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] => 11669607
[patent_doc_number] => 20170158327
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2017-06-08
[patent_title] => 'UAV WITH WING-PLATE ASSEMBLIES PROVIDING EFFICIENT VERTICAL TAKEOFF AND LANDING CAPABILITY'
[patent_app_type] => utility
[patent_app_number] => 15/370592
[patent_app_country] => US
[patent_app_date] => 2016-12-06
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 8
[patent_figures_cnt] => 8
[patent_no_of_words] => 4304
[patent_no_of_claims] => 21
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[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 15370592
[rel_patent_id] =>[rel_patent_doc_number] =>) 15/370592 | UAV with wing-plate assemblies providing efficient vertical takeoff and landing capability | Dec 5, 2016 | Issued |
Array
(
[id] => 15726133
[patent_doc_number] => 10611486
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2020-04-07
[patent_title] => Airflow diverter for aircraft and method of use
[patent_app_type] => utility
[patent_app_number] => 15/369837
[patent_app_country] => US
[patent_app_date] => 2016-12-05
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 11
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[patent_no_of_words] => 3222
[patent_no_of_claims] => 9
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[patent_maintenance] => 1
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[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 15369837
[rel_patent_id] =>[rel_patent_doc_number] =>) 15/369837 | Airflow diverter for aircraft and method of use | Dec 4, 2016 | Issued |
Array
(
[id] => 12050875
[patent_doc_number] => 20170327219
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2017-11-16
[patent_title] => 'VERTICAL TAKE-OFF AND LANDING AIRCRAFT WITH HYBRID POWER AND METHOD'
[patent_app_type] => utility
[patent_app_number] => 15/369270
[patent_app_country] => US
[patent_app_date] => 2016-12-05
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 7
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[patent_no_of_words] => 4551
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[rel_patent_id] =>[rel_patent_doc_number] =>) 15/369270 | VERTICAL TAKE-OFF AND LANDING AIRCRAFT WITH HYBRID POWER AND METHOD | Dec 4, 2016 | Abandoned |
Array
(
[id] => 12789502
[patent_doc_number] => 20180155003
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2018-06-07
[patent_title] => Adjustable Hinge
[patent_app_type] => utility
[patent_app_number] => 15/368650
[patent_app_country] => US
[patent_app_date] => 2016-12-04
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 0
[patent_figures_cnt] => 0
[patent_no_of_words] => 2887
[patent_no_of_claims] => 0
[patent_no_of_ind_claims] => -17
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[patent_current_assignee] =>[type] => publication
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 15368650
[rel_patent_id] =>[rel_patent_doc_number] =>) 15/368650 | Adjustable hinge | Dec 3, 2016 | Issued |
Array
(
[id] => 16042477
[patent_doc_number] => 10683095
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2020-06-16
[patent_title] => Collapsible aspirator barrel
[patent_app_type] => utility
[patent_app_number] => 15/368172
[patent_app_country] => US
[patent_app_date] => 2016-12-02
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 6
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[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 15368172
[rel_patent_id] =>[rel_patent_doc_number] =>) 15/368172 | Collapsible aspirator barrel | Dec 1, 2016 | Issued |
Array
(
[id] => 12789607
[patent_doc_number] => 20180155038
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2018-06-07
[patent_title] => Aircraft Parachute System
[patent_app_type] => utility
[patent_app_number] => 15/368108
[patent_app_country] => US
[patent_app_date] => 2016-12-02
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 0
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[patent_no_of_ind_claims] => -9
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[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 15368108
[rel_patent_id] =>[rel_patent_doc_number] =>) 15/368108 | Aircraft Parachute System | Dec 1, 2016 | Abandoned |
Array
(
[id] => 11492353
[patent_doc_number] => 20170066538
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2017-03-09
[patent_title] => 'WATER-INFLOW PREVENTION DEVICE OF AIRCRAFT, AIR PRESSURE REGULATING VALVE FOR AIRCRAFT, AND AIRCRAFT'
[patent_app_type] => utility
[patent_app_number] => 15/357131
[patent_app_country] => US
[patent_app_date] => 2016-11-21
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 11
[patent_figures_cnt] => 11
[patent_no_of_words] => 7136
[patent_no_of_claims] => 6
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[patent_current_assignee] =>[type] => publication
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 15357131
[rel_patent_id] =>[rel_patent_doc_number] =>) 15/357131 | Water-inflow prevention device of aircraft, air pressure regulating valve for aircraft, and aircraft | Nov 20, 2016 | Issued |
Array
(
[id] => 11705856
[patent_doc_number] => 20170174355
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2017-06-22
[patent_title] => 'TAIL ROTOR DRIVE SYSTEMS'
[patent_app_type] => utility
[patent_app_number] => 15/355773
[patent_app_country] => US
[patent_app_date] => 2016-11-18
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 11
[patent_figures_cnt] => 11
[patent_no_of_words] => 5700
[patent_no_of_claims] => 20
[patent_no_of_ind_claims] => 4
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[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 15355773
[rel_patent_id] =>[rel_patent_doc_number] =>) 15/355773 | TAIL ROTOR DRIVE SYSTEMS | Nov 17, 2016 | Abandoned |
Array
(
[id] => 16230222
[patent_doc_number] => 10737758
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2020-08-11
[patent_title] => Aircraft for the transport of passengers having lower deck facilities
[patent_app_type] => utility
[patent_app_number] => 15/355257
[patent_app_country] => US
[patent_app_date] => 2016-11-18
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
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[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 15355257
[rel_patent_id] =>[rel_patent_doc_number] =>) 15/355257 | Aircraft for the transport of passengers having lower deck facilities | Nov 17, 2016 | Issued |
Array
(
[id] => 14550691
[patent_doc_number] => 10343785
[patent_country] => US
[patent_kind] => B1
[patent_issue_date] => 2019-07-09
[patent_title] => Hybrid rotary drone and method of use
[patent_app_type] => utility
[patent_app_number] => 15/356364
[patent_app_country] => US
[patent_app_date] => 2016-11-18
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
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[patent_no_of_words] => 1314
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[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 15356364
[rel_patent_id] =>[rel_patent_doc_number] =>) 15/356364 | Hybrid rotary drone and method of use | Nov 17, 2016 | Issued |
Array
(
[id] => 11648871
[patent_doc_number] => 20170144771
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2017-05-25
[patent_title] => 'GIMBALED THRUSTER CONFIGURATION FOR USE WITH UNMANNED AERIAL VEHICLE'
[patent_app_type] => utility
[patent_app_number] => 15/355679
[patent_app_country] => US
[patent_app_date] => 2016-11-18
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 31
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[patent_current_assignee] =>[type] => publication
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 15355679
[rel_patent_id] =>[rel_patent_doc_number] =>) 15/355679 | Gimbaled thruster configuration for use with unmanned aerial vehicle | Nov 17, 2016 | Issued |
Array
(
[id] => 11626933
[patent_doc_number] => 20170137123
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2017-05-18
[patent_title] => 'System, Apparatus and Methods for an Airspace Plane with Shockwave Piercing Wings'
[patent_app_type] => utility
[patent_app_number] => 15/355010
[patent_app_country] => US
[patent_app_date] => 2016-11-17
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 10
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[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 15355010
[rel_patent_id] =>[rel_patent_doc_number] =>) 15/355010 | System, Apparatus and Methods for an Airspace Plane with Shockwave Piercing Wings | Nov 16, 2016 | Abandoned |
Array
(
[id] => 14467025
[patent_doc_number] => 20190185154
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2019-06-20
[patent_title] => INTERMESHING ROTARY-WING AIRCRAFT WITH SYMMETRICAL SWASH PLATE
[patent_app_type] => utility
[patent_app_number] => 16/327318
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[rel_patent_id] =>[rel_patent_doc_number] =>) 16/327318 | INTERMESHING ROTARY-WING AIRCRAFT WITH SYMMETRICAL SWASH PLATE | Nov 13, 2016 | Abandoned |
Array
(
[id] => 16444562
[patent_doc_number] => 10836472
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2020-11-17
[patent_title] => One-piece composite bifurcated winglet
[patent_app_type] => utility
[patent_app_number] => 15/344581
[patent_app_country] => US
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[rel_patent_id] =>[rel_patent_doc_number] =>) 15/344581 | One-piece composite bifurcated winglet | Nov 5, 2016 | Issued |
Array
(
[id] => 11603722
[patent_doc_number] => 20170121023
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2017-05-04
[patent_title] => 'APPARATUS AND METHOD FOR PROVIDING PACKAGE RELEASE TO UNMANNED AERIAL SYSTEM'
[patent_app_type] => utility
[patent_app_number] => 15/337397
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[rel_patent_id] =>[rel_patent_doc_number] =>) 15/337397 | Apparatus and method for providing package release to unmanned aerial system | Oct 27, 2016 | Issued |
Array
(
[id] => 13521407
[patent_doc_number] => 20180312246
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2018-11-01
[patent_title] => Flying Object
[patent_app_type] => utility
[patent_app_number] => 15/770254
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[rel_patent_id] =>[rel_patent_doc_number] =>) 15/770254 | Flying object | Oct 27, 2016 | Issued |
Array
(
[id] => 14820395
[patent_doc_number] => 10407189
[patent_country] => US
[patent_kind] => B1
[patent_issue_date] => 2019-09-10
[patent_title] => Spacecraft exoskeleton truss structure
[patent_app_type] => utility
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[rel_patent_id] =>[rel_patent_doc_number] =>) 15/336541 | Spacecraft exoskeleton truss structure | Oct 26, 2016 | Issued |
Array
(
[id] => 11582625
[patent_doc_number] => 09637247
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[patent_issue_date] => 2017-05-02
[patent_title] => 'Component deployment system'
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[rel_patent_id] =>[rel_patent_doc_number] =>) 15/335433 | Component deployment system | Oct 26, 2016 | Issued |
Array
(
[id] => 13506953
[patent_doc_number] => 20180305019
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[patent_title] => FIXED-WING AIRCRAFT WITH INCREASED STATIC STABILITY
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[rel_patent_id] =>[rel_patent_doc_number] =>) 15/767650 | FIXED-WING AIRCRAFT WITH INCREASED STATIC STABILITY | Oct 20, 2016 | Abandoned |
Array
(
[id] => 12607845
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[patent_issue_date] => 2018-04-05
[patent_title] => LANDING GEAR PLATFORM
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[rel_patent_id] =>[rel_patent_doc_number] =>) 15/281408 | Landing gear platform | Sep 29, 2016 | Issued |