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] => 7480071
[patent_doc_number] => 20110233336
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2011-09-29
[patent_title] => 'FUSELAGE STRUCTURE FOR COMBINED FIXING OF INSULATION BLANKETS AND ITEMS OF EQUIPMENT, AIRCRAFT INCORPORATING SUCH A STRUCTURE'
[patent_app_type] => utility
[patent_app_number] => 13/120164
[patent_app_country] => US
[patent_app_date] => 2009-09-22
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 11
[patent_figures_cnt] => 11
[patent_no_of_words] => 5520
[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] => publications/A1/0233/20110233336.pdf
[firstpage_image] =>[orig_patent_app_number] => 13120164
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/120164 | Fuselage structure for combined fixing of insulation blankets and items of equipment, aircraft incorporating such a structure | Sep 21, 2009 | Issued |
Array
(
[id] => 9182416
[patent_doc_number] => 08622344
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2014-01-07
[patent_title] => 'Load path-optimized pivotable hatrack'
[patent_app_type] => utility
[patent_app_number] => 13/121703
[patent_app_country] => US
[patent_app_date] => 2009-09-16
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 6
[patent_no_of_words] => 4659
[patent_no_of_claims] => 11
[patent_no_of_ind_claims] => 2
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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] => 13121703
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/121703 | Load path-optimized pivotable hatrack | Sep 15, 2009 | Issued |
Array
(
[id] => 9284670
[patent_doc_number] => 08640989
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2014-02-04
[patent_title] => 'Speed brake for aircraft'
[patent_app_type] => utility
[patent_app_number] => 13/060927
[patent_app_country] => US
[patent_app_date] => 2009-08-26
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 7
[patent_no_of_words] => 1245
[patent_no_of_claims] => 6
[patent_no_of_ind_claims] => 1
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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] => 13060927
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/060927 | Speed brake for aircraft | Aug 25, 2009 | Issued |
Array
(
[id] => 7699698
[patent_doc_number] => 20110226892
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2011-09-22
[patent_title] => 'ROTARY WING VEHICLE'
[patent_app_type] => utility
[patent_app_number] => 13/057931
[patent_app_country] => US
[patent_app_date] => 2009-08-10
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 28
[patent_figures_cnt] => 28
[patent_no_of_words] => 16128
[patent_no_of_claims] => 18
[patent_no_of_ind_claims] => 2
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[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0226/20110226892.pdf
[firstpage_image] =>[orig_patent_app_number] => 13057931
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/057931 | ROTARY WING VEHICLE | Aug 9, 2009 | Abandoned |
Array
(
[id] => 6330875
[patent_doc_number] => 20100018322
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2010-01-28
[patent_title] => 'Switchable Vortex Generator and Array Formed Therewith, and Uses of the Same'
[patent_app_type] => utility
[patent_app_number] => 12/436616
[patent_app_country] => US
[patent_app_date] => 2009-05-06
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 8
[patent_figures_cnt] => 8
[patent_no_of_words] => 4897
[patent_no_of_claims] => 42
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[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0018/20100018322.pdf
[firstpage_image] =>[orig_patent_app_number] => 12436616
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/436616 | Switchable vortex generator and array formed therewith, and uses of the same | May 5, 2009 | Issued |
Array
(
[id] => 6129909
[patent_doc_number] => 20110006154
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2011-01-13
[patent_title] => 'Enhanced Lubrication Skewed Roller Clutch Assembly And Actuator Including Same'
[patent_app_type] => utility
[patent_app_number] => 12/420305
[patent_app_country] => US
[patent_app_date] => 2009-04-08
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 8
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[patent_no_of_words] => 3554
[patent_no_of_claims] => 20
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[pdf_file] => publications/A1/0006/20110006154.pdf
[firstpage_image] =>[orig_patent_app_number] => 12420305
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/420305 | Enhanced lubrication skewed roller clutch assembly and actuator including same | Apr 7, 2009 | Issued |
Array
(
[id] => 9253092
[patent_doc_number] => 08616498
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2013-12-31
[patent_title] => 'Aircraft insulation systems and methods'
[patent_app_type] => utility
[patent_app_number] => 12/415040
[patent_app_country] => US
[patent_app_date] => 2009-03-31
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 9
[patent_figures_cnt] => 14
[patent_no_of_words] => 6213
[patent_no_of_claims] => 24
[patent_no_of_ind_claims] => 4
[patent_words_short_claim] => 164
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 12415040
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/415040 | Aircraft insulation systems and methods | Mar 30, 2009 | Issued |
Array
(
[id] => 6160003
[patent_doc_number] => 20110192663
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2011-08-11
[patent_title] => 'WIG Vehicle Excluding Horizontal Stabilizer'
[patent_app_type] => utility
[patent_app_number] => 13/059888
[patent_app_country] => US
[patent_app_date] => 2009-03-18
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 6
[patent_figures_cnt] => 6
[patent_no_of_words] => 4636
[patent_no_of_claims] => 5
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[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0192/20110192663.pdf
[firstpage_image] =>[orig_patent_app_number] => 13059888
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/059888 | WIG Vehicle Excluding Horizontal Stabilizer | Mar 17, 2009 | Abandoned |
Array
(
[id] => 4441251
[patent_doc_number] => 07861974
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2011-01-04
[patent_title] => 'Docking system'
[patent_app_type] => utility
[patent_app_number] => 12/406955
[patent_app_country] => US
[patent_app_date] => 2009-03-18
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 14
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[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/07/861/07861974.pdf
[firstpage_image] =>[orig_patent_app_number] => 12406955
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/406955 | Docking system | Mar 17, 2009 | Issued |
Array
(
[id] => 6046230
[patent_doc_number] => 20110206528
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2011-08-25
[patent_title] => 'Wing Structure for WIG Vehicle'
[patent_app_type] => utility
[patent_app_number] => 13/059945
[patent_app_country] => US
[patent_app_date] => 2009-03-18
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 10
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[patent_no_of_words] => 5941
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[pdf_file] => publications/A1/0206/20110206528.pdf
[firstpage_image] =>[orig_patent_app_number] => 13059945
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/059945 | Wing Structure for WIG Vehicle | Mar 17, 2009 | Abandoned |
Array
(
[id] => 8664816
[patent_doc_number] => 08378278
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2013-02-19
[patent_title] => 'Foldable and deployable panel'
[patent_app_type] => utility
[patent_app_number] => 12/867364
[patent_app_country] => US
[patent_app_date] => 2009-02-23
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
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[patent_no_of_words] => 3902
[patent_no_of_claims] => 30
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[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 12867364
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/867364 | Foldable and deployable panel | Feb 22, 2009 | Issued |
Array
(
[id] => 5493178
[patent_doc_number] => 20090261206
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2009-10-22
[patent_title] => 'Method of using microjet actuators for the control of flow separation and distortion'
[patent_app_type] => utility
[patent_app_number] => 12/378605
[patent_app_country] => US
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[pdf_file] => publications/A1/0261/20090261206.pdf
[firstpage_image] =>[orig_patent_app_number] => 12378605
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/378605 | Method of using microjet actuators for the control of flow separation and distortion | Feb 17, 2009 | Abandoned |
Array
(
[id] => 1994
[patent_doc_number] => 07815149
[patent_country] => US
[patent_kind] => B1
[patent_issue_date] => 2010-10-19
[patent_title] => 'Magnetic capture docking mechanism'
[patent_app_type] => utility
[patent_app_number] => 12/388345
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[pdf_file] => patents/07/815/07815149.pdf
[firstpage_image] =>[orig_patent_app_number] => 12388345
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/388345 | Magnetic capture docking mechanism | Feb 17, 2009 | Issued |
Array
(
[id] => 6574238
[patent_doc_number] => 20100307442
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2010-12-09
[patent_title] => 'ENGINE INTAKE FLAP FOR BEING ARRANGED ON THE HOUSING OF AN AIR INTAKE OF AN AIRCRAFT ENGINE, AS WELL AS ENGINE WITH SUCH AN ENGINE INTAKE FLAP AND AIRCRAFT SYSTEM'
[patent_app_type] => utility
[patent_app_number] => 12/865931
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[patent_app_date] => 2009-02-04
[patent_effective_date] => 0000-00-00
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[pdf_file] => publications/A1/0307/20100307442.pdf
[firstpage_image] =>[orig_patent_app_number] => 12865931
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/865931 | Engine intake flap for being arranged on the housing of an air intake of an aircraft engine, as well as engine with such an engine intake flap and aircraft system | Feb 3, 2009 | Issued |
Array
(
[id] => 8795860
[patent_doc_number] => 08434720
[patent_country] => US
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[patent_issue_date] => 2013-05-07
[patent_title] => 'Pressurised aircraft door equipped with a vent flap'
[patent_app_type] => utility
[patent_app_number] => 12/863667
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[patent_app_date] => 2009-01-15
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[rel_patent_id] =>[rel_patent_doc_number] =>) 12/863667 | Pressurised aircraft door equipped with a vent flap | Jan 14, 2009 | Issued |
Array
(
[id] => 6391019
[patent_doc_number] => 20100163669
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2010-07-01
[patent_title] => 'Super aircraft structrue'
[patent_app_type] => utility
[patent_app_number] => 12/317733
[patent_app_country] => US
[patent_app_date] => 2008-12-29
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[pdf_file] => publications/A1/0163/20100163669.pdf
[firstpage_image] =>[orig_patent_app_number] => 12317733
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/317733 | Super aircraft structrue | Dec 28, 2008 | Abandoned |
Array
(
[id] => 4567190
[patent_doc_number] => 07854412
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2010-12-21
[patent_title] => 'Energy-efficient electro-thermal and electro-mechanical ice-protection method'
[patent_app_type] => utility
[patent_app_number] => 12/323685
[patent_app_country] => US
[patent_app_date] => 2008-11-26
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[pdf_file] => patents/07/854/07854412.pdf
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[rel_patent_id] =>[rel_patent_doc_number] =>) 12/323685 | Energy-efficient electro-thermal and electro-mechanical ice-protection method | Nov 25, 2008 | Issued |
Array
(
[id] => 5419563
[patent_doc_number] => 20090146017
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[patent_issue_date] => 2009-06-11
[patent_title] => 'Aircraft Trailing Edge Devices, Including Devices With Non-Parallel Motion Paths, and Associated Methods'
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[rel_patent_id] =>[rel_patent_doc_number] =>) 12/264831 | Aircraft trailing edge devices, including devices with non-parallel motion paths, and associated methods | Nov 3, 2008 | Issued |
Array
(
[id] => 7564628
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[patent_title] => 'Method for connecting a first material to a second material in aircraft construction'
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[rel_patent_id] =>[rel_patent_doc_number] =>) 12/682455 | Method for connecting a first material to a second material in aircraft construction | Oct 12, 2008 | Issued |
Array
(
[id] => 5561428
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[patent_title] => 'RADIO CONTROLLED TOY MODEL'
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[pdf_file] => publications/A1/0134/20090134280.pdf
[firstpage_image] =>[orig_patent_app_number] => 12207074
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/207074 | RADIO CONTROLLED TOY MODEL | Sep 8, 2008 | Abandoned |