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] => 4968341 [patent_doc_number] => 20070108343 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2007-05-17 [patent_title] => 'Flight control surface actuator assembly including a free trail mechanism' [patent_app_type] => utility [patent_app_number] => 11/331755 [patent_app_country] => US [patent_app_date] => 2006-01-13 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 4 [patent_figures_cnt] => 4 [patent_no_of_words] => 3525 [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] => publications/A1/0108/20070108343.pdf [firstpage_image] =>[orig_patent_app_number] => 11331755 [rel_patent_id] =>[rel_patent_doc_number] =>)
11/331755
Flight control surface actuator assembly including a free trial mechanism Jan 12, 2006 Issued
Array ( [id] => 5779987 [patent_doc_number] => 20060202082 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2006-09-14 [patent_title] => 'Microjet actuators for the control of flow separation and distortion' [patent_app_type] => utility [patent_app_number] => 11/329721 [patent_app_country] => US [patent_app_date] => 2006-01-11 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 16 [patent_figures_cnt] => 16 [patent_no_of_words] => 3506 [patent_no_of_claims] => 20 [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] => publications/A1/0202/20060202082.pdf [firstpage_image] =>[orig_patent_app_number] => 11329721 [rel_patent_id] =>[rel_patent_doc_number] =>)
11/329721
Microjet actuators for the control of flow separation and distortion Jan 10, 2006 Abandoned
Array ( [id] => 5217185 [patent_doc_number] => 20070158496 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2007-07-12 [patent_title] => 'Mechanism for reducing heat generation in a joint' [patent_app_type] => utility [patent_app_number] => 11/326754 [patent_app_country] => US [patent_app_date] => 2006-01-06 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 7 [patent_figures_cnt] => 7 [patent_no_of_words] => 2907 [patent_no_of_claims] => 26 [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] => publications/A1/0158/20070158496.pdf [firstpage_image] =>[orig_patent_app_number] => 11326754 [rel_patent_id] =>[rel_patent_doc_number] =>)
11/326754
Mechanism for reducing heat generation in a joint Jan 5, 2006 Issued
Array ( [id] => 5157264 [patent_doc_number] => 20070170308 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2007-07-26 [patent_title] => 'Brake for a kite' [patent_app_type] => utility [patent_app_number] => 11/327300 [patent_app_country] => US [patent_app_date] => 2006-01-06 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 4 [patent_figures_cnt] => 4 [patent_no_of_words] => 2070 [patent_no_of_claims] => 20 [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] => publications/A1/0170/20070170308.pdf [firstpage_image] =>[orig_patent_app_number] => 11327300 [rel_patent_id] =>[rel_patent_doc_number] =>)
11/327300
Brake for a kite Jan 5, 2006 Issued
Array ( [id] => 5217189 [patent_doc_number] => 20070158500 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2007-07-12 [patent_title] => 'Solid oxide fuel cell system for aircraft power, heat, water, and oxygen generation' [patent_app_type] => utility [patent_app_number] => 11/326400 [patent_app_country] => US [patent_app_date] => 2006-01-06 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 3 [patent_figures_cnt] => 3 [patent_no_of_words] => 2997 [patent_no_of_claims] => 22 [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] => publications/A1/0158/20070158500.pdf [firstpage_image] =>[orig_patent_app_number] => 11326400 [rel_patent_id] =>[rel_patent_doc_number] =>)
11/326400
Solid oxide fuel cell system for aircraft power, heat, water, and oxygen generation Jan 5, 2006 Abandoned
Array ( [id] => 5157268 [patent_doc_number] => 20070170312 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2007-07-26 [patent_title] => 'Energy-efficient electro-thermal ice-protection system' [patent_app_type] => utility [patent_app_number] => 11/327262 [patent_app_country] => US [patent_app_date] => 2006-01-06 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 7 [patent_figures_cnt] => 7 [patent_no_of_words] => 6324 [patent_no_of_claims] => 20 [patent_no_of_ind_claims] => 14 [patent_words_short_claim] => 0 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] => publications/A1/0170/20070170312.pdf [firstpage_image] =>[orig_patent_app_number] => 11327262 [rel_patent_id] =>[rel_patent_doc_number] =>)
11/327262
Energy-efficient electro-thermal ice-protection system Jan 5, 2006 Issued
Array ( [id] => 128975 [patent_doc_number] => 07699260 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2010-04-20 [patent_title] => 'Vertical takeoff and landing aircraft using a redundant array of independent rotors' [patent_app_type] => utility [patent_app_number] => 11/325159 [patent_app_country] => US [patent_app_date] => 2006-01-04 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 12 [patent_figures_cnt] => 12 [patent_no_of_words] => 3798 [patent_no_of_claims] => 2 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 573 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/07/699/07699260.pdf [firstpage_image] =>[orig_patent_app_number] => 11325159 [rel_patent_id] =>[rel_patent_doc_number] =>)
11/325159
Vertical takeoff and landing aircraft using a redundant array of independent rotors Jan 3, 2006 Issued
Array ( [id] => 4985765 [patent_doc_number] => 20070152102 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2007-07-05 [patent_title] => 'High drag parachute with radial slots providing porosity distribution and enhanced stability without forward speed' [patent_app_type] => utility [patent_app_number] => 11/324241 [patent_app_country] => US [patent_app_date] => 2006-01-04 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 4 [patent_figures_cnt] => 4 [patent_no_of_words] => 3512 [patent_no_of_claims] => 22 [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] => publications/A1/0152/20070152102.pdf [firstpage_image] =>[orig_patent_app_number] => 11324241 [rel_patent_id] =>[rel_patent_doc_number] =>)
11/324241
High drag parachute with radial slots providing porosity distribution and enhanced stability without forward speed Jan 3, 2006 Abandoned
Array ( [id] => 4985767 [patent_doc_number] => 20070152104 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2007-07-05 [patent_title] => 'Method and system for flow control with arrays of dual bimorph synthetic jet fluidic actuators' [patent_app_type] => utility [patent_app_number] => 11/325063 [patent_app_country] => US [patent_app_date] => 2006-01-03 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 9 [patent_figures_cnt] => 9 [patent_no_of_words] => 7117 [patent_no_of_claims] => 24 [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] => publications/A1/0152/20070152104.pdf [firstpage_image] =>[orig_patent_app_number] => 11325063 [rel_patent_id] =>[rel_patent_doc_number] =>)
11/325063
Method and system for flow control with arrays of dual bimorph synthetic jet fluidic actuators Jan 2, 2006 Issued
Array ( [id] => 5628545 [patent_doc_number] => 20060145013 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2006-07-06 [patent_title] => 'Sealing device for a flap track in a belly fairing of an aircraft for a flap-actuating shaft' [patent_app_type] => utility [patent_app_number] => 11/323291 [patent_app_country] => US [patent_app_date] => 2005-12-30 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 7 [patent_figures_cnt] => 7 [patent_no_of_words] => 2545 [patent_no_of_claims] => 10 [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/A1/0145/20060145013.pdf [firstpage_image] =>[orig_patent_app_number] => 11323291 [rel_patent_id] =>[rel_patent_doc_number] =>)
11/323291
Sealing device for a flap track in a belly fairing of an aircraft for a flap-actuating shaft Dec 29, 2005 Issued
Array ( [id] => 4556048 [patent_doc_number] => 07857254 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2010-12-28 [patent_title] => 'System and method for utilizing stored electrical energy for VTOL aircraft thrust enhancement and attitude control' [patent_app_type] => utility [patent_app_number] => 11/313997 [patent_app_country] => US [patent_app_date] => 2005-12-22 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 40 [patent_figures_cnt] => 50 [patent_no_of_words] => 15292 [patent_no_of_claims] => 34 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 144 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/07/857/07857254.pdf [firstpage_image] =>[orig_patent_app_number] => 11313997 [rel_patent_id] =>[rel_patent_doc_number] =>)
11/313997
System and method for utilizing stored electrical energy for VTOL aircraft thrust enhancement and attitude control Dec 21, 2005 Issued
Array ( [id] => 8801030 [patent_doc_number] => 08439299 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2013-05-14 [patent_title] => 'Active cancellation and vibration isolation with feedback and feedforward control for an aircraft engine mount' [patent_app_type] => utility [patent_app_number] => 11/312410 [patent_app_country] => US [patent_app_date] => 2005-12-21 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 7 [patent_figures_cnt] => 7 [patent_no_of_words] => 3402 [patent_no_of_claims] => 18 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 80 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 11312410 [rel_patent_id] =>[rel_patent_doc_number] =>)
11/312410
Active cancellation and vibration isolation with feedback and feedforward control for an aircraft engine mount Dec 20, 2005 Issued
Array ( [id] => 5593707 [patent_doc_number] => 20060157623 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2006-07-20 [patent_title] => 'Wing, in particular airfoil of an aircraft, with a variable profile shape' [patent_app_type] => utility [patent_app_number] => 11/312860 [patent_app_country] => US [patent_app_date] => 2005-12-20 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 8 [patent_figures_cnt] => 8 [patent_no_of_words] => 4122 [patent_no_of_claims] => 24 [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/A1/0157/20060157623.pdf [firstpage_image] =>[orig_patent_app_number] => 11312860 [rel_patent_id] =>[rel_patent_doc_number] =>)
11/312860
Wing, in particular airfoil of an aircraft, with a variable profile shape Dec 19, 2005 Issued
Array ( [id] => 8197713 [patent_doc_number] => 08186616 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2012-05-29 [patent_title] => 'Hybrid transonic-subsonic aerofoils' [patent_app_type] => utility [patent_app_number] => 11/305345 [patent_app_country] => US [patent_app_date] => 2005-12-19 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 5 [patent_figures_cnt] => 26 [patent_no_of_words] => 7763 [patent_no_of_claims] => 28 [patent_no_of_ind_claims] => 4 [patent_words_short_claim] => 229 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/08/186/08186616.pdf [firstpage_image] =>[orig_patent_app_number] => 11305345 [rel_patent_id] =>[rel_patent_doc_number] =>)
11/305345
Hybrid transonic-subsonic aerofoils Dec 18, 2005 Issued
Array ( [id] => 4441696 [patent_doc_number] => 07971221 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2011-06-28 [patent_title] => 'Overhead video system for an aircraft' [patent_app_type] => utility [patent_app_number] => 11/303652 [patent_app_country] => US [patent_app_date] => 2005-12-16 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 10 [patent_figures_cnt] => 11 [patent_no_of_words] => 5282 [patent_no_of_claims] => 7 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 163 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/07/971/07971221.pdf [firstpage_image] =>[orig_patent_app_number] => 11303652 [rel_patent_id] =>[rel_patent_doc_number] =>)
11/303652
Overhead video system for an aircraft Dec 15, 2005 Issued
Array ( [id] => 7799761 [patent_doc_number] => 08128027 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2012-03-06 [patent_title] => 'Plug-n-play power system for an accessory in an aircraft' [patent_app_type] => utility [patent_app_number] => 11/303173 [patent_app_country] => US [patent_app_date] => 2005-12-16 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 10 [patent_figures_cnt] => 13 [patent_no_of_words] => 5012 [patent_no_of_claims] => 6 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 185 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/08/128/08128027.pdf [firstpage_image] =>[orig_patent_app_number] => 11303173 [rel_patent_id] =>[rel_patent_doc_number] =>)
11/303173
Plug-n-play power system for an accessory in an aircraft Dec 15, 2005 Issued
Array ( [id] => 5222772 [patent_doc_number] => 20070252038 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2007-11-01 [patent_title] => 'Aerial Security and Control System' [patent_app_type] => utility [patent_app_number] => 11/306090 [patent_app_country] => US [patent_app_date] => 2005-12-15 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 4 [patent_figures_cnt] => 4 [patent_no_of_words] => 2845 [patent_no_of_claims] => 28 [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/A1/0252/20070252038.pdf [firstpage_image] =>[orig_patent_app_number] => 11306090 [rel_patent_id] =>[rel_patent_doc_number] =>)
11/306090
Aerial Security and Control System Dec 14, 2005 Abandoned
Array ( [id] => 1076074 [patent_doc_number] => 07614583 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2009-11-10 [patent_title] => 'Monument fitting assembly' [patent_app_type] => utility [patent_app_number] => 11/306030 [patent_app_country] => US [patent_app_date] => 2005-12-14 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 7 [patent_figures_cnt] => 16 [patent_no_of_words] => 3099 [patent_no_of_claims] => 10 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 277 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/07/614/07614583.pdf [firstpage_image] =>[orig_patent_app_number] => 11306030 [rel_patent_id] =>[rel_patent_doc_number] =>)
11/306030
Monument fitting assembly Dec 13, 2005 Issued
Array ( [id] => 5250364 [patent_doc_number] => 20070131820 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2007-06-14 [patent_title] => 'Rotorcraft control system and method of using' [patent_app_type] => utility [patent_app_number] => 11/299158 [patent_app_country] => US [patent_app_date] => 2005-12-09 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 3 [patent_figures_cnt] => 3 [patent_no_of_words] => 3769 [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] => publications/A1/0131/20070131820.pdf [firstpage_image] =>[orig_patent_app_number] => 11299158 [rel_patent_id] =>[rel_patent_doc_number] =>)
11/299158
Rotorcraft control system and method of using Dec 8, 2005 Abandoned
Array ( [id] => 5076784 [patent_doc_number] => 20070120008 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2007-05-31 [patent_title] => 'Engine airframe J-seal damper' [patent_app_type] => utility [patent_app_number] => 11/291013 [patent_app_country] => US [patent_app_date] => 2005-11-30 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 5 [patent_figures_cnt] => 5 [patent_no_of_words] => 2930 [patent_no_of_claims] => 26 [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] => publications/A1/0120/20070120008.pdf [firstpage_image] =>[orig_patent_app_number] => 11291013 [rel_patent_id] =>[rel_patent_doc_number] =>)
11/291013
Engine airframe J-seal damper Nov 29, 2005 Issued
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