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 number | Title of the application | Filing Date | Status |
---|---|---|---|
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 |