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] => 5123323 [patent_doc_number] => 20070235593 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2007-10-11 [patent_title] => 'Flying control device for a rotorcraft' [patent_app_type] => utility [patent_app_number] => 11/730656 [patent_app_country] => US [patent_app_date] => 2007-04-03 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 2 [patent_figures_cnt] => 2 [patent_no_of_words] => 2970 [patent_no_of_claims] => 6 [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/A1/0235/20070235593.pdf [firstpage_image] =>[orig_patent_app_number] => 11730656 [rel_patent_id] =>[rel_patent_doc_number] =>)
11/730656
Flying control device for a rotorcraft Apr 2, 2007 Issued
Array ( [id] => 4626275 [patent_doc_number] => 08005583 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2011-08-23 [patent_title] => 'Method and device for determining the air turbulence likely to be encountered by an aircraft' [patent_app_type] => utility [patent_app_number] => 11/693191 [patent_app_country] => US [patent_app_date] => 2007-03-29 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 3 [patent_figures_cnt] => 3 [patent_no_of_words] => 4381 [patent_no_of_claims] => 19 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 223 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/08/005/08005583.pdf [firstpage_image] =>[orig_patent_app_number] => 11693191 [rel_patent_id] =>[rel_patent_doc_number] =>)
11/693191
Method and device for determining the air turbulence likely to be encountered by an aircraft Mar 28, 2007 Issued
Array ( [id] => 7810230 [patent_doc_number] => 08132759 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2012-03-13 [patent_title] => 'System and method for facilitating aerial refueling' [patent_app_type] => utility [patent_app_number] => 11/689280 [patent_app_country] => US [patent_app_date] => 2007-03-21 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 3 [patent_figures_cnt] => 3 [patent_no_of_words] => 2495 [patent_no_of_claims] => 7 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 382 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/08/132/08132759.pdf [firstpage_image] =>[orig_patent_app_number] => 11689280 [rel_patent_id] =>[rel_patent_doc_number] =>)
11/689280
System and method for facilitating aerial refueling Mar 20, 2007 Issued
Array ( [id] => 139610 [patent_doc_number] => 07690604 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2010-04-06 [patent_title] => 'Rudder pedal assembly including non-parallel slide rails' [patent_app_type] => utility [patent_app_number] => 11/688701 [patent_app_country] => US [patent_app_date] => 2007-03-20 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 6 [patent_figures_cnt] => 12 [patent_no_of_words] => 4118 [patent_no_of_claims] => 11 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 348 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/07/690/07690604.pdf [firstpage_image] =>[orig_patent_app_number] => 11688701 [rel_patent_id] =>[rel_patent_doc_number] =>)
11/688701
Rudder pedal assembly including non-parallel slide rails Mar 19, 2007 Issued
Array ( [id] => 4737003 [patent_doc_number] => 20080230655 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2008-09-25 [patent_title] => 'Air barrier for use with an expandable structure' [patent_app_type] => utility [patent_app_number] => 11/723237 [patent_app_country] => US [patent_app_date] => 2007-03-19 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 4 [patent_figures_cnt] => 4 [patent_no_of_words] => 1205 [patent_no_of_claims] => 9 [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/A1/0230/20080230655.pdf [firstpage_image] =>[orig_patent_app_number] => 11723237 [rel_patent_id] =>[rel_patent_doc_number] =>)
11/723237
Air barrier for use with an expandable structure Mar 18, 2007 Issued
Array ( [id] => 4816730 [patent_doc_number] => 20080223989 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2008-09-18 [patent_title] => 'Force Balancing Kite Control System' [patent_app_type] => utility [patent_app_number] => 11/686360 [patent_app_country] => US [patent_app_date] => 2007-03-15 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 6 [patent_figures_cnt] => 6 [patent_no_of_words] => 3510 [patent_no_of_claims] => 5 [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/A1/0223/20080223989.pdf [firstpage_image] =>[orig_patent_app_number] => 11686360 [rel_patent_id] =>[rel_patent_doc_number] =>)
11/686360
Force balancing kite control system Mar 14, 2007 Issued
Array ( [id] => 5217184 [patent_doc_number] => 20070158495 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2007-07-12 [patent_title] => 'High lift and high strength aerofoil' [patent_app_type] => utility [patent_app_number] => 11/717283 [patent_app_country] => US [patent_app_date] => 2007-03-14 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 7 [patent_figures_cnt] => 7 [patent_no_of_words] => 739 [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/A1/0158/20070158495.pdf [firstpage_image] =>[orig_patent_app_number] => 11717283 [rel_patent_id] =>[rel_patent_doc_number] =>)
11/717283
High lift and high strength aerofoil Mar 13, 2007 Abandoned
Array ( [id] => 4816721 [patent_doc_number] => 20080223980 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2008-09-18 [patent_title] => 'BUBBLE GLIDER' [patent_app_type] => utility [patent_app_number] => 11/685233 [patent_app_country] => US [patent_app_date] => 2007-03-13 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 2 [patent_figures_cnt] => 2 [patent_no_of_words] => 1546 [patent_no_of_claims] => 11 [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/A1/0223/20080223980.pdf [firstpage_image] =>[orig_patent_app_number] => 11685233 [rel_patent_id] =>[rel_patent_doc_number] =>)
11/685233
BUBBLE GLIDER Mar 12, 2007 Abandoned
Array ( [id] => 6239661 [patent_doc_number] => 20100133379 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2010-06-03 [patent_title] => 'Landing gear strut extender' [patent_app_type] => utility [patent_app_number] => 11/717904 [patent_app_country] => US [patent_app_date] => 2007-03-13 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 2 [patent_figures_cnt] => 2 [patent_no_of_words] => 1232 [patent_no_of_claims] => 17 [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/A1/0133/20100133379.pdf [firstpage_image] =>[orig_patent_app_number] => 11717904 [rel_patent_id] =>[rel_patent_doc_number] =>)
11/717904
Landing gear strut extender Mar 12, 2007 Issued
Array ( [id] => 4628055 [patent_doc_number] => 08006932 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2011-08-30 [patent_title] => 'Pivoting coupling system for a large dihedral empennage to the tail fuselage of an aircraft' [patent_app_type] => utility [patent_app_number] => 11/711758 [patent_app_country] => US [patent_app_date] => 2007-02-28 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 16 [patent_figures_cnt] => 33 [patent_no_of_words] => 5346 [patent_no_of_claims] => 17 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 369 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/08/006/08006932.pdf [firstpage_image] =>[orig_patent_app_number] => 11711758 [rel_patent_id] =>[rel_patent_doc_number] =>)
11/711758
Pivoting coupling system for a large dihedral empennage to the tail fuselage of an aircraft Feb 27, 2007 Issued
Array ( [id] => 4723677 [patent_doc_number] => 20080203218 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2008-08-28 [patent_title] => 'Systems And Methods For Reducing Pressure Loss Of Air Flowing From A First Area To A Second Area' [patent_app_type] => utility [patent_app_number] => 11/678899 [patent_app_country] => US [patent_app_date] => 2007-02-26 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 7 [patent_figures_cnt] => 7 [patent_no_of_words] => 2848 [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/A1/0203/20080203218.pdf [firstpage_image] =>[orig_patent_app_number] => 11678899 [rel_patent_id] =>[rel_patent_doc_number] =>)
11/678899
Systems And Methods For Reducing Pressure Loss Of Air Flowing From A First Area To A Second Area Feb 25, 2007 Abandoned
Array ( [id] => 11800276 [patent_doc_number] => 09541106 [patent_country] => US [patent_kind] => B1 [patent_issue_date] => 2017-01-10 [patent_title] => 'Plasma optimized aerostructures for efficient flow control' [patent_app_type] => utility [patent_app_number] => 11/710750 [patent_app_country] => US [patent_app_date] => 2007-02-26 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 9 [patent_figures_cnt] => 9 [patent_no_of_words] => 7922 [patent_no_of_claims] => 20 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 102 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 11710750 [rel_patent_id] =>[rel_patent_doc_number] =>)
11/710750
Plasma optimized aerostructures for efficient flow control Feb 25, 2007 Issued
Array ( [id] => 7758971 [patent_doc_number] => 08113469 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2012-02-14 [patent_title] => 'Passive micro-roughness array for drag modification' [patent_app_type] => utility [patent_app_number] => 11/708897 [patent_app_country] => US [patent_app_date] => 2007-02-21 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 7 [patent_figures_cnt] => 14 [patent_no_of_words] => 6991 [patent_no_of_claims] => 40 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 192 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/08/113/08113469.pdf [firstpage_image] =>[orig_patent_app_number] => 11708897 [rel_patent_id] =>[rel_patent_doc_number] =>)
11/708897
Passive micro-roughness array for drag modification Feb 20, 2007 Issued
Array ( [id] => 4648533 [patent_doc_number] => 20080035788 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2008-02-14 [patent_title] => 'Cellular support structures used for controlled actuation of fluid contact surfaces' [patent_app_type] => utility [patent_app_number] => 11/707052 [patent_app_country] => US [patent_app_date] => 2007-02-16 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 14 [patent_figures_cnt] => 14 [patent_no_of_words] => 6599 [patent_no_of_claims] => 30 [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/A1/0035/20080035788.pdf [firstpage_image] =>[orig_patent_app_number] => 11707052 [rel_patent_id] =>[rel_patent_doc_number] =>)
11/707052
Cellular support structures used for controlled actuation of fluid contact surfaces Feb 15, 2007 Issued
Array ( [id] => 5123320 [patent_doc_number] => 20070235590 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2007-10-11 [patent_title] => 'VORTEX GENERATOR' [patent_app_type] => utility [patent_app_number] => 11/669463 [patent_app_country] => US [patent_app_date] => 2007-01-31 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 10 [patent_figures_cnt] => 10 [patent_no_of_words] => 4666 [patent_no_of_claims] => 19 [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/A1/0235/20070235590.pdf [firstpage_image] =>[orig_patent_app_number] => 11669463 [rel_patent_id] =>[rel_patent_doc_number] =>)
11/669463
VORTEX GENERATOR Jan 30, 2007 Abandoned
Array ( [id] => 4843045 [patent_doc_number] => 20080179453 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2008-07-31 [patent_title] => 'Modular airship system and method' [patent_app_type] => utility [patent_app_number] => 11/698969 [patent_app_country] => US [patent_app_date] => 2007-01-26 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 7 [patent_figures_cnt] => 7 [patent_no_of_words] => 3490 [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/A1/0179/20080179453.pdf [firstpage_image] =>[orig_patent_app_number] => 11698969 [rel_patent_id] =>[rel_patent_doc_number] =>)
11/698969
Modular airship system and method Jan 25, 2007 Abandoned
Array ( [id] => 4654722 [patent_doc_number] => 20080023582 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2008-01-31 [patent_title] => 'Composite anti-crash structure with controlled buckling for an aircraft' [patent_app_type] => utility [patent_app_number] => 11/698020 [patent_app_country] => US [patent_app_date] => 2007-01-26 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 7 [patent_figures_cnt] => 7 [patent_no_of_words] => 5547 [patent_no_of_claims] => 15 [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/A1/0023/20080023582.pdf [firstpage_image] =>[orig_patent_app_number] => 11698020 [rel_patent_id] =>[rel_patent_doc_number] =>)
11/698020
Composite anti-crash structure with controlled buckling for an aircraft Jan 25, 2007 Issued
Array ( [id] => 4556101 [patent_doc_number] => 07857260 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2010-12-28 [patent_title] => 'Fuel jettison system' [patent_app_type] => utility [patent_app_number] => 11/624754 [patent_app_country] => US [patent_app_date] => 2007-01-19 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 3 [patent_figures_cnt] => 3 [patent_no_of_words] => 2655 [patent_no_of_claims] => 19 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 88 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/07/857/07857260.pdf [firstpage_image] =>[orig_patent_app_number] => 11624754 [rel_patent_id] =>[rel_patent_doc_number] =>)
11/624754
Fuel jettison system Jan 18, 2007 Issued
Array ( [id] => 5110257 [patent_doc_number] => 20070194172 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2007-08-23 [patent_title] => 'AIRCRAFT SHOCK STRUT HAVING IMPROVED CYLINDER AND BEARINGS' [patent_app_type] => utility [patent_app_number] => 11/622958 [patent_app_country] => US [patent_app_date] => 2007-01-12 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 5 [patent_figures_cnt] => 5 [patent_no_of_words] => 4329 [patent_no_of_claims] => 21 [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/A1/0194/20070194172.pdf [firstpage_image] =>[orig_patent_app_number] => 11622958 [rel_patent_id] =>[rel_patent_doc_number] =>)
11/622958
AIRCRAFT SHOCK STRUT HAVING IMPROVED CYLINDER AND BEARINGS Jan 11, 2007 Abandoned
Array ( [id] => 9322212 [patent_doc_number] => 08657226 [patent_country] => US [patent_kind] => B1 [patent_issue_date] => 2014-02-25 [patent_title] => 'Efficient control and stall prevention in advanced configuration aircraft' [patent_app_type] => utility [patent_app_number] => 11/623042 [patent_app_country] => US [patent_app_date] => 2007-01-12 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 15 [patent_figures_cnt] => 27 [patent_no_of_words] => 11373 [patent_no_of_claims] => 17 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 457 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 11623042 [rel_patent_id] =>[rel_patent_doc_number] =>)
11/623042
Efficient control and stall prevention in advanced configuration aircraft Jan 11, 2007 Issued
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