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] => 8506297
[patent_doc_number] => 20120305705
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2012-12-06
[patent_title] => 'SEAT WHICH CAN BE CONVERTED INTO A BED'
[patent_app_type] => utility
[patent_app_number] => 13/484594
[patent_app_country] => US
[patent_app_date] => 2012-05-31
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 4
[patent_no_of_words] => 7045
[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] => 13484594
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/484594 | Seat which can be converted into a bed | May 30, 2012 | Issued |
Array
(
[id] => 9178149
[patent_doc_number] => 20130320134
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2013-12-05
[patent_title] => 'AUXILIARY FIRE RESISTANT MOUNT SYSTEM FOR AN AUXILIARY POWER UNIT'
[patent_app_type] => utility
[patent_app_number] => 13/484880
[patent_app_country] => US
[patent_app_date] => 2012-05-31
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 3
[patent_no_of_words] => 1199
[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] => 13484880
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/484880 | Auxiliary fire resistant mount system for an auxiliary power unit | May 30, 2012 | Issued |
Array
(
[id] => 8439425
[patent_doc_number] => 20120256041
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2012-10-11
[patent_title] => 'AIRCRAFT STABILIZER SYSTEM AND METHODS OF USING THE SAME'
[patent_app_type] => utility
[patent_app_number] => 13/485623
[patent_app_country] => US
[patent_app_date] => 2012-05-31
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 16
[patent_figures_cnt] => 16
[patent_no_of_words] => 6572
[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] =>[firstpage_image] =>[orig_patent_app_number] => 13485623
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/485623 | Aircraft stabilizer system and methods of using the same | May 30, 2012 | Issued |
Array
(
[id] => 9942468
[patent_doc_number] => 08991757
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2015-03-31
[patent_title] => 'Self-supporting cabin structural segment'
[patent_app_type] => utility
[patent_app_number] => 13/479538
[patent_app_country] => US
[patent_app_date] => 2012-05-24
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 11
[patent_figures_cnt] => 11
[patent_no_of_words] => 6064
[patent_no_of_claims] => 16
[patent_no_of_ind_claims] => 3
[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] => 13479538
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/479538 | Self-supporting cabin structural segment | May 23, 2012 | Issued |
Array
(
[id] => 8519515
[patent_doc_number] => 20120318923
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2012-12-20
[patent_title] => 'ELECTROTHERMAL WING ICE PROTECTION SYSTEM'
[patent_app_type] => utility
[patent_app_number] => 13/479105
[patent_app_country] => US
[patent_app_date] => 2012-05-23
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 10
[patent_figures_cnt] => 10
[patent_no_of_words] => 1749
[patent_no_of_claims] => 35
[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] => 13479105
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/479105 | Electrothermal wing ice protection system | May 22, 2012 | Issued |
Array
(
[id] => 9113495
[patent_doc_number] => 08569670
[patent_country] => US
[patent_kind] => B1
[patent_issue_date] => 2013-10-29
[patent_title] => 'Pressure activated inertially locking base for projectiles'
[patent_app_type] => utility
[patent_app_number] => 13/476451
[patent_app_country] => US
[patent_app_date] => 2012-05-21
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 7
[patent_figures_cnt] => 7
[patent_no_of_words] => 3416
[patent_no_of_claims] => 6
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 360
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13476451
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/476451 | Pressure activated inertially locking base for projectiles | May 20, 2012 | Issued |
Array
(
[id] => 9058354
[patent_doc_number] => 08544787
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2013-10-01
[patent_title] => 'High performance tilt rotor aircraft in which nacelle tilt angle and flaperon angle mechanically interwork with each other'
[patent_app_type] => utility
[patent_app_number] => 13/476274
[patent_app_country] => US
[patent_app_date] => 2012-05-21
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 4
[patent_no_of_words] => 3787
[patent_no_of_claims] => 2
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 242
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13476274
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/476274 | High performance tilt rotor aircraft in which nacelle tilt angle and flaperon angle mechanically interwork with each other | May 20, 2012 | Issued |
Array
(
[id] => 8506293
[patent_doc_number] => 20120305701
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2012-12-06
[patent_title] => 'AIRCRAFT CONTROL SURFACE DRIVE MECHANISM'
[patent_app_type] => utility
[patent_app_number] => 13/476844
[patent_app_country] => US
[patent_app_date] => 2012-05-21
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 8
[patent_figures_cnt] => 8
[patent_no_of_words] => 7462
[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] =>[firstpage_image] =>[orig_patent_app_number] => 13476844
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/476844 | Aircraft control surface drive mechanism | May 20, 2012 | Issued |
Array
(
[id] => 10855843
[patent_doc_number] => 08882030
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2014-11-11
[patent_title] => 'Autonomous electricity production and conditioning system for an aircraft, associated aircraft and method'
[patent_app_type] => utility
[patent_app_number] => 13/471801
[patent_app_country] => US
[patent_app_date] => 2012-05-15
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 10
[patent_figures_cnt] => 14
[patent_no_of_words] => 8056
[patent_no_of_claims] => 16
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 207
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13471801
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/471801 | Autonomous electricity production and conditioning system for an aircraft, associated aircraft and method | May 14, 2012 | Issued |
Array
(
[id] => 8563401
[patent_doc_number] => 20120325972
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2012-12-27
[patent_title] => 'ROBOTIC SATELLITE REFUELLING TOOL'
[patent_app_type] => utility
[patent_app_number] => 13/470661
[patent_app_country] => US
[patent_app_date] => 2012-05-14
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 17
[patent_figures_cnt] => 17
[patent_no_of_words] => 9430
[patent_no_of_claims] => 13
[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] => 13470661
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/470661 | Robotic satellite refuelling tool | May 13, 2012 | Issued |
Array
(
[id] => 8783514
[patent_doc_number] => 08430353
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2013-04-30
[patent_title] => 'Helicopter torque counteraction device'
[patent_app_type] => utility
[patent_app_number] => 13/463400
[patent_app_country] => US
[patent_app_date] => 2012-05-03
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 4
[patent_no_of_words] => 2338
[patent_no_of_claims] => 24
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 62
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13463400
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/463400 | Helicopter torque counteraction device | May 2, 2012 | Issued |
Array
(
[id] => 8493027
[patent_doc_number] => 20120292434
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2012-11-22
[patent_title] => 'Six Degrees Of Freedom Vibration Suppression'
[patent_app_type] => utility
[patent_app_number] => 13/459821
[patent_app_country] => US
[patent_app_date] => 2012-04-30
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 4
[patent_no_of_words] => 1221
[patent_no_of_claims] => 11
[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] => 13459821
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/459821 | Six Degrees Of Freedom Vibration Suppression | Apr 29, 2012 | Abandoned |
Array
(
[id] => 8833149
[patent_doc_number] => 08448898
[patent_country] => US
[patent_kind] => B1
[patent_issue_date] => 2013-05-28
[patent_title] => 'Autonomous solar aircraft'
[patent_app_type] => utility
[patent_app_number] => 13/460146
[patent_app_country] => US
[patent_app_date] => 2012-04-30
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 9
[patent_figures_cnt] => 19
[patent_no_of_words] => 8537
[patent_no_of_claims] => 28
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 92
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13460146
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/460146 | Autonomous solar aircraft | Apr 29, 2012 | Issued |
Array
(
[id] => 9702153
[patent_doc_number] => 08827207
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2014-09-09
[patent_title] => 'Ice protection system'
[patent_app_type] => utility
[patent_app_number] => 13/455163
[patent_app_country] => US
[patent_app_date] => 2012-04-25
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 11
[patent_figures_cnt] => 11
[patent_no_of_words] => 2445
[patent_no_of_claims] => 20
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 254
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13455163
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/455163 | Ice protection system | Apr 24, 2012 | Issued |
Array
(
[id] => 8462313
[patent_doc_number] => 20120267482
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2012-10-25
[patent_title] => 'Device for Protecting an Optical Instrument of a Satellite'
[patent_app_type] => utility
[patent_app_number] => 13/451419
[patent_app_country] => US
[patent_app_date] => 2012-04-19
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 9
[patent_figures_cnt] => 9
[patent_no_of_words] => 3877
[patent_no_of_claims] => 13
[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] => 13451419
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/451419 | Device for protecting an optical instrument of a satellite | Apr 18, 2012 | Issued |
Array
(
[id] => 8474209
[patent_doc_number] => 20120273615
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2012-11-01
[patent_title] => 'OVERHEAD LUGGAGE COMPARTMENT'
[patent_app_type] => utility
[patent_app_number] => 13/449757
[patent_app_country] => US
[patent_app_date] => 2012-04-18
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 10
[patent_figures_cnt] => 10
[patent_no_of_words] => 2274
[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] =>[firstpage_image] =>[orig_patent_app_number] => 13449757
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/449757 | Overhead luggage compartment | Apr 17, 2012 | Issued |
Array
(
[id] => 8662812
[patent_doc_number] => 08376268
[patent_country] => US
[patent_kind] => B1
[patent_issue_date] => 2013-02-19
[patent_title] => 'Flight control system using thrust devices'
[patent_app_type] => utility
[patent_app_number] => 13/442439
[patent_app_country] => US
[patent_app_date] => 2012-04-09
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 10
[patent_figures_cnt] => 16
[patent_no_of_words] => 5624
[patent_no_of_claims] => 5
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 152
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13442439
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/442439 | Flight control system using thrust devices | Apr 8, 2012 | Issued |
Array
(
[id] => 9078890
[patent_doc_number] => 20130264420
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2013-10-10
[patent_title] => 'ADAPTABLE AIRPORT SYSTEM WITH INDUSTRIAL ZONES AND CLEAN ENERGY GENERATION'
[patent_app_type] => utility
[patent_app_number] => 13/442406
[patent_app_country] => US
[patent_app_date] => 2012-04-09
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 3
[patent_no_of_words] => 2168
[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] => 13442406
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/442406 | ADAPTABLE AIRPORT SYSTEM WITH INDUSTRIAL ZONES AND CLEAN ENERGY GENERATION | Apr 8, 2012 | Abandoned |
Array
(
[id] => 8287130
[patent_doc_number] => 20120175463
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2012-07-12
[patent_title] => 'Fuel Range For An Aircraft'
[patent_app_type] => utility
[patent_app_number] => 13/428468
[patent_app_country] => US
[patent_app_date] => 2012-03-23
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
[patent_figures_cnt] => 5
[patent_no_of_words] => 2643
[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] =>[firstpage_image] =>[orig_patent_app_number] => 13428468
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/428468 | Fuel range for an aircraft | Mar 22, 2012 | Issued |
Array
(
[id] => 8402921
[patent_doc_number] => 20120234982
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2012-09-20
[patent_title] => 'Retractable Plane Structure, and Satellite Comprising Such a Structure'
[patent_app_type] => utility
[patent_app_number] => 13/419302
[patent_app_country] => US
[patent_app_date] => 2012-03-13
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 3
[patent_no_of_words] => 1828
[patent_no_of_claims] => 9
[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] => 13419302
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/419302 | Retractable Plane Structure, and Satellite Comprising Such a Structure | Mar 12, 2012 | Abandoned |