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] => 9411881 [patent_doc_number] => 08695915 [patent_country] => US [patent_kind] => B1 [patent_issue_date] => 2014-04-15 [patent_title] => 'Flap side edge liners for airframe noise reduction' [patent_app_type] => utility [patent_app_number] => 13/417347 [patent_app_country] => US [patent_app_date] => 2012-03-12 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 5 [patent_figures_cnt] => 5 [patent_no_of_words] => 4020 [patent_no_of_claims] => 20 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 211 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13417347 [rel_patent_id] =>[rel_patent_doc_number] =>)
13/417347
Flap side edge liners for airframe noise reduction Mar 11, 2012 Issued
Array ( [id] => 9031335 [patent_doc_number] => 20130233973 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2013-09-12 [patent_title] => 'BONDED SPLICE JOINT' [patent_app_type] => utility [patent_app_number] => 13/414066 [patent_app_country] => US [patent_app_date] => 2012-03-07 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 8 [patent_figures_cnt] => 8 [patent_no_of_words] => 5310 [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] => 13414066 [rel_patent_id] =>[rel_patent_doc_number] =>)
13/414066
Bonded splice joint Mar 6, 2012 Issued
Array ( [id] => 8379563 [patent_doc_number] => 20120223190 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2012-09-06 [patent_title] => 'AERODYNAMIC BODY, REGULATING FLAP OR MAIN WING OR FIN OF AN AIRCRAFT AS WELL AS A STRUCTURAL COMPONENT WITH SUCH AN AERODYNAMIC BODY' [patent_app_type] => utility [patent_app_number] => 13/410365 [patent_app_country] => US [patent_app_date] => 2012-03-02 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 4 [patent_figures_cnt] => 4 [patent_no_of_words] => 5571 [patent_no_of_claims] => 12 [patent_no_of_ind_claims] => 1 [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] => 13410365 [rel_patent_id] =>[rel_patent_doc_number] =>)
13/410365
Aerodynamic body, regulating flap or main wing or fin of an aircraft as well as a structural component with such an aerodynamic body Mar 1, 2012 Issued
Array ( [id] => 9188575 [patent_doc_number] => 20130327890 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2013-12-12 [patent_title] => 'BUOYANCY SYSTEM' [patent_app_type] => utility [patent_app_number] => 14/001238 [patent_app_country] => US [patent_app_date] => 2012-02-27 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 11 [patent_figures_cnt] => 11 [patent_no_of_words] => 4358 [patent_no_of_claims] => 23 [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] => 14001238 [rel_patent_id] =>[rel_patent_doc_number] =>)
14/001238
BUOYANCY SYSTEM Feb 26, 2012 Abandoned
Array ( [id] => 9178148 [patent_doc_number] => 20130320133 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2013-12-05 [patent_title] => 'HOVERING AND GLIDING MULTI-WING FLAPPING MICRO AERIAL VEHICLE' [patent_app_type] => utility [patent_app_number] => 14/000191 [patent_app_country] => US [patent_app_date] => 2012-02-17 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 55 [patent_figures_cnt] => 55 [patent_no_of_words] => 22967 [patent_no_of_claims] => 30 [patent_no_of_ind_claims] => 13 [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] => 14000191 [rel_patent_id] =>[rel_patent_doc_number] =>)
14/000191
Hovering and gliding multi-wing flapping micro aerial vehicle Feb 16, 2012 Issued
Array ( [id] => 10862366 [patent_doc_number] => 08888050 [patent_country] => US [patent_kind] => B1 [patent_issue_date] => 2014-11-18 [patent_title] => 'Launch vehicle payload interface systems and methods' [patent_app_type] => utility [patent_app_number] => 13/397589 [patent_app_country] => US [patent_app_date] => 2012-02-15 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 5 [patent_figures_cnt] => 6 [patent_no_of_words] => 3995 [patent_no_of_claims] => 10 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 116 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13397589 [rel_patent_id] =>[rel_patent_doc_number] =>)
13/397589
Launch vehicle payload interface systems and methods Feb 14, 2012 Issued
Array ( [id] => 9709144 [patent_doc_number] => 08833701 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2014-09-16 [patent_title] => 'Moisture dispersion' [patent_app_type] => utility [patent_app_number] => 13/370870 [patent_app_country] => US [patent_app_date] => 2012-02-10 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 3 [patent_figures_cnt] => 5 [patent_no_of_words] => 5812 [patent_no_of_claims] => 8 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 104 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13370870 [rel_patent_id] =>[rel_patent_doc_number] =>)
13/370870
Moisture dispersion Feb 9, 2012 Issued
Array ( [id] => 9310204 [patent_doc_number] => 08651415 [patent_country] => US [patent_kind] => B1 [patent_issue_date] => 2014-02-18 [patent_title] => 'Engine cowl and inlet cover' [patent_app_type] => utility [patent_app_number] => 13/368802 [patent_app_country] => US [patent_app_date] => 2012-02-08 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 10 [patent_figures_cnt] => 12 [patent_no_of_words] => 7515 [patent_no_of_claims] => 20 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 113 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13368802 [rel_patent_id] =>[rel_patent_doc_number] =>)
13/368802
Engine cowl and inlet cover Feb 7, 2012 Issued
Array ( [id] => 8960618 [patent_doc_number] => 20130200220 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2013-08-08 [patent_title] => 'NON-INTERFERING DEPLOYABLE RADIATOR ARRANGEMENT FOR GEO SPACECRAFT' [patent_app_type] => utility [patent_app_number] => 13/368304 [patent_app_country] => US [patent_app_date] => 2012-02-07 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 8 [patent_figures_cnt] => 8 [patent_no_of_words] => 3289 [patent_no_of_claims] => 24 [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] => 13368304 [rel_patent_id] =>[rel_patent_doc_number] =>)
13/368304
Non-interfering deployable radiator arrangement for geo spacecraft Feb 6, 2012 Issued
Array ( [id] => 9467204 [patent_doc_number] => 08720830 [patent_country] => US [patent_kind] => B1 [patent_issue_date] => 2014-05-13 [patent_title] => 'Efficient solar panel wing-stowage on a space launch vehicle' [patent_app_type] => utility [patent_app_number] => 13/360919 [patent_app_country] => US [patent_app_date] => 2012-01-30 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 9 [patent_figures_cnt] => 9 [patent_no_of_words] => 4718 [patent_no_of_claims] => 18 [patent_no_of_ind_claims] => 4 [patent_words_short_claim] => 142 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13360919 [rel_patent_id] =>[rel_patent_doc_number] =>)
13/360919
Efficient solar panel wing-stowage on a space launch vehicle Jan 29, 2012 Issued
Array ( [id] => 9702150 [patent_doc_number] => 08827204 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2014-09-09 [patent_title] => 'Clutch system for rotary-wing aircraft with secondary thrust system' [patent_app_type] => utility [patent_app_number] => 13/349059 [patent_app_country] => US [patent_app_date] => 2012-01-12 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 5 [patent_figures_cnt] => 8 [patent_no_of_words] => 2573 [patent_no_of_claims] => 20 [patent_no_of_ind_claims] => 2 [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] => 13349059 [rel_patent_id] =>[rel_patent_doc_number] =>)
13/349059
Clutch system for rotary-wing aircraft with secondary thrust system Jan 11, 2012 Issued
Array ( [id] => 9587631 [patent_doc_number] => 08777165 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2014-07-15 [patent_title] => 'Aircraft fuel system' [patent_app_type] => utility [patent_app_number] => 13/346858 [patent_app_country] => US [patent_app_date] => 2012-01-10 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 7 [patent_figures_cnt] => 8 [patent_no_of_words] => 4306 [patent_no_of_claims] => 9 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 234 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13346858 [rel_patent_id] =>[rel_patent_doc_number] =>)
13/346858
Aircraft fuel system Jan 9, 2012 Issued
Array ( [id] => 9494887 [patent_doc_number] => 08733697 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2014-05-27 [patent_title] => 'Altitude control via rotation of balloon to adjust balloon density' [patent_app_type] => utility [patent_app_number] => 13/346620 [patent_app_country] => US [patent_app_date] => 2012-01-09 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 7 [patent_figures_cnt] => 10 [patent_no_of_words] => 11769 [patent_no_of_claims] => 34 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 153 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13346620 [rel_patent_id] =>[rel_patent_doc_number] =>)
13/346620
Altitude control via rotation of balloon to adjust balloon density Jan 8, 2012 Issued
Array ( [id] => 8913767 [patent_doc_number] => 20130175391 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2013-07-11 [patent_title] => 'Relative Positioning of Balloons with Altitude Control and Wind Data' [patent_app_type] => utility [patent_app_number] => 13/346637 [patent_app_country] => US [patent_app_date] => 2012-01-09 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 7 [patent_figures_cnt] => 7 [patent_no_of_words] => 14307 [patent_no_of_claims] => 47 [patent_no_of_ind_claims] => 5 [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] => 13346637 [rel_patent_id] =>[rel_patent_doc_number] =>)
13/346637
Relative positioning of balloons with altitude control and wind data Jan 8, 2012 Issued
Array ( [id] => 9231275 [patent_doc_number] => 08596575 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2013-12-03 [patent_title] => 'Aircraft actuator' [patent_app_type] => utility [patent_app_number] => 13/344204 [patent_app_country] => US [patent_app_date] => 2012-01-05 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 3 [patent_figures_cnt] => 3 [patent_no_of_words] => 10701 [patent_no_of_claims] => 5 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 350 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13344204 [rel_patent_id] =>[rel_patent_doc_number] =>)
13/344204
Aircraft actuator Jan 4, 2012 Issued
Array ( [id] => 8292973 [patent_doc_number] => 08220751 [patent_country] => US [patent_kind] => B1 [patent_issue_date] => 2012-07-17 [patent_title] => 'Multi-grommet retained slider for parachutes' [patent_app_type] => utility [patent_app_number] => 13/344138 [patent_app_country] => US [patent_app_date] => 2012-01-05 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 6 [patent_figures_cnt] => 21 [patent_no_of_words] => 7224 [patent_no_of_claims] => 22 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 193 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13344138 [rel_patent_id] =>[rel_patent_doc_number] =>)
13/344138
Multi-grommet retained slider for parachutes Jan 4, 2012 Issued
Array ( [id] => 8888260 [patent_doc_number] => 20130161444 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2013-06-27 [patent_title] => 'HIGH EFFICIENCY HUB FOR PRESSURE JET HELICOPTERS' [patent_app_type] => utility [patent_app_number] => 13/335887 [patent_app_country] => US [patent_app_date] => 2011-12-22 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 5 [patent_figures_cnt] => 5 [patent_no_of_words] => 2962 [patent_no_of_claims] => 20 [patent_no_of_ind_claims] => 7 [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] => 13335887 [rel_patent_id] =>[rel_patent_doc_number] =>)
13/335887
HIGH EFFICIENCY HUB FOR PRESSURE JET HELICOPTERS Dec 21, 2011 Abandoned
Array ( [id] => 10007548 [patent_doc_number] => 09051051 [patent_country] => US [patent_kind] => B1 [patent_issue_date] => 2015-06-09 [patent_title] => 'Floating aircraft archway and method therefor' [patent_app_type] => utility [patent_app_number] => 13/325825 [patent_app_country] => US [patent_app_date] => 2011-12-14 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 14 [patent_figures_cnt] => 16 [patent_no_of_words] => 3152 [patent_no_of_claims] => 20 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 135 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13325825 [rel_patent_id] =>[rel_patent_doc_number] =>)
13/325825
Floating aircraft archway and method therefor Dec 13, 2011 Issued
Array ( [id] => 8133415 [patent_doc_number] => 20120091256 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2012-04-19 [patent_title] => 'PROJECTILE' [patent_app_type] => utility [patent_app_number] => 13/324690 [patent_app_country] => US [patent_app_date] => 2011-12-13 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 5 [patent_figures_cnt] => 5 [patent_no_of_words] => 4283 [patent_no_of_claims] => 6 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 0 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] => publications/A1/0091/20120091256.pdf [firstpage_image] =>[orig_patent_app_number] => 13324690 [rel_patent_id] =>[rel_patent_doc_number] =>)
13/324690
PROJECTILE Dec 12, 2011 Abandoned
Array ( [id] => 12192473 [patent_doc_number] => 09896192 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2018-02-20 [patent_title] => 'Minimally intrusive wingtip vortex wake mitigation using microvane arrays' [patent_app_type] => utility [patent_app_number] => 13/324537 [patent_app_country] => US [patent_app_date] => 2011-12-13 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 1 [patent_figures_cnt] => 3 [patent_no_of_words] => 2022 [patent_no_of_claims] => 19 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 67 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13324537 [rel_patent_id] =>[rel_patent_doc_number] =>)
13/324537
Minimally intrusive wingtip vortex wake mitigation using microvane arrays Dec 12, 2011 Issued
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