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] => 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
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[patent_maintenance] => 1
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[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
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[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
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[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
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[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
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[patent_no_of_words] => 3402
[patent_no_of_claims] => 18
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[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
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[patent_drawing_sheets_cnt] => 8
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[patent_no_of_words] => 4122
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[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
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[patent_no_of_words] => 7763
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[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
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[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
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[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
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[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
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[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
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[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
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[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 |