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] => 6310360
[patent_doc_number] => 20100193643
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2010-08-05
[patent_title] => 'LIFT FAN SYSTEM'
[patent_app_type] => utility
[patent_app_number] => 12/643745
[patent_app_country] => US
[patent_app_date] => 2009-12-21
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 4
[patent_no_of_words] => 3648
[patent_no_of_claims] => 21
[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/A1/0193/20100193643.pdf
[firstpage_image] =>[orig_patent_app_number] => 12643745
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/643745 | LIFT FAN SYSTEM | Dec 20, 2009 | Abandoned |
Array
(
[id] => 6455524
[patent_doc_number] => 20100090068
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2010-04-15
[patent_title] => 'AIRCRAFT WITH WINGS WHOSE MAXIMUM LIFT CAN BE ALTERED BY CONTROLLABLE WING COMPONENTS'
[patent_app_type] => utility
[patent_app_number] => 12/640559
[patent_app_country] => US
[patent_app_date] => 2009-12-17
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 3
[patent_no_of_words] => 2461
[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] => publications/A1/0090/20100090068.pdf
[firstpage_image] =>[orig_patent_app_number] => 12640559
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/640559 | AIRCRAFT WITH WINGS WHOSE MAXIMUM LIFT CAN BE ALTERED BY CONTROLLABLE WING COMPONENTS | Dec 16, 2009 | Abandoned |
Array
(
[id] => 6398606
[patent_doc_number] => 20100147995
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2010-06-17
[patent_title] => 'AIRCRAFT UNDERCARRIAGE WITH MOTORIZATION AND TRANSMISSION'
[patent_app_type] => utility
[patent_app_number] => 12/637516
[patent_app_country] => US
[patent_app_date] => 2009-12-14
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 4
[patent_no_of_words] => 4780
[patent_no_of_claims] => 12
[patent_no_of_ind_claims] => 2
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[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0147/20100147995.pdf
[firstpage_image] =>[orig_patent_app_number] => 12637516
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/637516 | Aircraft undercarriage with motorization and transmission | Dec 13, 2009 | Issued |
Array
(
[id] => 9111551
[patent_doc_number] => 08567713
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2013-10-29
[patent_title] => 'Lift fan clutch'
[patent_app_type] => utility
[patent_app_number] => 12/635525
[patent_app_country] => US
[patent_app_date] => 2009-12-10
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 6
[patent_no_of_words] => 3699
[patent_no_of_claims] => 9
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 429
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 12635525
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/635525 | Lift fan clutch | Dec 9, 2009 | Issued |
12/634926 | PRESSURE ACTIVATED INERTIALLY LOCKING BASE FOR PROJECTILES | Dec 9, 2009 | Abandoned |
Array
(
[id] => 6476447
[patent_doc_number] => 20100213314
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2010-08-26
[patent_title] => 'ARRANGEMENT FOR INSTALLING ELECTRIC CABLES IN THE FLOOR REGION OF AN AIRCRAFT'
[patent_app_type] => utility
[patent_app_number] => 12/629171
[patent_app_country] => US
[patent_app_date] => 2009-12-02
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 3
[patent_no_of_words] => 2872
[patent_no_of_claims] => 18
[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/A1/0213/20100213314.pdf
[firstpage_image] =>[orig_patent_app_number] => 12629171
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/629171 | Arrangement for installing electric cables in the floor region of an aircraft | Dec 1, 2009 | Issued |
Array
(
[id] => 8857071
[patent_doc_number] => 08459596
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2013-06-11
[patent_title] => 'Sky/space elevators'
[patent_app_type] => utility
[patent_app_number] => 12/592655
[patent_app_country] => US
[patent_app_date] => 2009-12-01
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 13
[patent_figures_cnt] => 16
[patent_no_of_words] => 2503
[patent_no_of_claims] => 7
[patent_no_of_ind_claims] => 1
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[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 12592655
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/592655 | Sky/space elevators | Nov 30, 2009 | Issued |
Array
(
[id] => 8662813
[patent_doc_number] => 08376269
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2013-02-19
[patent_title] => 'Hydraulic valve, a hybrid helicopter provided with such a hydraulic valve, and a method implemented by the hydraulic valve'
[patent_app_type] => utility
[patent_app_number] => 12/628406
[patent_app_country] => US
[patent_app_date] => 2009-12-01
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 6
[patent_no_of_words] => 8312
[patent_no_of_claims] => 13
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 154
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 12628406
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/628406 | Hydraulic valve, a hybrid helicopter provided with such a hydraulic valve, and a method implemented by the hydraulic valve | Nov 30, 2009 | Issued |
Array
(
[id] => 8375646
[patent_doc_number] => 08258447
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2012-09-04
[patent_title] => 'Methods and apparatus for a frangible seal for deployable flight structures'
[patent_app_type] => utility
[patent_app_number] => 12/628610
[patent_app_country] => US
[patent_app_date] => 2009-12-01
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 2
[patent_figures_cnt] => 4
[patent_no_of_words] => 1559
[patent_no_of_claims] => 20
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 86
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 12628610
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/628610 | Methods and apparatus for a frangible seal for deployable flight structures | Nov 30, 2009 | Issued |
Array
(
[id] => 9045635
[patent_doc_number] => 08540186
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2013-09-24
[patent_title] => 'Rigid aircraft pylon structure in contact with a fuselage lateral extension for attachment'
[patent_app_type] => utility
[patent_app_number] => 13/131950
[patent_app_country] => US
[patent_app_date] => 2009-11-30
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 6
[patent_figures_cnt] => 7
[patent_no_of_words] => 4185
[patent_no_of_claims] => 10
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[patent_words_short_claim] => 187
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13131950
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/131950 | Rigid aircraft pylon structure in contact with a fuselage lateral extension for attachment | Nov 29, 2009 | Issued |
Array
(
[id] => 6430572
[patent_doc_number] => 20100187354
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2010-07-29
[patent_title] => 'INFORMATION SYSTEM FOR MESSAGES FROM PASSENGERS TO THE CABIN CREW'
[patent_app_type] => utility
[patent_app_number] => 12/627205
[patent_app_country] => US
[patent_app_date] => 2009-11-30
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 4
[patent_no_of_words] => 1321
[patent_no_of_claims] => 7
[patent_no_of_ind_claims] => 1
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[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0187/20100187354.pdf
[firstpage_image] =>[orig_patent_app_number] => 12627205
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/627205 | INFORMATION SYSTEM FOR MESSAGES FROM PASSENGERS TO THE CABIN CREW | Nov 29, 2009 | Abandoned |
Array
(
[id] => 6177030
[patent_doc_number] => 20110121130
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2011-05-26
[patent_title] => 'BLENDED WING BODY CARGO AIRPLANE'
[patent_app_type] => utility
[patent_app_number] => 12/623404
[patent_app_country] => US
[patent_app_date] => 2009-11-21
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 12
[patent_figures_cnt] => 12
[patent_no_of_words] => 9921
[patent_no_of_claims] => 20
[patent_no_of_ind_claims] => 3
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[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0121/20110121130.pdf
[firstpage_image] =>[orig_patent_app_number] => 12623404
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/623404 | Blended wing body cargo airplane | Nov 20, 2009 | Issued |
Array
(
[id] => 8559286
[patent_doc_number] => 08333346
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2012-12-18
[patent_title] => 'Sky station'
[patent_app_type] => utility
[patent_app_number] => 12/592031
[patent_app_country] => US
[patent_app_date] => 2009-11-18
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 17
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[patent_no_of_words] => 5556
[patent_no_of_claims] => 8
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[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 12592031
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/592031 | Sky station | Nov 17, 2009 | Issued |
Array
(
[id] => 6407578
[patent_doc_number] => 20100140418
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2010-06-10
[patent_title] => 'Air Induction Control'
[patent_app_type] => utility
[patent_app_number] => 12/619028
[patent_app_country] => US
[patent_app_date] => 2009-11-16
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 13
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[pdf_file] => publications/A1/0140/20100140418.pdf
[firstpage_image] =>[orig_patent_app_number] => 12619028
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/619028 | Air induction control | Nov 15, 2009 | Issued |
Array
(
[id] => 8967041
[patent_doc_number] => 08505849
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2013-08-13
[patent_title] => 'Device for retracting aircraft landing gear'
[patent_app_type] => utility
[patent_app_number] => 13/125717
[patent_app_country] => US
[patent_app_date] => 2009-11-10
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[patent_drawing_sheets_cnt] => 3
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[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13125717
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/125717 | Device for retracting aircraft landing gear | Nov 9, 2009 | Issued |
Array
(
[id] => 9152093
[patent_doc_number] => 08584991
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2013-11-19
[patent_title] => 'Vane having a regulating flap and a gap covering device and an adjusting mechanism for a gap covering device'
[patent_app_type] => utility
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[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13128242
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/128242 | Vane having a regulating flap and a gap covering device and an adjusting mechanism for a gap covering device | Nov 9, 2009 | Issued |
Array
(
[id] => 9467190
[patent_doc_number] => 08720816
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2014-05-13
[patent_title] => 'Unmanned aerial vehicle'
[patent_app_type] => utility
[patent_app_number] => 13/130481
[patent_app_country] => US
[patent_app_date] => 2009-11-10
[patent_effective_date] => 0000-00-00
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[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13130481
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/130481 | Unmanned aerial vehicle | Nov 9, 2009 | Issued |
Array
(
[id] => 8805932
[patent_doc_number] => 08443575
[patent_country] => US
[patent_kind] => B1
[patent_issue_date] => 2013-05-21
[patent_title] => 'Composite access door'
[patent_app_type] => utility
[patent_app_number] => 12/606331
[patent_app_country] => US
[patent_app_date] => 2009-10-27
[patent_effective_date] => 0000-00-00
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[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 12606331
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/606331 | Composite access door | Oct 26, 2009 | Issued |
Array
(
[id] => 4638201
[patent_doc_number] => 08016226
[patent_country] => US
[patent_kind] => B1
[patent_issue_date] => 2011-09-13
[patent_title] => 'Vertical take off and landing aircraft system with energy recapture technology'
[patent_app_type] => utility
[patent_app_number] => 12/587286
[patent_app_country] => US
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[pdf_file] => patents/08/016/08016226.pdf
[firstpage_image] =>[orig_patent_app_number] => 12587286
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/587286 | Vertical take off and landing aircraft system with energy recapture technology | Oct 4, 2009 | Issued |
Array
(
[id] => 9007813
[patent_doc_number] => 08523102
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2013-09-03
[patent_title] => 'Method and apparatus for aircraft sensor and actuator failure protection using reconfigurable flight control laws'
[patent_app_type] => utility
[patent_app_number] => 13/121458
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[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13121458
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/121458 | Method and apparatus for aircraft sensor and actuator failure protection using reconfigurable flight control laws | Oct 4, 2009 | Issued |