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] => 6310360 [patent_doc_number] => 20100193643 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2010-08-05 [patent_title] => 'LIFT FAN SYSTEM' [patent_app_type] => utility [patent_app_number] => 12/643745 [patent_app_country] => US [patent_app_date] => 2009-12-21 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 4 [patent_figures_cnt] => 4 [patent_no_of_words] => 3648 [patent_no_of_claims] => 21 [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/A1/0193/20100193643.pdf [firstpage_image] =>[orig_patent_app_number] => 12643745 [rel_patent_id] =>[rel_patent_doc_number] =>)
12/643745
LIFT FAN SYSTEM Dec 20, 2009 Abandoned
Array ( [id] => 6455524 [patent_doc_number] => 20100090068 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2010-04-15 [patent_title] => 'AIRCRAFT WITH WINGS WHOSE MAXIMUM LIFT CAN BE ALTERED BY CONTROLLABLE WING COMPONENTS' [patent_app_type] => utility [patent_app_number] => 12/640559 [patent_app_country] => US [patent_app_date] => 2009-12-17 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 3 [patent_figures_cnt] => 3 [patent_no_of_words] => 2461 [patent_no_of_claims] => 14 [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/A1/0090/20100090068.pdf [firstpage_image] =>[orig_patent_app_number] => 12640559 [rel_patent_id] =>[rel_patent_doc_number] =>)
12/640559
AIRCRAFT WITH WINGS WHOSE MAXIMUM LIFT CAN BE ALTERED BY CONTROLLABLE WING COMPONENTS Dec 16, 2009 Abandoned
Array ( [id] => 6398606 [patent_doc_number] => 20100147995 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2010-06-17 [patent_title] => 'AIRCRAFT UNDERCARRIAGE WITH MOTORIZATION AND TRANSMISSION' [patent_app_type] => utility [patent_app_number] => 12/637516 [patent_app_country] => US [patent_app_date] => 2009-12-14 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 4 [patent_figures_cnt] => 4 [patent_no_of_words] => 4780 [patent_no_of_claims] => 12 [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/A1/0147/20100147995.pdf [firstpage_image] =>[orig_patent_app_number] => 12637516 [rel_patent_id] =>[rel_patent_doc_number] =>)
12/637516
Aircraft undercarriage with motorization and transmission Dec 13, 2009 Issued
Array ( [id] => 9111551 [patent_doc_number] => 08567713 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2013-10-29 [patent_title] => 'Lift fan clutch' [patent_app_type] => utility [patent_app_number] => 12/635525 [patent_app_country] => US [patent_app_date] => 2009-12-10 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 4 [patent_figures_cnt] => 6 [patent_no_of_words] => 3699 [patent_no_of_claims] => 9 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 429 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 12635525 [rel_patent_id] =>[rel_patent_doc_number] =>)
12/635525
Lift fan clutch Dec 9, 2009 Issued
12/634926 PRESSURE ACTIVATED INERTIALLY LOCKING BASE FOR PROJECTILES Dec 9, 2009 Abandoned
Array ( [id] => 6476447 [patent_doc_number] => 20100213314 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2010-08-26 [patent_title] => 'ARRANGEMENT FOR INSTALLING ELECTRIC CABLES IN THE FLOOR REGION OF AN AIRCRAFT' [patent_app_type] => utility [patent_app_number] => 12/629171 [patent_app_country] => US [patent_app_date] => 2009-12-02 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 3 [patent_figures_cnt] => 3 [patent_no_of_words] => 2872 [patent_no_of_claims] => 18 [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/A1/0213/20100213314.pdf [firstpage_image] =>[orig_patent_app_number] => 12629171 [rel_patent_id] =>[rel_patent_doc_number] =>)
12/629171
Arrangement for installing electric cables in the floor region of an aircraft Dec 1, 2009 Issued
Array ( [id] => 8857071 [patent_doc_number] => 08459596 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2013-06-11 [patent_title] => 'Sky/space elevators' [patent_app_type] => utility [patent_app_number] => 12/592655 [patent_app_country] => US [patent_app_date] => 2009-12-01 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 13 [patent_figures_cnt] => 16 [patent_no_of_words] => 2503 [patent_no_of_claims] => 7 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 214 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 12592655 [rel_patent_id] =>[rel_patent_doc_number] =>)
12/592655
Sky/space elevators Nov 30, 2009 Issued
Array ( [id] => 8662813 [patent_doc_number] => 08376269 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2013-02-19 [patent_title] => 'Hydraulic valve, a hybrid helicopter provided with such a hydraulic valve, and a method implemented by the hydraulic valve' [patent_app_type] => utility [patent_app_number] => 12/628406 [patent_app_country] => US [patent_app_date] => 2009-12-01 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 3 [patent_figures_cnt] => 6 [patent_no_of_words] => 8312 [patent_no_of_claims] => 13 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 154 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 12628406 [rel_patent_id] =>[rel_patent_doc_number] =>)
12/628406
Hydraulic valve, a hybrid helicopter provided with such a hydraulic valve, and a method implemented by the hydraulic valve Nov 30, 2009 Issued
Array ( [id] => 8375646 [patent_doc_number] => 08258447 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2012-09-04 [patent_title] => 'Methods and apparatus for a frangible seal for deployable flight structures' [patent_app_type] => utility [patent_app_number] => 12/628610 [patent_app_country] => US [patent_app_date] => 2009-12-01 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 2 [patent_figures_cnt] => 4 [patent_no_of_words] => 1559 [patent_no_of_claims] => 20 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 86 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 12628610 [rel_patent_id] =>[rel_patent_doc_number] =>)
12/628610
Methods and apparatus for a frangible seal for deployable flight structures Nov 30, 2009 Issued
Array ( [id] => 9045635 [patent_doc_number] => 08540186 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2013-09-24 [patent_title] => 'Rigid aircraft pylon structure in contact with a fuselage lateral extension for attachment' [patent_app_type] => utility [patent_app_number] => 13/131950 [patent_app_country] => US [patent_app_date] => 2009-11-30 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 6 [patent_figures_cnt] => 7 [patent_no_of_words] => 4185 [patent_no_of_claims] => 10 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 187 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13131950 [rel_patent_id] =>[rel_patent_doc_number] =>)
13/131950
Rigid aircraft pylon structure in contact with a fuselage lateral extension for attachment Nov 29, 2009 Issued
Array ( [id] => 6430572 [patent_doc_number] => 20100187354 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2010-07-29 [patent_title] => 'INFORMATION SYSTEM FOR MESSAGES FROM PASSENGERS TO THE CABIN CREW' [patent_app_type] => utility [patent_app_number] => 12/627205 [patent_app_country] => US [patent_app_date] => 2009-11-30 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 4 [patent_figures_cnt] => 4 [patent_no_of_words] => 1321 [patent_no_of_claims] => 7 [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/A1/0187/20100187354.pdf [firstpage_image] =>[orig_patent_app_number] => 12627205 [rel_patent_id] =>[rel_patent_doc_number] =>)
12/627205
INFORMATION SYSTEM FOR MESSAGES FROM PASSENGERS TO THE CABIN CREW Nov 29, 2009 Abandoned
Array ( [id] => 6177030 [patent_doc_number] => 20110121130 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2011-05-26 [patent_title] => 'BLENDED WING BODY CARGO AIRPLANE' [patent_app_type] => utility [patent_app_number] => 12/623404 [patent_app_country] => US [patent_app_date] => 2009-11-21 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 12 [patent_figures_cnt] => 12 [patent_no_of_words] => 9921 [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/A1/0121/20110121130.pdf [firstpage_image] =>[orig_patent_app_number] => 12623404 [rel_patent_id] =>[rel_patent_doc_number] =>)
12/623404
Blended wing body cargo airplane Nov 20, 2009 Issued
Array ( [id] => 8559286 [patent_doc_number] => 08333346 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2012-12-18 [patent_title] => 'Sky station' [patent_app_type] => utility [patent_app_number] => 12/592031 [patent_app_country] => US [patent_app_date] => 2009-11-18 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 17 [patent_figures_cnt] => 17 [patent_no_of_words] => 5556 [patent_no_of_claims] => 8 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 192 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 12592031 [rel_patent_id] =>[rel_patent_doc_number] =>)
12/592031
Sky station Nov 17, 2009 Issued
Array ( [id] => 6407578 [patent_doc_number] => 20100140418 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2010-06-10 [patent_title] => 'Air Induction Control' [patent_app_type] => utility [patent_app_number] => 12/619028 [patent_app_country] => US [patent_app_date] => 2009-11-16 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 13 [patent_figures_cnt] => 13 [patent_no_of_words] => 4130 [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/A1/0140/20100140418.pdf [firstpage_image] =>[orig_patent_app_number] => 12619028 [rel_patent_id] =>[rel_patent_doc_number] =>)
12/619028
Air induction control Nov 15, 2009 Issued
Array ( [id] => 8967041 [patent_doc_number] => 08505849 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2013-08-13 [patent_title] => 'Device for retracting aircraft landing gear' [patent_app_type] => utility [patent_app_number] => 13/125717 [patent_app_country] => US [patent_app_date] => 2009-11-10 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 3 [patent_figures_cnt] => 5 [patent_no_of_words] => 2814 [patent_no_of_claims] => 4 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 183 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13125717 [rel_patent_id] =>[rel_patent_doc_number] =>)
13/125717
Device for retracting aircraft landing gear Nov 9, 2009 Issued
Array ( [id] => 9152093 [patent_doc_number] => 08584991 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2013-11-19 [patent_title] => 'Vane having a regulating flap and a gap covering device and an adjusting mechanism for a gap covering device' [patent_app_type] => utility [patent_app_number] => 13/128242 [patent_app_country] => US [patent_app_date] => 2009-11-10 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 2 [patent_figures_cnt] => 4 [patent_no_of_words] => 4195 [patent_no_of_claims] => 12 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 197 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13128242 [rel_patent_id] =>[rel_patent_doc_number] =>)
13/128242
Vane having a regulating flap and a gap covering device and an adjusting mechanism for a gap covering device Nov 9, 2009 Issued
Array ( [id] => 9467190 [patent_doc_number] => 08720816 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2014-05-13 [patent_title] => 'Unmanned aerial vehicle' [patent_app_type] => utility [patent_app_number] => 13/130481 [patent_app_country] => US [patent_app_date] => 2009-11-10 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 1 [patent_figures_cnt] => 2 [patent_no_of_words] => 6380 [patent_no_of_claims] => 15 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 73 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13130481 [rel_patent_id] =>[rel_patent_doc_number] =>)
13/130481
Unmanned aerial vehicle Nov 9, 2009 Issued
Array ( [id] => 8805932 [patent_doc_number] => 08443575 [patent_country] => US [patent_kind] => B1 [patent_issue_date] => 2013-05-21 [patent_title] => 'Composite access door' [patent_app_type] => utility [patent_app_number] => 12/606331 [patent_app_country] => US [patent_app_date] => 2009-10-27 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 9 [patent_figures_cnt] => 23 [patent_no_of_words] => 4620 [patent_no_of_claims] => 23 [patent_no_of_ind_claims] => 4 [patent_words_short_claim] => 68 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 12606331 [rel_patent_id] =>[rel_patent_doc_number] =>)
12/606331
Composite access door Oct 26, 2009 Issued
Array ( [id] => 4638201 [patent_doc_number] => 08016226 [patent_country] => US [patent_kind] => B1 [patent_issue_date] => 2011-09-13 [patent_title] => 'Vertical take off and landing aircraft system with energy recapture technology' [patent_app_type] => utility [patent_app_number] => 12/587286 [patent_app_country] => US [patent_app_date] => 2009-10-05 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 3 [patent_figures_cnt] => 6 [patent_no_of_words] => 5246 [patent_no_of_claims] => 1 [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/08/016/08016226.pdf [firstpage_image] =>[orig_patent_app_number] => 12587286 [rel_patent_id] =>[rel_patent_doc_number] =>)
12/587286
Vertical take off and landing aircraft system with energy recapture technology Oct 4, 2009 Issued
Array ( [id] => 9007813 [patent_doc_number] => 08523102 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2013-09-03 [patent_title] => 'Method and apparatus for aircraft sensor and actuator failure protection using reconfigurable flight control laws' [patent_app_type] => utility [patent_app_number] => 13/121458 [patent_app_country] => US [patent_app_date] => 2009-10-05 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 15 [patent_figures_cnt] => 23 [patent_no_of_words] => 6388 [patent_no_of_claims] => 19 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 96 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13121458 [rel_patent_id] =>[rel_patent_doc_number] =>)
13/121458
Method and apparatus for aircraft sensor and actuator failure protection using reconfigurable flight control laws Oct 4, 2009 Issued
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