2023-06-27 [patent_title] => Turbo engine with cooler for cooling inlet air and turbine for expanding cryogenic fuel [patent_app_type] => utility [patent_app_number] => 17/837100 [patent_app_country] => US [patent_app_date] => 2022-06-10 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 5 [patent_figures_cnt] => 5 [patent_no_of_words] => 1977 [patent_no_of_claims] => 15 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 153 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 17837100 [rel_patent_id] =>[rel_patent_doc_number] =>)
17/837100
Turbo engine with cooler for cooling inlet air and turbine for expanding cryogenic fuel Jun 9, 2022 Issued
Array ( [id] => 18225183 [patent_doc_number] => 20230064177 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2023-03-02 [patent_title] => TWIN-ENGINE SYSTEM WITH ELECTRIC DRIVE [patent_app_type] => utility [patent_app_number] => 17/804631 [patent_app_country] => US [patent_app_date] => 2022-05-31 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 0 [patent_figures_cnt] => 0 [patent_no_of_words] => 6519 [patent_no_of_claims] => 0 [patent_no_of_ind_claims] => -9 [patent_words_short_claim] => 94 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 17804631 [rel_patent_id] =>[rel_patent_doc_number] =>)
17/804631
Twin-engine system with electric drive May 30, 2022 Issued
Array ( [id] => 18870860 [patent_doc_number] => 11858645 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2024-01-02 [patent_title] => Adjustable support links for aircraft [patent_app_type] => utility [patent_app_number] => 17/752450 [patent_app_country] => US [patent_app_date] => 2022-05-24 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 7 [patent_figures_cnt] => 8 [patent_no_of_words] => 7160 [patent_no_of_claims] => 20 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 237 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 17752450 [rel_patent_id] =>[rel_patent_doc_number] =>)
17/752450
Adjustable support links for aircraft May 23, 2022 Issued
Array ( [id] => 19855318 [patent_doc_number] => 12258137 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2025-03-25 [patent_title] => Assembly for supporting an accessory gearbox of an aircraft turbine engine [patent_app_type] => utility [patent_app_number] => 18/563040 [patent_app_country] => US [patent_app_date] => 2022-05-20 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 8 [patent_figures_cnt] => 15 [patent_no_of_words] => 7240 [patent_no_of_claims] => 16 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 173 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 18563040 [rel_patent_id] =>[rel_patent_doc_number] =>)
18/563040
Assembly for supporting an accessory gearbox of an aircraft turbine engine May 19, 2022 Issued
Array ( [id] => 19346043 [patent_doc_number] => 20240255006 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2024-08-01 [patent_title] => DEVICE FOR GUIDING A MAIN AIR FLOW FOR AN AIRCRAFT TURBINE ENGINE [patent_app_type] => utility [patent_app_number] => 18/560598 [patent_app_country] => US [patent_app_date] => 2022-05-10 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 0 [patent_figures_cnt] => 0 [patent_no_of_words] => 3166 [patent_no_of_claims] => 0 [patent_no_of_ind_claims] => -12 [patent_words_short_claim] => 172 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 18560598 [rel_patent_id] =>[rel_patent_doc_number] =>)
18/560598
Device for guiding a main air flow for an aircraft turbine engine May 9, 2022 Issued
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] => 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] => 20818947 [patent_doc_number] => 12674412 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2026-07-07 [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] => 5 [patent_figures_cnt] => 5 [patent_no_of_words] => 1105 [patent_no_of_claims] => 7 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 425 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [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 Issued
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] => 19247011 [patent_doc_number] => 20240197995 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2024-06-20 [patent_title] => A COMPONENT AND A SUB-ASSEMBLY FOR A MEDICAMENT DELIVERY DEVICE [patent_app_type] => utility [patent_app_number] => 18/553605 [patent_app_country] => US [patent_app_date] => 2022-04-19 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 0 [patent_figures_cnt] => 0 [patent_no_of_words] => 8473 [patent_no_of_claims] => 0 [patent_no_of_ind_claims] => -12 [patent_words_short_claim] => 102 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 18553605 [rel_patent_id] =>[rel_patent_doc_number] =>)
18/553605
A COMPONENT AND A SUB-ASSEMBLY FOR A MEDICAMENT DELIVERY DEVICE Apr 18, 2022 Pending
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] => 19462612 [patent_doc_number] => 20240316281 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2024-09-26 [patent_title] => A PREFILLED SYRINGE CONTAINING A STERILE ULTRACONCENTRATED HYDROGEL [patent_app_type] => utility [patent_app_number] => 18/554197 [patent_app_country] => US [patent_app_date] => 2022-03-31 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 0 [patent_figures_cnt] => 0 [patent_no_of_words] => 11600 [patent_no_of_claims] => 0 [patent_no_of_ind_claims] => -19 [patent_words_short_claim] => 89 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 18554197 [rel_patent_id] =>[rel_patent_doc_number] =>)
18/554197
A PREFILLED SYRINGE CONTAINING A STERILE ULTRACONCENTRATED HYDROGEL Mar 30, 2022 Pending
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] => 19201627 [patent_doc_number] => 20240173526 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2024-05-30 [patent_title] => VENOUS CANNULAS WITH INFLATABLE BALLOONS [patent_app_type] => utility [patent_app_number] => 18/553197 [patent_app_country] => US [patent_app_date] => 2022-03-29 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 0 [patent_figures_cnt] => 0 [patent_no_of_words] => 10058 [patent_no_of_claims] => 0 [patent_no_of_ind_claims] => -18 [patent_words_short_claim] => 73 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 18553197 [rel_patent_id] =>[rel_patent_doc_number] =>)
18/553197
VENOUS CANNULAS WITH INFLATABLE BALLOONS Mar 28, 2022 Pending
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