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] => 5868814 [patent_doc_number] => 20060163431 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2006-07-27 [patent_title] => 'Cover skin for a variable-shape aerodynamic area' [patent_app_type] => utility [patent_app_number] => 11/286834 [patent_app_country] => US [patent_app_date] => 2005-11-23 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 5 [patent_figures_cnt] => 5 [patent_no_of_words] => 3769 [patent_no_of_claims] => 28 [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/A1/0163/20060163431.pdf [firstpage_image] =>[orig_patent_app_number] => 11286834 [rel_patent_id] =>[rel_patent_doc_number] =>)
11/286834
Cover skin for a variable-shape aerodynamic area Nov 22, 2005 Issued
Array ( [id] => 5092720 [patent_doc_number] => 20070114329 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2007-05-24 [patent_title] => 'Aircraft trailing edge devices, including devices with non-parallel motion paths, and associated methods' [patent_app_type] => utility [patent_app_number] => 11/284247 [patent_app_country] => US [patent_app_date] => 2005-11-21 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 8 [patent_figures_cnt] => 8 [patent_no_of_words] => 6116 [patent_no_of_claims] => 25 [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/A1/0114/20070114329.pdf [firstpage_image] =>[orig_patent_app_number] => 11284247 [rel_patent_id] =>[rel_patent_doc_number] =>)
11/284247
Aircraft trailing edge devices, including devices with non-parallel motion paths, and associated methods Nov 20, 2005 Issued
Array ( [id] => 5628529 [patent_doc_number] => 20060144997 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2006-07-06 [patent_title] => 'Method and system for health monitoring of aircraft landing gear' [patent_app_type] => utility [patent_app_number] => 11/281504 [patent_app_country] => US [patent_app_date] => 2005-11-18 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 10 [patent_figures_cnt] => 10 [patent_no_of_words] => 6912 [patent_no_of_claims] => 50 [patent_no_of_ind_claims] => 7 [patent_words_short_claim] => 0 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] => publications/A1/0144/20060144997.pdf [firstpage_image] =>[orig_patent_app_number] => 11281504 [rel_patent_id] =>[rel_patent_doc_number] =>)
11/281504
Method and system for health monitoring of aircraft landing gear Nov 17, 2005 Abandoned
Array ( [id] => 149418 [patent_doc_number] => 07677492 [patent_country] => US [patent_kind] => B1 [patent_issue_date] => 2010-03-16 [patent_title] => 'Automatic mechanical control of rotor blade collective pitch' [patent_app_type] => utility [patent_app_number] => 11/280036 [patent_app_country] => US [patent_app_date] => 2005-11-16 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 5 [patent_figures_cnt] => 5 [patent_no_of_words] => 3519 [patent_no_of_claims] => 13 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 241 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/07/677/07677492.pdf [firstpage_image] =>[orig_patent_app_number] => 11280036 [rel_patent_id] =>[rel_patent_doc_number] =>)
11/280036
Automatic mechanical control of rotor blade collective pitch Nov 15, 2005 Issued
Array ( [id] => 4967275 [patent_doc_number] => 20070107277 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2007-05-17 [patent_title] => 'SEAT IDENTIFICATION SYSTEM' [patent_app_type] => utility [patent_app_number] => 11/164200 [patent_app_country] => US [patent_app_date] => 2005-11-14 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 4 [patent_figures_cnt] => 4 [patent_no_of_words] => 2566 [patent_no_of_claims] => 27 [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/A1/0107/20070107277.pdf [firstpage_image] =>[orig_patent_app_number] => 11164200 [rel_patent_id] =>[rel_patent_doc_number] =>)
11/164200
SEAT IDENTIFICATION SYSTEM Nov 13, 2005 Abandoned
Array ( [id] => 5031438 [patent_doc_number] => 20070095977 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2007-05-03 [patent_title] => 'Mesh fender for protecting an aircraft against damage from foreign objects' [patent_app_type] => utility [patent_app_number] => 11/263511 [patent_app_country] => US [patent_app_date] => 2005-10-31 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 7 [patent_figures_cnt] => 7 [patent_no_of_words] => 2857 [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/A1/0095/20070095977.pdf [firstpage_image] =>[orig_patent_app_number] => 11263511 [rel_patent_id] =>[rel_patent_doc_number] =>)
11/263511
Mesh fender for protecting an aircraft against damage from foreign objects Oct 30, 2005 Abandoned
Array ( [id] => 5031445 [patent_doc_number] => 20070095984 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2007-05-03 [patent_title] => 'Window assembly retaining system' [patent_app_type] => utility [patent_app_number] => 11/262361 [patent_app_country] => US [patent_app_date] => 2005-10-28 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 7 [patent_figures_cnt] => 7 [patent_no_of_words] => 2535 [patent_no_of_claims] => 29 [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/A1/0095/20070095984.pdf [firstpage_image] =>[orig_patent_app_number] => 11262361 [rel_patent_id] =>[rel_patent_doc_number] =>)
11/262361
Window assembly retaining system Oct 27, 2005 Issued
Array ( [id] => 5213491 [patent_doc_number] => 20070102571 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2007-05-10 [patent_title] => 'Airship for lifting heavy loads & methods of operation' [patent_app_type] => utility [patent_app_number] => 11/253753 [patent_app_country] => US [patent_app_date] => 2005-10-20 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 3 [patent_figures_cnt] => 3 [patent_no_of_words] => 5160 [patent_no_of_claims] => 24 [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/A1/0102/20070102571.pdf [firstpage_image] =>[orig_patent_app_number] => 11253753 [rel_patent_id] =>[rel_patent_doc_number] =>)
11/253753
Airship for lifting heavy loads & methods of operation Oct 19, 2005 Abandoned
Array ( [id] => 4896707 [patent_doc_number] => 20080116320 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2008-05-22 [patent_title] => 'Aircraft With Wings Whose Maximum Lift Can Be Altered By Controllable Wing Components' [patent_app_type] => utility [patent_app_number] => 11/663055 [patent_app_country] => US [patent_app_date] => 2005-09-21 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 3 [patent_figures_cnt] => 3 [patent_no_of_words] => 1747 [patent_no_of_claims] => 10 [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/A1/0116/20080116320.pdf [firstpage_image] =>[orig_patent_app_number] => 11663055 [rel_patent_id] =>[rel_patent_doc_number] =>)
11/663055
Aircraft With Wings Whose Maximum Lift Can Be Altered By Controllable Wing Components Sep 20, 2005 Abandoned
Array ( [id] => 372563 [patent_doc_number] => 07472865 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2009-01-06 [patent_title] => 'Dehumidification system for an airship' [patent_app_type] => utility [patent_app_number] => 11/228652 [patent_app_country] => US [patent_app_date] => 2005-09-15 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 3 [patent_figures_cnt] => 3 [patent_no_of_words] => 3804 [patent_no_of_claims] => 2 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 102 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/07/472/07472865.pdf [firstpage_image] =>[orig_patent_app_number] => 11228652 [rel_patent_id] =>[rel_patent_doc_number] =>)
11/228652
Dehumidification system for an airship Sep 14, 2005 Issued
Array ( [id] => 5222774 [patent_doc_number] => 20070252040 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2007-11-01 [patent_title] => 'Seal assemblies for use with drooped spoilers and other control surfaces on aircraft' [patent_app_type] => utility [patent_app_number] => 11/220446 [patent_app_country] => US [patent_app_date] => 2005-09-07 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 8 [patent_figures_cnt] => 8 [patent_no_of_words] => 3321 [patent_no_of_claims] => 23 [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/A1/0252/20070252040.pdf [firstpage_image] =>[orig_patent_app_number] => 11220446 [rel_patent_id] =>[rel_patent_doc_number] =>)
11/220446
Seal assemblies for use with drooped spoilers and other control surfaces on aircraft Sep 6, 2005 Issued
Array ( [id] => 4610300 [patent_doc_number] => 07988096 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2011-08-02 [patent_title] => 'Space manufacturing module system and method' [patent_app_type] => utility [patent_app_number] => 11/217649 [patent_app_country] => US [patent_app_date] => 2005-09-01 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 6 [patent_figures_cnt] => 6 [patent_no_of_words] => 6493 [patent_no_of_claims] => 14 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 188 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/07/988/07988096.pdf [firstpage_image] =>[orig_patent_app_number] => 11217649 [rel_patent_id] =>[rel_patent_doc_number] =>)
11/217649
Space manufacturing module system and method Aug 31, 2005 Issued
Array ( [id] => 5145412 [patent_doc_number] => 20070045466 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2007-03-01 [patent_title] => 'Foldable, lockable control surface and method of using same' [patent_app_type] => utility [patent_app_number] => 11/216355 [patent_app_country] => US [patent_app_date] => 2005-08-31 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 9 [patent_figures_cnt] => 9 [patent_no_of_words] => 4356 [patent_no_of_claims] => 22 [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/A1/0045/20070045466.pdf [firstpage_image] =>[orig_patent_app_number] => 11216355 [rel_patent_id] =>[rel_patent_doc_number] =>)
11/216355
Foldable, lockable control surface and method of using same Aug 30, 2005 Abandoned
Array ( [id] => 571462 [patent_doc_number] => 07448577 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2008-11-11 [patent_title] => 'Apparatus for providing velocity differential between parachute and payload to reduce shock load' [patent_app_type] => utility [patent_app_number] => 11/217848 [patent_app_country] => US [patent_app_date] => 2005-08-23 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 5 [patent_figures_cnt] => 5 [patent_no_of_words] => 3087 [patent_no_of_claims] => 2 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 443 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/07/448/07448577.pdf [firstpage_image] =>[orig_patent_app_number] => 11217848 [rel_patent_id] =>[rel_patent_doc_number] =>)
11/217848
Apparatus for providing velocity differential between parachute and payload to reduce shock load Aug 22, 2005 Issued
Array ( [id] => 5898009 [patent_doc_number] => 20060043242 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2006-03-02 [patent_title] => 'Aircraft flight control surface actuation system communication architecture' [patent_app_type] => utility [patent_app_number] => 11/207250 [patent_app_country] => US [patent_app_date] => 2005-08-19 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 4 [patent_figures_cnt] => 4 [patent_no_of_words] => 3997 [patent_no_of_claims] => 21 [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/A1/0043/20060043242.pdf [firstpage_image] =>[orig_patent_app_number] => 11207250 [rel_patent_id] =>[rel_patent_doc_number] =>)
11/207250
Aircraft flight control surface actuation system communication architecture Aug 18, 2005 Issued
Array ( [id] => 5227990 [patent_doc_number] => 20070290097 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2007-12-20 [patent_title] => 'Vertical take-off and landing aircraft' [patent_app_type] => utility [patent_app_number] => 11/206909 [patent_app_country] => US [patent_app_date] => 2005-08-19 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 14 [patent_figures_cnt] => 14 [patent_no_of_words] => 5979 [patent_no_of_claims] => 6 [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/A1/0290/20070290097.pdf [firstpage_image] =>[orig_patent_app_number] => 11206909 [rel_patent_id] =>[rel_patent_doc_number] =>)
11/206909
Vertical take-off and landing aircraft Aug 18, 2005 Abandoned
Array ( [id] => 200420 [patent_doc_number] => 07631839 [patent_country] => US [patent_kind] => B1 [patent_issue_date] => 2009-12-15 [patent_title] => 'Enhanced multiple instrument distributed aperture sensor' [patent_app_type] => utility [patent_app_number] => 11/205012 [patent_app_country] => US [patent_app_date] => 2005-08-17 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 7 [patent_figures_cnt] => 7 [patent_no_of_words] => 6088 [patent_no_of_claims] => 40 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 202 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/07/631/07631839.pdf [firstpage_image] =>[orig_patent_app_number] => 11205012 [rel_patent_id] =>[rel_patent_doc_number] =>)
11/205012
Enhanced multiple instrument distributed aperture sensor Aug 16, 2005 Issued
Array ( [id] => 5615745 [patent_doc_number] => 20060185277 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2006-08-24 [patent_title] => 'Modular platform system' [patent_app_type] => utility [patent_app_number] => 11/205347 [patent_app_country] => US [patent_app_date] => 2005-08-16 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 13 [patent_figures_cnt] => 13 [patent_no_of_words] => 4476 [patent_no_of_claims] => 37 [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/A1/0185/20060185277.pdf [firstpage_image] =>[orig_patent_app_number] => 11205347 [rel_patent_id] =>[rel_patent_doc_number] =>)
11/205347
Modular platform system Aug 15, 2005 Abandoned
Array ( [id] => 5151867 [patent_doc_number] => 20070034749 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2007-02-15 [patent_title] => 'Deployable airfoil assembly for aircraft' [patent_app_type] => utility [patent_app_number] => 11/202494 [patent_app_country] => US [patent_app_date] => 2005-08-12 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 7 [patent_figures_cnt] => 7 [patent_no_of_words] => 4453 [patent_no_of_claims] => 26 [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/A1/0034/20070034749.pdf [firstpage_image] =>[orig_patent_app_number] => 11202494 [rel_patent_id] =>[rel_patent_doc_number] =>)
11/202494
Deployable airfoil assembly for aircraft Aug 11, 2005 Abandoned
Array ( [id] => 5151862 [patent_doc_number] => 20070034744 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2007-02-15 [patent_title] => 'Multi-grommet retained slider for parachutes' [patent_app_type] => utility [patent_app_number] => 11/201186 [patent_app_country] => US [patent_app_date] => 2005-08-11 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 6 [patent_figures_cnt] => 6 [patent_no_of_words] => 6111 [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/A1/0034/20070034744.pdf [firstpage_image] =>[orig_patent_app_number] => 11201186 [rel_patent_id] =>[rel_patent_doc_number] =>)
11/201186
Multi-grommet retained slider for parachutes Aug 10, 2005 Issued
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