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] => 10169041
[patent_doc_number] => 09199742
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2015-12-01
[patent_title] => 'Aircraft parachute with bowden cables energized by the dynamic shock of the canopy'
[patent_app_type] => utility
[patent_app_number] => 13/694334
[patent_app_country] => US
[patent_app_date] => 2012-11-21
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 9
[patent_figures_cnt] => 23
[patent_no_of_words] => 10943
[patent_no_of_claims] => 10
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 772
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13694334
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/694334 | Aircraft parachute with bowden cables energized by the dynamic shock of the canopy | Nov 20, 2012 | Issued |
Array
(
[id] => 9488082
[patent_doc_number] => 20140138488
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2014-05-22
[patent_title] => 'COUNTERBALANCE MECHANISM FOR BOTTOM-HINGED AIRCRAFT FUSELAGE DOORS'
[patent_app_type] => utility
[patent_app_number] => 13/682607
[patent_app_country] => US
[patent_app_date] => 2012-11-20
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 6
[patent_figures_cnt] => 6
[patent_no_of_words] => 2584
[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] =>[firstpage_image] =>[orig_patent_app_number] => 13682607
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/682607 | Counterbalance mechanism for bottom-hinged aircraft fuselage doors | Nov 19, 2012 | Issued |
Array
(
[id] => 9171374
[patent_doc_number] => 20130313358
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2013-11-28
[patent_title] => 'Tie Rod Lock'
[patent_app_type] => utility
[patent_app_number] => 13/678229
[patent_app_country] => US
[patent_app_date] => 2012-11-15
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 32
[patent_figures_cnt] => 32
[patent_no_of_words] => 5769
[patent_no_of_claims] => 20
[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] =>[firstpage_image] =>[orig_patent_app_number] => 13678229
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/678229 | Tie rod lock | Nov 14, 2012 | Issued |
Array
(
[id] => 9445484
[patent_doc_number] => 20140116652
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2014-05-01
[patent_title] => 'Passive Cooling of Transmission Using Mast Mounted Heat Pipes'
[patent_app_type] => utility
[patent_app_number] => 13/676954
[patent_app_country] => US
[patent_app_date] => 2012-11-14
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 13
[patent_figures_cnt] => 13
[patent_no_of_words] => 6786
[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] =>[firstpage_image] =>[orig_patent_app_number] => 13676954
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/676954 | Passive cooling of transmission using mast mounted heat pipes | Nov 13, 2012 | Issued |
Array
(
[id] => 10418359
[patent_doc_number] => 20150303369
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2015-10-22
[patent_title] => 'DE-ICING ARRANGEMENT AND METHOD FOR DE-ICING A STRUCTURAL ELEMENT'
[patent_app_type] => utility
[patent_app_number] => 14/441017
[patent_app_country] => US
[patent_app_date] => 2012-11-08
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 6
[patent_figures_cnt] => 6
[patent_no_of_words] => 6013
[patent_no_of_claims] => 15
[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] =>[firstpage_image] =>[orig_patent_app_number] => 14441017
[rel_patent_id] =>[rel_patent_doc_number] =>) 14/441017 | De-icing arrangement and method for de-icing a structural element | Nov 7, 2012 | Issued |
Array
(
[id] => 10332867
[patent_doc_number] => 20150217871
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2015-08-06
[patent_title] => 'ANCHORING HARPOON AND ASSOCIATED ANCHORING METHOD'
[patent_app_type] => utility
[patent_app_number] => 13/824655
[patent_app_country] => US
[patent_app_date] => 2012-11-08
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 8
[patent_figures_cnt] => 8
[patent_no_of_words] => 5440
[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] =>[firstpage_image] =>[orig_patent_app_number] => 13824655
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/824655 | Anchoring harpoon and associated anchoring method | Nov 7, 2012 | Issued |
Array
(
[id] => 8811762
[patent_doc_number] => 20130112807
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2013-05-09
[patent_title] => 'METHOD FOR REDUCING AIRCRAFT MAINTENANCE COSTS AND TIME OUT OF SERVICE'
[patent_app_type] => utility
[patent_app_number] => 13/671561
[patent_app_country] => US
[patent_app_date] => 2012-11-08
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 2
[patent_figures_cnt] => 2
[patent_no_of_words] => 5443
[patent_no_of_claims] => 12
[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] =>[firstpage_image] =>[orig_patent_app_number] => 13671561
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/671561 | METHOD FOR REDUCING AIRCRAFT MAINTENANCE COSTS AND TIME OUT OF SERVICE | Nov 7, 2012 | Abandoned |
Array
(
[id] => 9316309
[patent_doc_number] => 20140048647
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2014-02-20
[patent_title] => 'AMPHIBIOUS AIRCRAFT'
[patent_app_type] => utility
[patent_app_number] => 13/667874
[patent_app_country] => US
[patent_app_date] => 2012-11-02
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 7
[patent_figures_cnt] => 7
[patent_no_of_words] => 3938
[patent_no_of_claims] => 22
[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] =>[firstpage_image] =>[orig_patent_app_number] => 13667874
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/667874 | Amphibious aircraft | Nov 1, 2012 | Issued |
Array
(
[id] => 8788657
[patent_doc_number] => 20130105626
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2013-05-02
[patent_title] => 'CHANGING CUBICLE IN AN AIRCRAFT AND METHOD FOR RETROFITTING AN AIRCRAFT WITH A CHANGING CUBICLE'
[patent_app_type] => utility
[patent_app_number] => 13/662440
[patent_app_country] => US
[patent_app_date] => 2012-10-27
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 7
[patent_figures_cnt] => 7
[patent_no_of_words] => 2490
[patent_no_of_claims] => 16
[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] =>[firstpage_image] =>[orig_patent_app_number] => 13662440
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/662440 | CHANGING CUBICLE IN AN AIRCRAFT AND METHOD FOR RETROFITTING AN AIRCRAFT WITH A CHANGING CUBICLE | Oct 26, 2012 | Abandoned |
Array
(
[id] => 8960606
[patent_doc_number] => 20130200208
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2013-08-08
[patent_title] => 'CHORD-EXPANDING AIR VEHICLE WINGS'
[patent_app_type] => utility
[patent_app_number] => 13/660209
[patent_app_country] => US
[patent_app_date] => 2012-10-25
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 6
[patent_figures_cnt] => 6
[patent_no_of_words] => 2773
[patent_no_of_claims] => 20
[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] =>[firstpage_image] =>[orig_patent_app_number] => 13660209
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/660209 | Chord-expanding air vehicle wings | Oct 24, 2012 | Issued |
Array
(
[id] => 9646930
[patent_doc_number] => 08800934
[patent_country] => US
[patent_kind] => B1
[patent_issue_date] => 2014-08-12
[patent_title] => 'Space access system with reusable booster'
[patent_app_type] => utility
[patent_app_number] => 13/659697
[patent_app_country] => US
[patent_app_date] => 2012-10-24
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 9
[patent_figures_cnt] => 9
[patent_no_of_words] => 5498
[patent_no_of_claims] => 21
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 97
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13659697
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/659697 | Space access system with reusable booster | Oct 23, 2012 | Issued |
Array
(
[id] => 8775955
[patent_doc_number] => 20130097930
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2013-04-25
[patent_title] => 'AIRCRAFT HATCH EMERGENCY OPENING ACTUATOR INCLUDING OPENING DELAY MEANS'
[patent_app_type] => utility
[patent_app_number] => 13/656229
[patent_app_country] => US
[patent_app_date] => 2012-10-19
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
[patent_figures_cnt] => 5
[patent_no_of_words] => 6240
[patent_no_of_claims] => 20
[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] =>[firstpage_image] =>[orig_patent_app_number] => 13656229
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/656229 | Aircraft hatch emergency opening actuator including opening delay means | Oct 18, 2012 | Issued |
Array
(
[id] => 9880799
[patent_doc_number] => 08967552
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2015-03-03
[patent_title] => 'Direct-drive control of aircraft stability augmentation'
[patent_app_type] => utility
[patent_app_number] => 13/655778
[patent_app_country] => US
[patent_app_date] => 2012-10-19
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 4
[patent_no_of_words] => 2565
[patent_no_of_claims] => 17
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 114
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13655778
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/655778 | Direct-drive control of aircraft stability augmentation | Oct 18, 2012 | Issued |
Array
(
[id] => 8788655
[patent_doc_number] => 20130105624
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2013-05-02
[patent_title] => 'LANDING GEAR, AN AIRCRAFT, AND A METHOD'
[patent_app_type] => utility
[patent_app_number] => 13/654603
[patent_app_country] => US
[patent_app_date] => 2012-10-18
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 3
[patent_no_of_words] => 6056
[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] =>[firstpage_image] =>[orig_patent_app_number] => 13654603
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/654603 | Landing gear, an aircraft, and a method | Oct 17, 2012 | Issued |
Array
(
[id] => 8788655
[patent_doc_number] => 20130105624
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2013-05-02
[patent_title] => 'LANDING GEAR, AN AIRCRAFT, AND A METHOD'
[patent_app_type] => utility
[patent_app_number] => 13/654603
[patent_app_country] => US
[patent_app_date] => 2012-10-18
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 3
[patent_no_of_words] => 6056
[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] =>[firstpage_image] =>[orig_patent_app_number] => 13654603
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/654603 | Landing gear, an aircraft, and a method | Oct 17, 2012 | Issued |
Array
(
[id] => 8788655
[patent_doc_number] => 20130105624
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2013-05-02
[patent_title] => 'LANDING GEAR, AN AIRCRAFT, AND A METHOD'
[patent_app_type] => utility
[patent_app_number] => 13/654603
[patent_app_country] => US
[patent_app_date] => 2012-10-18
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 3
[patent_no_of_words] => 6056
[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] =>[firstpage_image] =>[orig_patent_app_number] => 13654603
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/654603 | Landing gear, an aircraft, and a method | Oct 17, 2012 | Issued |
Array
(
[id] => 9117933
[patent_doc_number] => 20130284855
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2013-10-31
[patent_title] => 'GUIDING MECHANISM FOR OPENING AND CLOSING A CARGO DOOR OF AN AIRCRAFT, AIRCRAFT WITH SUCH A GUIDING MECHANISM AND METHOD FOR OPENING AND CLOSING A CARGO DOOR OF AN AIRCRAFT'
[patent_app_type] => utility
[patent_app_number] => 13/655119
[patent_app_country] => US
[patent_app_date] => 2012-10-18
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 6
[patent_figures_cnt] => 6
[patent_no_of_words] => 7750
[patent_no_of_claims] => 14
[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] =>[firstpage_image] =>[orig_patent_app_number] => 13655119
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/655119 | Guiding mechanism for opening and closing a cargo door of an aircraft, aircraft with such a guiding mechanism and method for opening and closing a cargo door of an aircraft | Oct 17, 2012 | Issued |
Array
(
[id] => 8788655
[patent_doc_number] => 20130105624
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2013-05-02
[patent_title] => 'LANDING GEAR, AN AIRCRAFT, AND A METHOD'
[patent_app_type] => utility
[patent_app_number] => 13/654603
[patent_app_country] => US
[patent_app_date] => 2012-10-18
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 3
[patent_no_of_words] => 6056
[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] =>[firstpage_image] =>[orig_patent_app_number] => 13654603
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/654603 | Landing gear, an aircraft, and a method | Oct 17, 2012 | Issued |
Array
(
[id] => 9084799
[patent_doc_number] => 08556215
[patent_country] => US
[patent_kind] => B1
[patent_issue_date] => 2013-10-15
[patent_title] => 'Aerodynamically efficient surfaces'
[patent_app_type] => utility
[patent_app_number] => 13/654629
[patent_app_country] => US
[patent_app_date] => 2012-10-18
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 16
[patent_figures_cnt] => 23
[patent_no_of_words] => 3252
[patent_no_of_claims] => 1
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 232
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13654629
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/654629 | Aerodynamically efficient surfaces | Oct 17, 2012 | Issued |
Array
(
[id] => 9709142
[patent_doc_number] => 08833700
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2014-09-16
[patent_title] => 'Cover plate, door covering and aircraft or spacecraft'
[patent_app_type] => utility
[patent_app_number] => 13/652069
[patent_app_country] => US
[patent_app_date] => 2012-10-15
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 6
[patent_figures_cnt] => 9
[patent_no_of_words] => 3434
[patent_no_of_claims] => 10
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 176
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13652069
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/652069 | Cover plate, door covering and aircraft or spacecraft | Oct 14, 2012 | Issued |