Frederick Lyndon Lagman
Examiner (ID: 14185, Phone: (571)272-7043 , Office: P/3678 )
Most Active Art Unit | 3678 |
Art Unit(s) | 3678, 3672, 3501, 3625, 3673, 3506 |
Total Applications | 3144 |
Issued Applications | 2523 |
Pending Applications | 198 |
Abandoned Applications | 421 |
Applications
Application number | Title of the application | Filing Date | Status |
---|---|---|---|
Array
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[id] => 16664784
[patent_doc_number] => 10934013
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[patent_issue_date] => 2021-03-02
[patent_title] => Aircraft fuselage apparatus having embedded structural batteries
[patent_app_type] => utility
[patent_app_number] => 15/712618
[patent_app_country] => US
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Array
(
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[patent_issue_date] => 2021-05-25
[patent_title] => Airframe
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Array
(
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[patent_issue_date] => 2018-03-22
[patent_title] => 'Automated Recovery System for Unmanned Aircraft'
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Array
(
[id] => 14071565
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[patent_issue_date] => 2019-03-21
[patent_title] => UNMANNED AERIAL VEHICLE-MOUNTED APPARATUS
[patent_app_type] => utility
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Array
(
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[patent_issue_date] => 2018-03-29
[patent_title] => Non-Pressurized Accessory Gearbox
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Array
(
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[patent_issue_date] => 2018-03-29
[patent_title] => High Speed Engine Reduction Gearboxes
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Array
(
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[patent_title] => TRANSLATABLE SCOOP FOR AUXILIARY POWER UNITS AIR INTAKE
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Array
(
[id] => 14071593
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Array
(
[id] => 14071601
[patent_doc_number] => 20190084688
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2019-03-21
[patent_title] => ROTORCRAFT ENGINE INLET CONFIGURATION TO OPTIMIZE PERFORMANCE IN BOTH HOVER AND HIGH SPEED FLIGHT
[patent_app_type] => utility
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[rel_patent_id] =>[rel_patent_doc_number] =>) 15/710622 | Rotorcraft engine inlet configuration to optimize performance in both hover and high speed flight | Sep 19, 2017 | Issued |
Array
(
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[patent_title] => Aircraft self-rescue system
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Array
(
[id] => 13050943
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[patent_title] => Landing gear noise abatement devices
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Array
(
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[patent_doc_number] => 20190241282
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[patent_issue_date] => 2019-08-08
[patent_title] => DUCTED FAN UNMANNED AERIAL VEHICLE DOCKING STATION
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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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[rel_patent_id] =>[rel_patent_doc_number] =>) 15/609502 | SIMPLE PITCH CONTROL DEVICE FOR DUAL-MODE AIRCRAFT WITH VTOL AND FIXED-WING FLIGHT | May 30, 2017 | Abandoned |