Search

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 numberTitle of the applicationFiling DateStatus
Array ( [id] => 10318199 [patent_doc_number] => 20150203202 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2015-07-23 [patent_title] => 'RAPID ENVIRONMENTAL CONTROL AERIAL DELIVERY SYSTEM' [patent_app_type] => utility [patent_app_number] => 14/162166 [patent_app_country] => US [patent_app_date] => 2014-01-23 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 16 [patent_figures_cnt] => 16 [patent_no_of_words] => 2261 [patent_no_of_claims] => 28 [patent_no_of_ind_claims] => 3 [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] => 14162166 [rel_patent_id] =>[rel_patent_doc_number] =>)
14/162166
RAPID ENVIRONMENTAL CONTROL AERIAL DELIVERY SYSTEM Jan 22, 2014 Abandoned
Array ( [id] => 10318213 [patent_doc_number] => 20150203217 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2015-07-23 [patent_title] => 'COMPOSITE BONDED REPAIR METHOD' [patent_app_type] => utility [patent_app_number] => 14/158077 [patent_app_country] => US [patent_app_date] => 2014-01-17 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 4 [patent_figures_cnt] => 4 [patent_no_of_words] => 1529 [patent_no_of_claims] => 15 [patent_no_of_ind_claims] => 3 [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] => 14158077 [rel_patent_id] =>[rel_patent_doc_number] =>)
14/158077
Composite bonded repair method Jan 16, 2014 Issued
Array ( [id] => 9600591 [patent_doc_number] => 20140197272 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2014-07-17 [patent_title] => 'AIRCRAFT WING FLAP DEVICE AND METHOD OF OPERATING THE SAME' [patent_app_type] => utility [patent_app_number] => 14/154661 [patent_app_country] => US [patent_app_date] => 2014-01-14 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 15 [patent_figures_cnt] => 15 [patent_no_of_words] => 8944 [patent_no_of_claims] => 11 [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] => 14154661 [rel_patent_id] =>[rel_patent_doc_number] =>)
14/154661
Aircraft wing flap device and method of operating the same Jan 13, 2014 Issued
Array ( [id] => 11225116 [patent_doc_number] => 09452830 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2016-09-27 [patent_title] => 'Constant velocity drive for tilt rotor assembly' [patent_app_type] => utility [patent_app_number] => 14/153482 [patent_app_country] => US [patent_app_date] => 2014-01-13 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 5 [patent_figures_cnt] => 7 [patent_no_of_words] => 2459 [patent_no_of_claims] => 17 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 210 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14153482 [rel_patent_id] =>[rel_patent_doc_number] =>)
14/153482
Constant velocity drive for tilt rotor assembly Jan 12, 2014 Issued
Array ( [id] => 10642232 [patent_doc_number] => 09359084 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2016-06-07 [patent_title] => 'Avionics cargo hold module having an upper integrated floor' [patent_app_type] => utility [patent_app_number] => 14/138588 [patent_app_country] => US [patent_app_date] => 2013-12-23 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 6 [patent_figures_cnt] => 19 [patent_no_of_words] => 8534 [patent_no_of_claims] => 30 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 60 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14138588 [rel_patent_id] =>[rel_patent_doc_number] =>)
14/138588
Avionics cargo hold module having an upper integrated floor Dec 22, 2013 Issued
Array ( [id] => 9613289 [patent_doc_number] => 20140203146 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2014-07-24 [patent_title] => 'Method And Device For Using Hot Air To De-Ice The Leading Edges Of A Jet Aircraft' [patent_app_type] => utility [patent_app_number] => 14/132018 [patent_app_country] => US [patent_app_date] => 2013-12-18 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 3 [patent_figures_cnt] => 3 [patent_no_of_words] => 3616 [patent_no_of_claims] => 16 [patent_no_of_ind_claims] => 3 [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] => 14132018 [rel_patent_id] =>[rel_patent_doc_number] =>)
14/132018
Method and device for using hot air to de-ice the leading edges of a jet aircraft Dec 17, 2013 Issued
Array ( [id] => 11211700 [patent_doc_number] => 09440726 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2016-09-13 [patent_title] => 'Joining structure for interior panel for aircraft' [patent_app_type] => utility [patent_app_number] => 14/652448 [patent_app_country] => US [patent_app_date] => 2013-12-18 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 14 [patent_figures_cnt] => 14 [patent_no_of_words] => 5741 [patent_no_of_claims] => 14 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 345 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14652448 [rel_patent_id] =>[rel_patent_doc_number] =>)
14/652448
Joining structure for interior panel for aircraft Dec 17, 2013 Issued
Array ( [id] => 13647415 [patent_doc_number] => 09850009 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2017-12-26 [patent_title] => Device, system and method for attitude control [patent_app_type] => utility [patent_app_number] => 14/651632 [patent_app_country] => US [patent_app_date] => 2013-12-17 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 6 [patent_figures_cnt] => 12 [patent_no_of_words] => 10138 [patent_no_of_claims] => 19 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 117 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14651632 [rel_patent_id] =>[rel_patent_doc_number] =>)
14/651632
Device, system and method for attitude control Dec 16, 2013 Issued
Array ( [id] => 9613282 [patent_doc_number] => 20140203138 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2014-07-24 [patent_title] => 'Lighter-Than-Air Systems, Methods, and Kits for Obtaining Aerial Images' [patent_app_type] => utility [patent_app_number] => 14/104059 [patent_app_country] => US [patent_app_date] => 2013-12-12 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 27 [patent_figures_cnt] => 27 [patent_no_of_words] => 34835 [patent_no_of_claims] => 20 [patent_no_of_ind_claims] => 3 [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] => 14104059 [rel_patent_id] =>[rel_patent_doc_number] =>)
14/104059
Lighter-than-air systems, methods, and kits for obtaining aerial images Dec 11, 2013 Issued
Array ( [id] => 9568467 [patent_doc_number] => 20140186180 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2014-07-03 [patent_title] => 'Switchable Vortex Generator and Array Formed Therewith, and Uses of the Same' [patent_app_type] => utility [patent_app_number] => 14/089992 [patent_app_country] => US [patent_app_date] => 2013-11-26 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 8 [patent_figures_cnt] => 8 [patent_no_of_words] => 4941 [patent_no_of_claims] => 16 [patent_no_of_ind_claims] => 3 [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] => 14089992 [rel_patent_id] =>[rel_patent_doc_number] =>)
14/089992
Switchable vortex generator and array formed therewith, and uses of the same Nov 25, 2013 Issued
Array ( [id] => 10581845 [patent_doc_number] => 09303964 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2016-04-05 [patent_title] => 'Low cost guiding device for projectile and method of operation' [patent_app_type] => utility [patent_app_number] => 14/065467 [patent_app_country] => US [patent_app_date] => 2013-10-29 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 6 [patent_figures_cnt] => 15 [patent_no_of_words] => 8141 [patent_no_of_claims] => 13 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 216 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14065467 [rel_patent_id] =>[rel_patent_doc_number] =>)
14/065467
Low cost guiding device for projectile and method of operation Oct 28, 2013 Issued
Array ( [id] => 14245659 [patent_doc_number] => 10273018 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2019-04-30 [patent_title] => Upturned exhaust system for rotary wing aircraft [patent_app_type] => utility [patent_app_number] => 14/049535 [patent_app_country] => US [patent_app_date] => 2013-10-09 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 11 [patent_figures_cnt] => 11 [patent_no_of_words] => 3473 [patent_no_of_claims] => 20 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 123 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14049535 [rel_patent_id] =>[rel_patent_doc_number] =>)
14/049535
Upturned exhaust system for rotary wing aircraft Oct 8, 2013 Issued
Array ( [id] => 13674513 [patent_doc_number] => 20160375990 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2016-12-29 [patent_title] => Landing Gear Noise Abatement Devices [patent_app_type] => utility [patent_app_number] => 14/048914 [patent_app_country] => US [patent_app_date] => 2013-10-08 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 0 [patent_figures_cnt] => 0 [patent_no_of_words] => 3622 [patent_no_of_claims] => 0 [patent_no_of_ind_claims] => -13 [patent_words_short_claim] => 42 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14048914 [rel_patent_id] =>[rel_patent_doc_number] =>)
14/048914
Landing gear noise abatement devices Oct 7, 2013 Issued
Array ( [id] => 11810051 [patent_doc_number] => 09714612 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2017-07-25 [patent_title] => 'Drag link fitting and vent combination' [patent_app_type] => utility [patent_app_number] => 14/045971 [patent_app_country] => US [patent_app_date] => 2013-10-04 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 7 [patent_figures_cnt] => 10 [patent_no_of_words] => 4175 [patent_no_of_claims] => 11 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 65 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14045971 [rel_patent_id] =>[rel_patent_doc_number] =>)
14/045971
Drag link fitting and vent combination Oct 3, 2013 Issued
Array ( [id] => 9277599 [patent_doc_number] => 20140027567 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2014-01-30 [patent_title] => 'LANDING GEAR ASSEMBLY OF AIRCRAFT' [patent_app_type] => utility [patent_app_number] => 14/042469 [patent_app_country] => US [patent_app_date] => 2013-09-30 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 7 [patent_figures_cnt] => 7 [patent_no_of_words] => 11230 [patent_no_of_claims] => 18 [patent_no_of_ind_claims] => 3 [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] => 14042469 [rel_patent_id] =>[rel_patent_doc_number] =>)
14/042469
Landing gear assembly of aircraft Sep 29, 2013 Issued
Array ( [id] => 9366281 [patent_doc_number] => 20140076154 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2014-03-20 [patent_title] => 'FLAP ACTUATOR' [patent_app_type] => utility [patent_app_number] => 14/031466 [patent_app_country] => US [patent_app_date] => 2013-09-19 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 6 [patent_figures_cnt] => 6 [patent_no_of_words] => 2473 [patent_no_of_claims] => 10 [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] => 14031466 [rel_patent_id] =>[rel_patent_doc_number] =>)
14/031466
Flap actuator Sep 18, 2013 Issued
Array ( [id] => 9913980 [patent_doc_number] => 20150069184 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2015-03-12 [patent_title] => 'CRYOGENIC FUEL TANKS FOR USE IN AIRCRAFT STRUCTURES' [patent_app_type] => utility [patent_app_number] => 14/025437 [patent_app_country] => US [patent_app_date] => 2013-09-12 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 15 [patent_figures_cnt] => 15 [patent_no_of_words] => 7539 [patent_no_of_claims] => 20 [patent_no_of_ind_claims] => 3 [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] => 14025437 [rel_patent_id] =>[rel_patent_doc_number] =>)
14/025437
Cryogenic fuel tanks for use in aircraft structures Sep 11, 2013 Issued
Array ( [id] => 10141952 [patent_doc_number] => 09174747 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2015-11-03 [patent_title] => 'Smart helipad for supporting landing of vertical takeoff and landing aircraft, system including the smart helipad, and method of providing the smart helipad' [patent_app_type] => utility [patent_app_number] => 14/025196 [patent_app_country] => US [patent_app_date] => 2013-09-12 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 6 [patent_figures_cnt] => 6 [patent_no_of_words] => 3613 [patent_no_of_claims] => 13 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 111 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14025196 [rel_patent_id] =>[rel_patent_doc_number] =>)
14/025196
Smart helipad for supporting landing of vertical takeoff and landing aircraft, system including the smart helipad, and method of providing the smart helipad Sep 11, 2013 Issued
Array ( [id] => 9206685 [patent_doc_number] => 20140005862 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2014-01-02 [patent_title] => 'Method and Apparatus for Aircraft Sensor and Actuator Failure Protection Using Reconfigurable Flight Control Laws' [patent_app_type] => utility [patent_app_number] => 14/017129 [patent_app_country] => US [patent_app_date] => 2013-09-03 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 16 [patent_figures_cnt] => 16 [patent_no_of_words] => 6387 [patent_no_of_claims] => 18 [patent_no_of_ind_claims] => 3 [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] => 14017129 [rel_patent_id] =>[rel_patent_doc_number] =>)
14/017129
Method and apparatus for aircraft sensor and actuator failure protection using reconfigurable flight control laws Sep 2, 2013 Issued
Array ( [id] => 10528791 [patent_doc_number] => 09254915 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2016-02-09 [patent_title] => 'Rotor system with torque-splitter assembly' [patent_app_type] => utility [patent_app_number] => 13/975830 [patent_app_country] => US [patent_app_date] => 2013-08-26 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 11 [patent_figures_cnt] => 11 [patent_no_of_words] => 3052 [patent_no_of_claims] => 20 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 73 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13975830 [rel_patent_id] =>[rel_patent_doc_number] =>)
13/975830
Rotor system with torque-splitter assembly Aug 25, 2013 Issued
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