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] => 8268971 [patent_doc_number] => 08210468 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2012-07-03 [patent_title] => 'Aircraft stabilizer system and methods of using the same' [patent_app_type] => utility [patent_app_number] => 12/152661 [patent_app_country] => US [patent_app_date] => 2008-05-14 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 15 [patent_figures_cnt] => 26 [patent_no_of_words] => 6551 [patent_no_of_claims] => 15 [patent_no_of_ind_claims] => 4 [patent_words_short_claim] => 135 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 12152661 [rel_patent_id] =>[rel_patent_doc_number] =>)
12/152661
Aircraft stabilizer system and methods of using the same May 13, 2008 Issued
Array ( [id] => 9045639 [patent_doc_number] => 08540190 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2013-09-24 [patent_title] => 'Connecting arrangement comprising a coupling element and two curved ribs of an aircraft or spacecraft' [patent_app_type] => utility [patent_app_number] => 12/597027 [patent_app_country] => US [patent_app_date] => 2008-05-02 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 5 [patent_figures_cnt] => 6 [patent_no_of_words] => 2905 [patent_no_of_claims] => 8 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 143 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 12597027 [rel_patent_id] =>[rel_patent_doc_number] =>)
12/597027
Connecting arrangement comprising a coupling element and two curved ribs of an aircraft or spacecraft May 1, 2008 Issued
Array ( [id] => 6546428 [patent_doc_number] => 20100127122 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2010-05-27 [patent_title] => 'COMPOSITE STRUCTURE COMPRISING A STRINGER WITH A PAD EMBEDDED IN THE RECESS OF A PANEL AND METHOD OF TRANSMITTING FORCES' [patent_app_type] => utility [patent_app_number] => 12/451178 [patent_app_country] => US [patent_app_date] => 2008-04-15 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 5 [patent_figures_cnt] => 5 [patent_no_of_words] => 2682 [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/A1/0127/20100127122.pdf [firstpage_image] =>[orig_patent_app_number] => 12451178 [rel_patent_id] =>[rel_patent_doc_number] =>)
12/451178
Composite structure comprising a stringer with a pad embedded in the recess of a panel and method of transmitting forces Apr 14, 2008 Issued
Array ( [id] => 10874743 [patent_doc_number] => 08899523 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2014-12-02 [patent_title] => 'Fire protection space for aircraft passengers provided with the aid of fuselage skin of fibre-metal laminates' [patent_app_type] => utility [patent_app_number] => 12/595227 [patent_app_country] => US [patent_app_date] => 2008-04-14 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 4 [patent_figures_cnt] => 7 [patent_no_of_words] => 3096 [patent_no_of_claims] => 11 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 186 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 12595227 [rel_patent_id] =>[rel_patent_doc_number] =>)
12/595227
Fire protection space for aircraft passengers provided with the aid of fuselage skin of fibre-metal laminates Apr 13, 2008 Issued
Array ( [id] => 8456561 [patent_doc_number] => 08292223 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2012-10-23 [patent_title] => 'Securing emergency and safety equipment on aircraft' [patent_app_type] => utility [patent_app_number] => 12/059891 [patent_app_country] => US [patent_app_date] => 2008-03-31 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 10 [patent_figures_cnt] => 20 [patent_no_of_words] => 7774 [patent_no_of_claims] => 10 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 120 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 12059891 [rel_patent_id] =>[rel_patent_doc_number] =>)
12/059891
Securing emergency and safety equipment on aircraft Mar 30, 2008 Issued
Array ( [id] => 8628298 [patent_doc_number] => 08360362 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2013-01-29 [patent_title] => 'Aircraft floor and method of assembly' [patent_app_type] => utility [patent_app_number] => 12/056456 [patent_app_country] => US [patent_app_date] => 2008-03-27 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 12 [patent_figures_cnt] => 23 [patent_no_of_words] => 9410 [patent_no_of_claims] => 11 [patent_no_of_ind_claims] => 1 [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] => 12056456 [rel_patent_id] =>[rel_patent_doc_number] =>)
12/056456
Aircraft floor and method of assembly Mar 26, 2008 Issued
Array ( [id] => 8954055 [patent_doc_number] => 08499822 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2013-08-06 [patent_title] => 'System for cooling and adjusting the temperature of apparatuses in the propulsion assembly of an aircraft' [patent_app_type] => utility [patent_app_number] => 12/532696 [patent_app_country] => US [patent_app_date] => 2008-03-25 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 3 [patent_figures_cnt] => 6 [patent_no_of_words] => 3103 [patent_no_of_claims] => 10 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 145 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 12532696 [rel_patent_id] =>[rel_patent_doc_number] =>)
12/532696
System for cooling and adjusting the temperature of apparatuses in the propulsion assembly of an aircraft Mar 24, 2008 Issued
Array ( [id] => 5530450 [patent_doc_number] => 20090230238 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2009-09-17 [patent_title] => 'Aircraft fuselage structure' [patent_app_type] => utility [patent_app_number] => 12/077121 [patent_app_country] => US [patent_app_date] => 2008-03-17 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 3 [patent_figures_cnt] => 3 [patent_no_of_words] => 1455 [patent_no_of_claims] => 14 [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/A1/0230/20090230238.pdf [firstpage_image] =>[orig_patent_app_number] => 12077121 [rel_patent_id] =>[rel_patent_doc_number] =>)
12/077121
Aircraft fuselage structure Mar 16, 2008 Issued
Array ( [id] => 8553667 [patent_doc_number] => 08328134 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2012-12-11 [patent_title] => 'Connection element for power transmission between a flap actuator and a flap mounted on a wing of an aircraft so as to swivel' [patent_app_type] => utility [patent_app_number] => 12/047863 [patent_app_country] => US [patent_app_date] => 2008-03-13 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 3 [patent_figures_cnt] => 3 [patent_no_of_words] => 2085 [patent_no_of_claims] => 14 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 281 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 12047863 [rel_patent_id] =>[rel_patent_doc_number] =>)
12/047863
Connection element for power transmission between a flap actuator and a flap mounted on a wing of an aircraft so as to swivel Mar 12, 2008 Issued
Array ( [id] => 7533850 [patent_doc_number] => 08047472 [patent_country] => US [patent_kind] => B1 [patent_issue_date] => 2011-11-01 [patent_title] => 'Ram booster' [patent_app_type] => utility [patent_app_number] => 12/045970 [patent_app_country] => US [patent_app_date] => 2008-03-11 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 6 [patent_figures_cnt] => 8 [patent_no_of_words] => 5034 [patent_no_of_claims] => 7 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 167 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/08/047/08047472.pdf [firstpage_image] =>[orig_patent_app_number] => 12045970 [rel_patent_id] =>[rel_patent_doc_number] =>)
12/045970
Ram booster Mar 10, 2008 Issued
Array ( [id] => 4714878 [patent_doc_number] => 20080237400 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2008-10-02 [patent_title] => 'Satellite refuelling system and method' [patent_app_type] => utility [patent_app_number] => 12/073795 [patent_app_country] => US [patent_app_date] => 2008-03-10 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 17 [patent_figures_cnt] => 17 [patent_no_of_words] => 9662 [patent_no_of_claims] => 35 [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/A1/0237/20080237400.pdf [firstpage_image] =>[orig_patent_app_number] => 12073795 [rel_patent_id] =>[rel_patent_doc_number] =>)
12/073795
Satellite refuelling system and method Mar 9, 2008 Issued
Array ( [id] => 8420364 [patent_doc_number] => 08276848 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2012-10-02 [patent_title] => 'Rib structure for torsion boxes of a wing or horizontal stabiliser of an aircraft' [patent_app_type] => utility [patent_app_number] => 12/044419 [patent_app_country] => US [patent_app_date] => 2008-03-07 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 6 [patent_figures_cnt] => 9 [patent_no_of_words] => 3217 [patent_no_of_claims] => 30 [patent_no_of_ind_claims] => 2 [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] => 12044419 [rel_patent_id] =>[rel_patent_doc_number] =>)
12/044419
Rib structure for torsion boxes of a wing or horizontal stabiliser of an aircraft Mar 6, 2008 Issued
Array ( [id] => 5382863 [patent_doc_number] => 20090224107 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2009-09-10 [patent_title] => 'Reduced Span Wings with Wing Tip Devices, and Associated Systems and Methods' [patent_app_type] => utility [patent_app_number] => 12/042174 [patent_app_country] => US [patent_app_date] => 2008-03-04 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 8 [patent_figures_cnt] => 8 [patent_no_of_words] => 5895 [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/A1/0224/20090224107.pdf [firstpage_image] =>[orig_patent_app_number] => 12042174 [rel_patent_id] =>[rel_patent_doc_number] =>)
12/042174
Reduced Span Wings with Wing Tip Devices, and Associated Systems and Methods Mar 3, 2008 Abandoned
Array ( [id] => 7709203 [patent_doc_number] => 08091834 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2012-01-10 [patent_title] => 'Multi-grommet retained slider for parachutes' [patent_app_type] => utility [patent_app_number] => 12/073206 [patent_app_country] => US [patent_app_date] => 2008-03-03 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 6 [patent_figures_cnt] => 21 [patent_no_of_words] => 7196 [patent_no_of_claims] => 20 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 163 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/08/091/08091834.pdf [firstpage_image] =>[orig_patent_app_number] => 12073206 [rel_patent_id] =>[rel_patent_doc_number] =>)
12/073206
Multi-grommet retained slider for parachutes Mar 2, 2008 Issued
Array ( [id] => 5419550 [patent_doc_number] => 20090146004 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2009-06-11 [patent_title] => 'Aircraft seating arrangement and seat' [patent_app_type] => utility [patent_app_number] => 12/039000 [patent_app_country] => US [patent_app_date] => 2008-02-28 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 10 [patent_figures_cnt] => 10 [patent_no_of_words] => 4133 [patent_no_of_claims] => 18 [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/A1/0146/20090146004.pdf [firstpage_image] =>[orig_patent_app_number] => 12039000 [rel_patent_id] =>[rel_patent_doc_number] =>)
12/039000
Aircraft seating arrangement and seat Feb 27, 2008 Abandoned
Array ( [id] => 4566852 [patent_doc_number] => 07832690 [patent_country] => US [patent_kind] => B1 [patent_issue_date] => 2010-11-16 [patent_title] => 'Telescoping wing locking system' [patent_app_type] => utility [patent_app_number] => 12/030077 [patent_app_country] => US [patent_app_date] => 2008-02-12 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 1 [patent_figures_cnt] => 1 [patent_no_of_words] => 2369 [patent_no_of_claims] => 17 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 243 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/07/832/07832690.pdf [firstpage_image] =>[orig_patent_app_number] => 12030077 [rel_patent_id] =>[rel_patent_doc_number] =>)
12/030077
Telescoping wing locking system Feb 11, 2008 Issued
Array ( [id] => 5572736 [patent_doc_number] => 20090140096 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2009-06-04 [patent_title] => 'Impact resistant aircraft fuselage' [patent_app_type] => utility [patent_app_number] => 12/012009 [patent_app_country] => US [patent_app_date] => 2008-01-30 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 3 [patent_figures_cnt] => 3 [patent_no_of_words] => 1658 [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/A1/0140/20090140096.pdf [firstpage_image] =>[orig_patent_app_number] => 12012009 [rel_patent_id] =>[rel_patent_doc_number] =>)
12/012009
Impact resistant aircraft fuselage Jan 29, 2008 Issued
Array ( [id] => 4638202 [patent_doc_number] => 08016227 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2011-09-13 [patent_title] => 'Non-handed engine cowl doors for fuselage mounted turbine engines' [patent_app_type] => utility [patent_app_number] => 12/020843 [patent_app_country] => US [patent_app_date] => 2008-01-28 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 3 [patent_figures_cnt] => 3 [patent_no_of_words] => 2803 [patent_no_of_claims] => 20 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 161 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/08/016/08016227.pdf [firstpage_image] =>[orig_patent_app_number] => 12020843 [rel_patent_id] =>[rel_patent_doc_number] =>)
12/020843
Non-handed engine cowl doors for fuselage mounted turbine engines Jan 27, 2008 Issued
Array ( [id] => 4477627 [patent_doc_number] => 07900874 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2011-03-08 [patent_title] => 'Device to move an object back and forth' [patent_app_type] => utility [patent_app_number] => 12/009852 [patent_app_country] => US [patent_app_date] => 2008-01-22 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 49 [patent_figures_cnt] => 56 [patent_no_of_words] => 31752 [patent_no_of_claims] => 9 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 89 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/07/900/07900874.pdf [firstpage_image] =>[orig_patent_app_number] => 12009852 [rel_patent_id] =>[rel_patent_doc_number] =>)
12/009852
Device to move an object back and forth Jan 21, 2008 Issued
Array ( [id] => 4762552 [patent_doc_number] => 20080173761 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2008-07-24 [patent_title] => 'Fitting for introducing high forces into a fuselage cell of an aircraft' [patent_app_type] => utility [patent_app_number] => 12/009149 [patent_app_country] => US [patent_app_date] => 2008-01-16 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 3 [patent_figures_cnt] => 3 [patent_no_of_words] => 2553 [patent_no_of_claims] => 12 [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/A1/0173/20080173761.pdf [firstpage_image] =>[orig_patent_app_number] => 12009149 [rel_patent_id] =>[rel_patent_doc_number] =>)
12/009149
Fitting for introducing high forces into a fuselage cell of an aircraft Jan 15, 2008 Issued
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