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] => 11542386
[patent_doc_number] => 20170096211
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2017-04-06
[patent_title] => 'AJUSTIBLE AREA KITE OR WING'
[patent_app_type] => utility
[patent_app_number] => 15/282222
[patent_app_country] => US
[patent_app_date] => 2016-09-30
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 11
[patent_figures_cnt] => 11
[patent_no_of_words] => 8011
[patent_no_of_claims] => 19
[patent_no_of_ind_claims] => 4
[patent_words_short_claim] => 0
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 15282222
[rel_patent_id] =>[rel_patent_doc_number] =>) 15/282222 | Adjustable area kite or wing | Sep 29, 2016 | Issued |
Array
(
[id] => 16060407
[patent_doc_number] => 10689133
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2020-06-23
[patent_title] => Satellite with cylindrical main body, stack comprising such a satellite and launch assembly for such a satellite
[patent_app_type] => utility
[patent_app_number] => 15/764678
[patent_app_country] => US
[patent_app_date] => 2016-09-30
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 7
[patent_figures_cnt] => 10
[patent_no_of_words] => 5406
[patent_no_of_claims] => 14
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[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 15764678
[rel_patent_id] =>[rel_patent_doc_number] =>) 15/764678 | Satellite with cylindrical main body, stack comprising such a satellite and launch assembly for such a satellite | Sep 29, 2016 | Issued |
Array
(
[id] => 11993578
[patent_doc_number] => 20170297733
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2017-10-19
[patent_title] => 'Unmanned Helicopter'
[patent_app_type] => utility
[patent_app_number] => 15/278309
[patent_app_country] => US
[patent_app_date] => 2016-09-28
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 12
[patent_figures_cnt] => 12
[patent_no_of_words] => 8960
[patent_no_of_claims] => 10
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[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 15278309
[rel_patent_id] =>[rel_patent_doc_number] =>) 15/278309 | Unmanned Helicopter | Sep 27, 2016 | Abandoned |
Array
(
[id] => 11993532
[patent_doc_number] => 20170297687
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2017-10-19
[patent_title] => 'Tandem Rigid Rotor System and Method'
[patent_app_type] => utility
[patent_app_number] => 15/278636
[patent_app_country] => US
[patent_app_date] => 2016-09-28
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 6
[patent_figures_cnt] => 6
[patent_no_of_words] => 3872
[patent_no_of_claims] => 18
[patent_no_of_ind_claims] => 1
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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] => 15278636
[rel_patent_id] =>[rel_patent_doc_number] =>) 15/278636 | Tandem rigid rotor system and method | Sep 27, 2016 | Issued |
Array
(
[id] => 12583800
[patent_doc_number] => 20180086429
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2018-03-29
[patent_title] => Airfoil-Shaped Body Having Composite Base Skin with Integral Hat-Shaped Spar
[patent_app_type] => utility
[patent_app_number] => 15/278144
[patent_app_country] => US
[patent_app_date] => 2016-09-28
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 0
[patent_figures_cnt] => 0
[patent_no_of_words] => 8456
[patent_no_of_claims] => 0
[patent_no_of_ind_claims] => -19
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[patent_current_assignee] =>[type] => publication
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 15278144
[rel_patent_id] =>[rel_patent_doc_number] =>) 15/278144 | Airfoil-Shaped Body Having Composite Base Skin with Integral Hat-Shaped Spar | Sep 27, 2016 | Abandoned |
Array
(
[id] => 12583863
[patent_doc_number] => 20180086450
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2018-03-29
[patent_title] => AMPHIBIOUS FLYING VEHICLE
[patent_app_type] => utility
[patent_app_number] => 15/276809
[patent_app_country] => US
[patent_app_date] => 2016-09-27
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 0
[patent_figures_cnt] => 0
[patent_no_of_words] => 11894
[patent_no_of_claims] => 0
[patent_no_of_ind_claims] => -6
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[patent_current_assignee] =>[type] => publication
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 15276809
[rel_patent_id] =>[rel_patent_doc_number] =>) 15/276809 | AMPHIBIOUS FLYING VEHICLE | Sep 26, 2016 | Abandoned |
Array
(
[id] => 11513970
[patent_doc_number] => 20170081043
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2017-03-23
[patent_title] => 'PORTABLE UNMANNED DELIVERY AIRCRAFT LAUNCH SYSTEMS, AND METHODS OF DELIVERING PRODUCTS UTILIZING AIRCRAFT LAUNCH SYSTEMS'
[patent_app_type] => utility
[patent_app_number] => 15/271763
[patent_app_country] => US
[patent_app_date] => 2016-09-21
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 4
[patent_no_of_words] => 6568
[patent_no_of_claims] => 18
[patent_no_of_ind_claims] => 2
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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] => 15271763
[rel_patent_id] =>[rel_patent_doc_number] =>) 15/271763 | Portable unmanned delivery aircraft launch systems, and methods of delivering products utilizing aircraft launch systems | Sep 20, 2016 | Issued |
Array
(
[id] => 12260307
[patent_doc_number] => 20180079503
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2018-03-22
[patent_title] => 'ROTATING PROPROTOR ARRANGEMENT FOR A TILTROTOR AIRCRAFT'
[patent_app_type] => utility
[patent_app_number] => 15/272062
[patent_app_country] => US
[patent_app_date] => 2016-09-21
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 14
[patent_figures_cnt] => 14
[patent_no_of_words] => 4816
[patent_no_of_claims] => 31
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 0
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 15272062
[rel_patent_id] =>[rel_patent_doc_number] =>) 15/272062 | Rotating proprotor arrangement for a tiltrotor aircraft | Sep 20, 2016 | Issued |
Array
(
[id] => 11844264
[patent_doc_number] => 09731808
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2017-08-15
[patent_title] => 'Upper joints between outboard wing boxes and wing center sections of aircraft wing assemblies'
[patent_app_type] => utility
[patent_app_number] => 15/266779
[patent_app_country] => US
[patent_app_date] => 2016-09-15
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 10
[patent_figures_cnt] => 23
[patent_no_of_words] => 12111
[patent_no_of_claims] => 20
[patent_no_of_ind_claims] => 3
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[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 15266779
[rel_patent_id] =>[rel_patent_doc_number] =>) 15/266779 | Upper joints between outboard wing boxes and wing center sections of aircraft wing assemblies | Sep 14, 2016 | Issued |
Array
(
[id] => 12565122
[patent_doc_number] => 10017279
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2018-07-10
[patent_title] => Space vehicle comprising posts for forming a stack, stack comprising at least two such vehicles placed in a launcher, and method for releasing the vehicles
[patent_app_type] => utility
[patent_app_number] => 15/564816
[patent_app_country] => US
[patent_app_date] => 2016-09-12
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 9
[patent_figures_cnt] => 16
[patent_no_of_words] => 6875
[patent_no_of_claims] => 20
[patent_no_of_ind_claims] => 1
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[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 15564816
[rel_patent_id] =>[rel_patent_doc_number] =>) 15/564816 | Space vehicle comprising posts for forming a stack, stack comprising at least two such vehicles placed in a launcher, and method for releasing the vehicles | Sep 11, 2016 | Issued |
Array
(
[id] => 11476513
[patent_doc_number] => 20170063296
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2017-03-02
[patent_title] => 'Solar Panel with Flexible Optical Elements'
[patent_app_type] => utility
[patent_app_number] => 15/255172
[patent_app_country] => US
[patent_app_date] => 2016-09-02
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 13
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[patent_no_of_words] => 10543
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[patent_current_assignee] =>[type] => publication
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 15255172
[rel_patent_id] =>[rel_patent_doc_number] =>) 15/255172 | Solar panel with flexible optical elements | Sep 1, 2016 | Issued |
Array
(
[id] => 12232870
[patent_doc_number] => 20180065733
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2018-03-08
[patent_title] => 'LANDING GEAR TOGGLE LOCK MECHANISM'
[patent_app_type] => utility
[patent_app_number] => 15/255698
[patent_app_country] => US
[patent_app_date] => 2016-09-02
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 22
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[patent_no_of_words] => 11651
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[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 15255698
[rel_patent_id] =>[rel_patent_doc_number] =>) 15/255698 | Landing gear toggle lock mechanism | Sep 1, 2016 | Issued |
Array
(
[id] => 11492335
[patent_doc_number] => 20170066520
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2017-03-09
[patent_title] => 'INTEGRATED RIBS FOR CENTRAL WING BOX'
[patent_app_type] => utility
[patent_app_number] => 15/255639
[patent_app_country] => US
[patent_app_date] => 2016-09-02
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
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[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 15255639
[rel_patent_id] =>[rel_patent_doc_number] =>) 15/255639 | Integrated ribs for central wing box | Sep 1, 2016 | Issued |
Array
(
[id] => 11470831
[patent_doc_number] => 20170057614
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2017-03-02
[patent_title] => 'System, Apparatus and Methods for Hypersonic Shockwave Muffler'
[patent_app_type] => utility
[patent_app_number] => 15/256455
[patent_app_country] => US
[patent_app_date] => 2016-09-02
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 11
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[patent_current_assignee] =>[type] => publication
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 15256455
[rel_patent_id] =>[rel_patent_doc_number] =>) 15/256455 | System, apparatus and methods for hypersonic shockwave muffler | Sep 1, 2016 | Issued |
Array
(
[id] => 14245651
[patent_doc_number] => 10273014
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2019-04-30
[patent_title] => Oil cooler integrated into the pylon
[patent_app_type] => utility
[patent_app_number] => 15/255043
[patent_app_country] => US
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[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 15255043
[rel_patent_id] =>[rel_patent_doc_number] =>) 15/255043 | Oil cooler integrated into the pylon | Aug 31, 2016 | Issued |
Array
(
[id] => 11470869
[patent_doc_number] => 20170057652
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2017-03-02
[patent_title] => 'AIRCRAFT ENGINE UNIT COMPRISING AN IMPROVED FRONT ENGINE ATTACHMENT'
[patent_app_type] => utility
[patent_app_number] => 15/252585
[patent_app_country] => US
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[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 15252585
[rel_patent_id] =>[rel_patent_doc_number] =>) 15/252585 | Aircraft engine unit comprising an improved front engine attachment | Aug 30, 2016 | Issued |
Array
(
[id] => 14030793
[patent_doc_number] => 10227134
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2019-03-12
[patent_title] => Using drones to lift personnel up cell towers
[patent_app_type] => utility
[patent_app_number] => 15/248634
[patent_app_country] => US
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[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 15248634
[rel_patent_id] =>[rel_patent_doc_number] =>) 15/248634 | Using drones to lift personnel up cell towers | Aug 25, 2016 | Issued |
Array
(
[id] => 14118699
[patent_doc_number] => 10246192
[patent_country] => US
[patent_kind] => B1
[patent_issue_date] => 2019-04-02
[patent_title] => Passenger seat module
[patent_app_type] => utility
[patent_app_number] => 15/249255
[patent_app_country] => US
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[rel_patent_id] =>[rel_patent_doc_number] =>) 15/249255 | Passenger seat module | Aug 25, 2016 | Issued |
Array
(
[id] => 12218791
[patent_doc_number] => 20180057150
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2018-03-01
[patent_title] => 'DEPLOYABLE ASSEMBLY FOR A PROPULSOR'
[patent_app_type] => utility
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[patent_app_country] => US
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[rel_patent_id] =>[rel_patent_doc_number] =>) 15/244032 | Deployable assembly for a propulsor | Aug 22, 2016 | Issued |
Array
(
[id] => 14004997
[patent_doc_number] => 10220933
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2019-03-05
[patent_title] => Flight deck door assembly
[patent_app_type] => utility
[patent_app_number] => 15/241978
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[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 15241978
[rel_patent_id] =>[rel_patent_doc_number] =>) 15/241978 | Flight deck door assembly | Aug 18, 2016 | Issued |