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] => 9949357
[patent_doc_number] => 08998130
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2015-04-07
[patent_title] => 'Self-aligning inlet plenum system for rotorcraft'
[patent_app_type] => utility
[patent_app_number] => 13/703785
[patent_app_country] => US
[patent_app_date] => 2011-04-28
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 8
[patent_figures_cnt] => 9
[patent_no_of_words] => 2857
[patent_no_of_claims] => 15
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[patent_words_short_claim] => 148
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13703785
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/703785 | Self-aligning inlet plenum system for rotorcraft | Apr 27, 2011 | Issued |
Array
(
[id] => 7583889
[patent_doc_number] => 20110278399
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2011-11-17
[patent_title] => 'PANEL TYPE ARTIFICIAL SATELLITE AND ARTIFICIAL SATELLITE SYSTEM THEREWITH'
[patent_app_type] => utility
[patent_app_number] => 13/096078
[patent_app_country] => US
[patent_app_date] => 2011-04-28
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 6
[patent_figures_cnt] => 6
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[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0278/20110278399.pdf
[firstpage_image] =>[orig_patent_app_number] => 13096078
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/096078 | Panel type artificial satellite and artificial satellite system therewith | Apr 27, 2011 | Issued |
Array
(
[id] => 8474204
[patent_doc_number] => 20120273611
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2012-11-01
[patent_title] => 'EXHAUST SILENCER WITH BAFFLES'
[patent_app_type] => utility
[patent_app_number] => 13/094179
[patent_app_country] => US
[patent_app_date] => 2011-04-26
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 6
[patent_figures_cnt] => 6
[patent_no_of_words] => 3117
[patent_no_of_claims] => 20
[patent_no_of_ind_claims] => 3
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[patent_current_assignee] =>[type] => publication
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13094179
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/094179 | Exhaust silencer with baffles | Apr 25, 2011 | Issued |
Array
(
[id] => 8310222
[patent_doc_number] => 20120187247
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2012-07-26
[patent_title] => 'Manhole assembly in the lower skin of an aircraft wing made of a composite material'
[patent_app_type] => utility
[patent_app_number] => 13/066771
[patent_app_country] => US
[patent_app_date] => 2011-04-25
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 3
[patent_no_of_words] => 1666
[patent_no_of_claims] => 9
[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] => 13066771
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/066771 | Manhole assembly in the lower skin of an aircraft wing made of a composite material | Apr 24, 2011 | Issued |
Array
(
[id] => 8133447
[patent_doc_number] => 20120091270
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2012-04-19
[patent_title] => 'AIRCRAFT CONFIGURATION'
[patent_app_type] => utility
[patent_app_number] => 13/093596
[patent_app_country] => US
[patent_app_date] => 2011-04-25
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 22
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[patent_no_of_words] => 8629
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[pdf_file] => publications/A1/0091/20120091270.pdf
[firstpage_image] =>[orig_patent_app_number] => 13093596
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/093596 | Aircraft configuration | Apr 24, 2011 | Issued |
Array
(
[id] => 7496568
[patent_doc_number] => 20110260008
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2011-10-27
[patent_title] => 'Fluid flow control device for an aerofoil'
[patent_app_type] => utility
[patent_app_number] => 13/066736
[patent_app_country] => US
[patent_app_date] => 2011-04-22
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 16
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[patent_no_of_words] => 6926
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[pdf_file] => publications/A1/0260/20110260008.pdf
[firstpage_image] =>[orig_patent_app_number] => 13066736
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/066736 | Fluid flow control device for an aerofoil | Apr 21, 2011 | Abandoned |
Array
(
[id] => 8795852
[patent_doc_number] => 08434712
[patent_country] => US
[patent_kind] => B1
[patent_issue_date] => 2013-05-07
[patent_title] => 'Methods and apparatus for driving rotational elements of a vehicle'
[patent_app_type] => utility
[patent_app_number] => 13/091102
[patent_app_country] => US
[patent_app_date] => 2011-04-20
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 11
[patent_figures_cnt] => 18
[patent_no_of_words] => 9045
[patent_no_of_claims] => 20
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[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13091102
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/091102 | Methods and apparatus for driving rotational elements of a vehicle | Apr 19, 2011 | Issued |
Array
(
[id] => 8462307
[patent_doc_number] => 20120267475
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2012-10-25
[patent_title] => 'ACOUSTIC SEAL FOR AIRCRAFT'
[patent_app_type] => utility
[patent_app_number] => 13/090597
[patent_app_country] => US
[patent_app_date] => 2011-04-20
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
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[patent_no_of_words] => 1188
[patent_no_of_claims] => 9
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[patent_current_assignee] =>[type] => publication
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13090597
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/090597 | ACOUSTIC SEAL FOR AIRCRAFT | Apr 19, 2011 | Abandoned |
Array
(
[id] => 9587622
[patent_doc_number] => 08777156
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2014-07-15
[patent_title] => 'Heavier than air internal ballast'
[patent_app_type] => utility
[patent_app_number] => 13/091095
[patent_app_country] => US
[patent_app_date] => 2011-04-20
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
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[patent_no_of_words] => 3568
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[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13091095
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/091095 | Heavier than air internal ballast | Apr 19, 2011 | Issued |
Array
(
[id] => 9272321
[patent_doc_number] => 08636247
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2014-01-28
[patent_title] => 'Closed gas generator and micro power unit including the same'
[patent_app_type] => utility
[patent_app_number] => 13/089441
[patent_app_country] => US
[patent_app_date] => 2011-04-19
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 9
[patent_figures_cnt] => 12
[patent_no_of_words] => 13550
[patent_no_of_claims] => 16
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[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13089441
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/089441 | Closed gas generator and micro power unit including the same | Apr 18, 2011 | Issued |
Array
(
[id] => 8801035
[patent_doc_number] => 08439304
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2013-05-14
[patent_title] => 'Energy absorber system for an undercarriage, and an aircraft provided with said energy absorber system'
[patent_app_type] => utility
[patent_app_number] => 13/088511
[patent_app_country] => US
[patent_app_date] => 2011-04-18
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
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[patent_no_of_words] => 4801
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[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13088511
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/088511 | Energy absorber system for an undercarriage, and an aircraft provided with said energy absorber system | Apr 17, 2011 | Issued |
Array
(
[id] => 8806448
[patent_doc_number] => 08444093
[patent_country] => US
[patent_kind] => B1
[patent_issue_date] => 2013-05-21
[patent_title] => 'Airplane leading edge de-icing apparatus'
[patent_app_type] => utility
[patent_app_number] => 13/088630
[patent_app_country] => US
[patent_app_date] => 2011-04-18
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
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[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13088630
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/088630 | Airplane leading edge de-icing apparatus | Apr 17, 2011 | Issued |
Array
(
[id] => 9182413
[patent_doc_number] => 08622341
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2014-01-07
[patent_title] => 'Suspension rudder bar for an aircraft turbojet and a suspension with fan hanger provided therewith'
[patent_app_type] => utility
[patent_app_number] => 13/087693
[patent_app_country] => US
[patent_app_date] => 2011-04-15
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
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[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13087693
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/087693 | Suspension rudder bar for an aircraft turbojet and a suspension with fan hanger provided therewith | Apr 14, 2011 | Issued |
Array
(
[id] => 8770860
[patent_doc_number] => 08424801
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2013-04-23
[patent_title] => 'Slat support assembly'
[patent_app_type] => utility
[patent_app_number] => 13/064754
[patent_app_country] => US
[patent_app_date] => 2011-04-13
[patent_effective_date] => 0000-00-00
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[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13064754
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/064754 | Slat support assembly | Apr 12, 2011 | Issued |
Array
(
[id] => 7560302
[patent_doc_number] => 20110274134
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2011-11-10
[patent_title] => 'SOLAR PUMPED LASER MICROTHRUSTER'
[patent_app_type] => utility
[patent_app_number] => 13/084686
[patent_app_country] => US
[patent_app_date] => 2011-04-12
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[pdf_file] => publications/A1/0274/20110274134.pdf
[firstpage_image] =>[orig_patent_app_number] => 13084686
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/084686 | SOLAR PUMPED LASER MICROTHRUSTER | Apr 11, 2011 | Abandoned |
Array
(
[id] => 7666543
[patent_doc_number] => 20110315812
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2011-12-29
[patent_title] => 'WING DEVICE AND FLIGHT VEHICLE HAVING THE SAME'
[patent_app_type] => utility
[patent_app_number] => 13/084434
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[patent_app_date] => 2011-04-11
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[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13084434
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/084434 | Wing device and flight vehicle having the same | Apr 10, 2011 | Issued |
Array
(
[id] => 7506328
[patent_doc_number] => 20110253841
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2011-10-20
[patent_title] => 'METHOD AND SYSTEM FOR CHECKING THE FORMATION OF ICE ON AN AIRCRAFT IN FLIGHT'
[patent_app_type] => utility
[patent_app_number] => 13/082893
[patent_app_country] => US
[patent_app_date] => 2011-04-08
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[pdf_file] => publications/A1/0253/20110253841.pdf
[firstpage_image] =>[orig_patent_app_number] => 13082893
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/082893 | Method and system for checking the formation of ice on an aircraft in flight | Apr 7, 2011 | Issued |
Array
(
[id] => 7480060
[patent_doc_number] => 20110233330
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2011-09-29
[patent_title] => 'DEVICE FOR GENERATING AERODYNAMIC RESISTANCE ON AN AIRCRAFT'
[patent_app_type] => utility
[patent_app_number] => 13/082075
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[rel_patent_id] =>[rel_patent_doc_number] =>) 13/082075 | DEVICE FOR GENERATING AERODYNAMIC RESISTANCE ON AN AIRCRAFT | Apr 6, 2011 | Abandoned |
Array
(
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[patent_issue_date] => 2017-11-07
[patent_title] => 'Flight trajectory compensation system for airspeed variations'
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[rel_patent_id] =>[rel_patent_doc_number] =>) 13/078086 | Flight trajectory compensation system for airspeed variations | Mar 31, 2011 | Issued |
Array
(
[id] => 9702145
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[patent_kind] => B2
[patent_issue_date] => 2014-09-09
[patent_title] => 'Turboshaft engine supporting pylon covered with a porous material and turboshaft engine/pylon assembly'
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[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13636864
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/636864 | Turboshaft engine supporting pylon covered with a porous material and turboshaft engine/pylon assembly | Mar 20, 2011 | Issued |