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] => 9880788
[patent_doc_number] => 08967541
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2015-03-03
[patent_title] => 'Structural arrangement, aircraft or spacecraft and method'
[patent_app_type] => utility
[patent_app_number] => 13/649218
[patent_app_country] => US
[patent_app_date] => 2012-10-11
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 23
[patent_figures_cnt] => 25
[patent_no_of_words] => 8636
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[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13649218
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/649218 | Structural arrangement, aircraft or spacecraft and method | Oct 10, 2012 | Issued |
Array
(
[id] => 10916254
[patent_doc_number] => 20140319273
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2014-10-30
[patent_title] => 'Device for a Helicopter Deck'
[patent_app_type] => utility
[patent_app_number] => 14/346843
[patent_app_country] => US
[patent_app_date] => 2012-10-04
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
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[rel_patent_id] =>[rel_patent_doc_number] =>) 14/346843 | Device for a helicopter deck | Oct 3, 2012 | Issued |
Array
(
[id] => 10829603
[patent_doc_number] => 08857760
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2014-10-14
[patent_title] => 'Propulsive unit for an aircraft'
[patent_app_type] => utility
[patent_app_number] => 13/644980
[patent_app_country] => US
[patent_app_date] => 2012-10-04
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
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[rel_patent_id] =>[rel_patent_doc_number] =>) 13/644980 | Propulsive unit for an aircraft | Oct 3, 2012 | Issued |
Array
(
[id] => 9522364
[patent_doc_number] => 08746619
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2014-06-10
[patent_title] => 'Tail capable of improving anti-bird strike performance of aircraft'
[patent_app_type] => utility
[patent_app_number] => 13/630654
[patent_app_country] => US
[patent_app_date] => 2012-09-28
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 6
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[patent_no_of_words] => 3696
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[rel_patent_id] =>[rel_patent_doc_number] =>) 13/630654 | Tail capable of improving anti-bird strike performance of aircraft | Sep 27, 2012 | Issued |
Array
(
[id] => 9935723
[patent_doc_number] => 08985520
[patent_country] => US
[patent_kind] => B1
[patent_issue_date] => 2015-03-24
[patent_title] => 'Method of improved distribution over the surface of a parachute canopy'
[patent_app_type] => utility
[patent_app_number] => 13/625232
[patent_app_country] => US
[patent_app_date] => 2012-09-24
[patent_effective_date] => 0000-00-00
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[rel_patent_id] =>[rel_patent_doc_number] =>) 13/625232 | Method of improved distribution over the surface of a parachute canopy | Sep 23, 2012 | Issued |
Array
(
[id] => 8657644
[patent_doc_number] => 20130038473
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2013-02-14
[patent_title] => 'Securing Emergency and Safety Equipment on Aircraft'
[patent_app_type] => utility
[patent_app_number] => 13/621666
[patent_app_country] => US
[patent_app_date] => 2012-09-17
[patent_effective_date] => 0000-00-00
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[rel_patent_id] =>[rel_patent_doc_number] =>) 13/621666 | Securing emergency and safety equipment on aircraft | Sep 16, 2012 | Issued |
Array
(
[id] => 10155410
[patent_doc_number] => 09187165
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2015-11-17
[patent_title] => 'Systems and methods for attitude control of tethered aerostats'
[patent_app_type] => utility
[patent_app_number] => 13/621537
[patent_app_country] => US
[patent_app_date] => 2012-09-17
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[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13621537
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/621537 | Systems and methods for attitude control of tethered aerostats | Sep 16, 2012 | Issued |
Array
(
[id] => 11656936
[patent_doc_number] => 09669924
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2017-06-06
[patent_title] => 'Unmanned aerial vehicle'
[patent_app_type] => utility
[patent_app_number] => 14/347375
[patent_app_country] => US
[patent_app_date] => 2012-09-14
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 6
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[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14347375
[rel_patent_id] =>[rel_patent_doc_number] =>) 14/347375 | Unmanned aerial vehicle | Sep 13, 2012 | Issued |
Array
(
[id] => 9360177
[patent_doc_number] => 20140070049
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2014-03-13
[patent_title] => 'Ram Air Turbine Release Cable Assembly'
[patent_app_type] => utility
[patent_app_number] => 13/614535
[patent_app_country] => US
[patent_app_date] => 2012-09-13
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 7
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[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13614535
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/614535 | Ram air turbine release cable assembly | Sep 12, 2012 | Issued |
Array
(
[id] => 9334587
[patent_doc_number] => 20140061369
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2014-03-06
[patent_title] => 'Rotor Position Determination System with Hall-Effect Sensors'
[patent_app_type] => utility
[patent_app_number] => 13/601077
[patent_app_country] => US
[patent_app_date] => 2012-08-31
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 14
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[patent_no_of_claims] => 48
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[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13601077
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/601077 | Rotor position determination system with hall-effect sensors | Aug 30, 2012 | Issued |
Array
(
[id] => 9291140
[patent_doc_number] => 20140034774
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2014-02-06
[patent_title] => 'FAST, LONG-RANGE AIRCRAFT'
[patent_app_type] => utility
[patent_app_number] => 13/592772
[patent_app_country] => US
[patent_app_date] => 2012-08-23
[patent_effective_date] => 0000-00-00
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[rel_patent_id] =>[rel_patent_doc_number] =>) 13/592772 | Fast, long-range aircraft | Aug 22, 2012 | Issued |
Array
(
[id] => 9880780
[patent_doc_number] => 08967533
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2015-03-03
[patent_title] => 'Balloon power sources with a buoyancy trade-off'
[patent_app_type] => utility
[patent_app_number] => 13/590020
[patent_app_country] => US
[patent_app_date] => 2012-08-20
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[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13590020
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/590020 | Balloon power sources with a buoyancy trade-off | Aug 19, 2012 | Issued |
Array
(
[id] => 8646936
[patent_doc_number] => 20130032666
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2013-02-07
[patent_title] => 'AMPHIBIOUS AIRCRAFT'
[patent_app_type] => utility
[patent_app_number] => 13/589620
[patent_app_country] => US
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[rel_patent_id] =>[rel_patent_doc_number] =>) 13/589620 | Amphibious aircraft | Aug 19, 2012 | Issued |
Array
(
[id] => 8783516
[patent_doc_number] => 08430355
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2013-04-30
[patent_title] => 'Amphibious aircraft'
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[rel_patent_id] =>[rel_patent_doc_number] =>) 13/589574 | Amphibious aircraft | Aug 19, 2012 | Issued |
Array
(
[id] => 8680499
[patent_doc_number] => 20130048783
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2013-02-28
[patent_title] => 'LANDING GEAR ATTACHMENT'
[patent_app_type] => utility
[patent_app_number] => 13/569528
[patent_app_country] => US
[patent_app_date] => 2012-08-08
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[rel_patent_id] =>[rel_patent_doc_number] =>) 13/569528 | Landing gear attachment | Aug 7, 2012 | Issued |
Array
(
[id] => 9291146
[patent_doc_number] => 20140034779
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2014-02-06
[patent_title] => 'INDEPENDENT BLADE CONTROL SYSTEM WITH HYDRAULIC CYCLIC CONTROL'
[patent_app_type] => utility
[patent_app_number] => 13/565597
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[rel_patent_id] =>[rel_patent_doc_number] =>) 13/565597 | Independent blade control system with hydraulic cyclic control | Aug 1, 2012 | Issued |
Array
(
[id] => 8634503
[patent_doc_number] => 20130026305
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2013-01-31
[patent_title] => 'CONVERTIPLANE'
[patent_app_type] => utility
[patent_app_number] => 13/560219
[patent_app_country] => US
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[patent_effective_date] => 0000-00-00
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[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13560219
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/560219 | Convertiplane | Jul 26, 2012 | Issued |
Array
(
[id] => 8480672
[patent_doc_number] => 20120280079
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2012-11-08
[patent_title] => 'Airfoil Shaped Tail Boom'
[patent_app_type] => utility
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[patent_app_country] => US
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[rel_patent_id] =>[rel_patent_doc_number] =>) 13/554309 | Airfoil shaped tail boom | Jul 19, 2012 | Issued |
Array
(
[id] => 8801032
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Array
(
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[patent_title] => 'AIRCRAFT LANDING GEAR'
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[rel_patent_id] =>[rel_patent_doc_number] =>) 13/529150 | Aircraft landing gear | Jun 20, 2012 | Issued |