
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] => 19150962
[patent_doc_number] => 11975857
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[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
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Array
(
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[patent_issue_date] => 2023-08-22
[patent_title] => Controlling soot
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Array
(
[id] => 18709916
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[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
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[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
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[patent_kind] => A1
[patent_issue_date] => 2024-01-04
[patent_title] => IN-FLIGHT ENGINE RE-START
[patent_app_type] => utility
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[patent_app_country] => US
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Array
(
[id] => 19180789
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[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
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[patent_app_number] => 17/849882
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Array
(
[id] => 18461259
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[patent_title] => Turbo engine with cooler for cooling inlet air and turbine for expanding cryogenic fuel
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Array
(
[id] => 18225183
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[patent_title] => TWIN-ENGINE SYSTEM WITH ELECTRIC DRIVE
[patent_app_type] => utility
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[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
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[patent_issue_date] => 2024-01-02
[patent_title] => Adjustable support links for aircraft
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[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
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[patent_issue_date] => 2025-03-25
[patent_title] => Assembly for supporting an accessory gearbox of an aircraft turbine engine
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Array
(
[id] => 19346043
[patent_doc_number] => 20240255006
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[patent_issue_date] => 2024-08-01
[patent_title] => DEVICE FOR GUIDING A MAIN AIR FLOW FOR AN AIRCRAFT TURBINE ENGINE
[patent_app_type] => utility
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Array
(
[id] => 17989908
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[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
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Array
(
[id] => 18743772
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Array
(
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Array
(
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[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
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Array
(
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Array
(
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Array
(
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Array
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Array
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Array
(
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