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
(
[id] => 13371157
[patent_doc_number] => 20180237119
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2018-08-23
[patent_title] => Adhesive Joints for Aircraft
[patent_app_type] => utility
[patent_app_number] => 15/437198
[patent_app_country] => US
[patent_app_date] => 2017-02-20
[patent_effective_date] => 0000-00-00
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[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 15437198
[rel_patent_id] =>[rel_patent_doc_number] =>) 15/437198 | Adhesive joints for aircraft | Feb 19, 2017 | Issued |
Array
(
[id] => 14977261
[patent_doc_number] => 10442524
[patent_country] => US
[patent_kind] => B1
[patent_issue_date] => 2019-10-15
[patent_title] => Wind energy kite tail
[patent_app_type] => utility
[patent_app_number] => 15/435471
[patent_app_country] => US
[patent_app_date] => 2017-02-17
[patent_effective_date] => 0000-00-00
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[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 15435471
[rel_patent_id] =>[rel_patent_doc_number] =>) 15/435471 | Wind energy kite tail | Feb 16, 2017 | Issued |
Array
(
[id] => 15948033
[patent_doc_number] => 10661903
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2020-05-26
[patent_title] => Aircraft passenger suite seating arrangements with all aisle access
[patent_app_type] => utility
[patent_app_number] => 15/436482
[patent_app_country] => US
[patent_app_date] => 2017-02-17
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 44
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[rel_patent_id] =>[rel_patent_doc_number] =>) 15/436482 | Aircraft passenger suite seating arrangements with all aisle access | Feb 16, 2017 | Issued |
Array
(
[id] => 11949171
[patent_doc_number] => 20170253323
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2017-09-07
[patent_title] => 'AIRCRAFT LANDING GEAR ASSEMBLY'
[patent_app_type] => utility
[patent_app_number] => 15/434295
[patent_app_country] => US
[patent_app_date] => 2017-02-16
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 6
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[rel_patent_id] =>[rel_patent_doc_number] =>) 15/434295 | Aircraft landing gear assembly | Feb 15, 2017 | Issued |
Array
(
[id] => 11835853
[patent_doc_number] => 20170217572
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2017-08-03
[patent_title] => 'METHOD FOR USING AIRCRAFT WHEEL TYRE PRESSURE TO IMPROVE AIRCRAFT ENERGY EFFICIENCY AND DRIVE SYSTEM PERFORMANCE'
[patent_app_type] => utility
[patent_app_number] => 15/433900
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[patent_app_date] => 2017-02-15
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[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 15433900
[rel_patent_id] =>[rel_patent_doc_number] =>) 15/433900 | Method for using aircraft wheel tyre pressure to improve aircraft energy efficiency and drive system performance | Feb 14, 2017 | Issued |
Array
(
[id] => 11865780
[patent_doc_number] => 20170233065
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2017-08-17
[patent_title] => 'CURVED WINGTIP FOR AIRCRAFT'
[patent_app_type] => utility
[patent_app_number] => 15/430661
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[rel_patent_id] =>[rel_patent_doc_number] =>) 15/430661 | Curved wingtip for aircraft | Feb 12, 2017 | Issued |
Array
(
[id] => 16429140
[patent_doc_number] => 10829206
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2020-11-10
[patent_title] => Wing leading edge features to attenuate propeller wake-wing acoustic interactions
[patent_app_type] => utility
[patent_app_number] => 15/429829
[patent_app_country] => US
[patent_app_date] => 2017-02-10
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[rel_patent_id] =>[rel_patent_doc_number] =>) 15/429829 | Wing leading edge features to attenuate propeller wake-wing acoustic interactions | Feb 9, 2017 | Issued |
Array
(
[id] => 12120643
[patent_doc_number] => 20180004229
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2018-01-04
[patent_title] => 'ROTOR MOMENT CONTROL SYSTEM FOR A ROTARY WING AIRCRAFT'
[patent_app_type] => utility
[patent_app_number] => 15/425634
[patent_app_country] => US
[patent_app_date] => 2017-02-06
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[rel_patent_id] =>[rel_patent_doc_number] =>) 15/425634 | Rotor moment control system for a rotary wing aircraft | Feb 5, 2017 | Issued |
Array
(
[id] => 11865799
[patent_doc_number] => 20170233084
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2017-08-17
[patent_title] => 'ANTI-ICING SYSTEM AND AIRCRAFT'
[patent_app_type] => utility
[patent_app_number] => 15/420465
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[rel_patent_id] =>[rel_patent_doc_number] =>) 15/420465 | Anti-icing system and aircraft | Jan 30, 2017 | Issued |
Array
(
[id] => 18117274
[patent_doc_number] => 11548650
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2023-01-10
[patent_title] => Hybrid airship
[patent_app_type] => utility
[patent_app_number] => 15/530528
[patent_app_country] => US
[patent_app_date] => 2017-01-25
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[rel_patent_id] =>[rel_patent_doc_number] =>) 15/530528 | Hybrid airship | Jan 24, 2017 | Issued |
Array
(
[id] => 13313521
[patent_doc_number] => 20180208297
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2018-07-26
[patent_title] => NACELLE FOR AN AIRCRAFT AFT FAN
[patent_app_type] => utility
[patent_app_number] => 15/411228
[patent_app_country] => US
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[rel_patent_id] =>[rel_patent_doc_number] =>) 15/411228 | NACELLE FOR AN AIRCRAFT AFT FAN | Jan 19, 2017 | Abandoned |
Array
(
[id] => 17222386
[patent_doc_number] => 11174878
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2021-11-16
[patent_title] => Aspirator system
[patent_app_type] => utility
[patent_app_number] => 15/405797
[patent_app_country] => US
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[rel_patent_id] =>[rel_patent_doc_number] =>) 15/405797 | Aspirator system | Jan 12, 2017 | Issued |
Array
(
[id] => 11865770
[patent_doc_number] => 20170233054
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2017-08-17
[patent_title] => 'HIGH ALTITUDE BALLOON SYSTEMS AND METHODS'
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[patent_app_number] => 15/401447
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[rel_patent_id] =>[rel_patent_doc_number] =>) 15/401447 | High altitude balloon systems and methods using continuous multi-compartment super pressure balloon | Jan 8, 2017 | Issued |
Array
(
[id] => 11821539
[patent_doc_number] => 20170210476
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[patent_title] => 'ANTI-ICING SYSTEM AND AIRCRAFT'
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[rel_patent_id] =>[rel_patent_doc_number] =>) 15/390799 | Anti-icing system and aircraft | Dec 26, 2016 | Issued |
Array
(
[id] => 11568356
[patent_doc_number] => 20170107000
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2017-04-20
[patent_title] => 'AIRPORT CAPACITY FROM TAKEOFF ASSIST'
[patent_app_type] => utility
[patent_app_number] => 15/390414
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[rel_patent_id] =>[rel_patent_doc_number] =>) 15/390414 | Airport capacity from takeoff assist | Dec 22, 2016 | Issued |
Array
(
[id] => 11705858
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[patent_title] => 'Aircraft With A Bleed Supply Hybrid Architecture'
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[rel_patent_id] =>[rel_patent_doc_number] =>) 15/379782 | Aircraft With A Bleed Supply Hybrid Architecture | Dec 14, 2016 | Abandoned |
Array
(
[id] => 11669596
[patent_doc_number] => 20170158316
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[patent_title] => 'FULLY ELECTRIC SPEED-PROPORTIONAL NOSE WHEEL STEERING SYSTEM FOR AN AIRCRAFT'
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[rel_patent_id] =>[rel_patent_doc_number] =>) 15/371566 | FULLY ELECTRIC SPEED-PROPORTIONAL NOSE WHEEL STEERING SYSTEM FOR AN AIRCRAFT | Dec 6, 2016 | Abandoned |
Array
(
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[patent_doc_number] => 10358217
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[patent_issue_date] => 2019-07-23
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Array
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Array
(
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