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] => 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 [patent_no_of_ind_claims] => 2 [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 [patent_no_of_words] => 4303 [patent_no_of_claims] => 6 [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/A1/0278/20110278399.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 [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] => 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 [patent_figures_cnt] => 22 [patent_no_of_words] => 8629 [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/A1/0091/20120091270.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 [patent_figures_cnt] => 16 [patent_no_of_words] => 6926 [patent_no_of_claims] => 22 [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/A1/0260/20110260008.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 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 132 [patent_maintenance] => 1 [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 [patent_figures_cnt] => 3 [patent_no_of_words] => 1188 [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] => 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 [patent_figures_cnt] => 6 [patent_no_of_words] => 3568 [patent_no_of_claims] => 16 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 166 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [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 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 137 [patent_maintenance] => 1 [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 [patent_figures_cnt] => 7 [patent_no_of_words] => 4801 [patent_no_of_claims] => 22 [patent_no_of_ind_claims] => 4 [patent_words_short_claim] => 31 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [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 [patent_figures_cnt] => 8 [patent_no_of_words] => 5314 [patent_no_of_claims] => 10 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 302 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [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 [patent_figures_cnt] => 9 [patent_no_of_words] => 2754 [patent_no_of_claims] => 10 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 144 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [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 [patent_drawing_sheets_cnt] => 9 [patent_figures_cnt] => 13 [patent_no_of_words] => 6329 [patent_no_of_claims] => 27 [patent_no_of_ind_claims] => 5 [patent_words_short_claim] => 169 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [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 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 2 [patent_figures_cnt] => 2 [patent_no_of_words] => 1994 [patent_no_of_claims] => 30 [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/A1/0274/20110274134.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 [patent_app_country] => US [patent_app_date] => 2011-04-11 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 5 [patent_figures_cnt] => 5 [patent_no_of_words] => 3693 [patent_no_of_claims] => 17 [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] => 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 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 3 [patent_figures_cnt] => 3 [patent_no_of_words] => 5017 [patent_no_of_claims] => 12 [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/A1/0253/20110253841.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 [patent_app_country] => US [patent_app_date] => 2011-04-07 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 7 [patent_figures_cnt] => 7 [patent_no_of_words] => 4064 [patent_no_of_claims] => 15 [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/A1/0233/20110233330.pdf [firstpage_image] =>[orig_patent_app_number] => 13082075 [rel_patent_id] =>[rel_patent_doc_number] =>)
13/082075
DEVICE FOR GENERATING AERODYNAMIC RESISTANCE ON AN AIRCRAFT Apr 6, 2011 Abandoned
Array ( [id] => 12018392 [patent_doc_number] => 09811093 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2017-11-07 [patent_title] => 'Flight trajectory compensation system for airspeed variations' [patent_app_type] => utility [patent_app_number] => 13/078086 [patent_app_country] => US [patent_app_date] => 2011-04-01 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 7 [patent_figures_cnt] => 7 [patent_no_of_words] => 8506 [patent_no_of_claims] => 9 [patent_no_of_ind_claims] => 2 [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] => 13078086 [rel_patent_id] =>[rel_patent_doc_number] =>)
13/078086
Flight trajectory compensation system for airspeed variations Mar 31, 2011 Issued
Array ( [id] => 9702145 [patent_doc_number] => 08827199 [patent_country] => US [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' [patent_app_type] => utility [patent_app_number] => 13/636864 [patent_app_country] => US [patent_app_date] => 2011-03-21 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 3 [patent_figures_cnt] => 5 [patent_no_of_words] => 3443 [patent_no_of_claims] => 11 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 181 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [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
Menu