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] => 5123323
[patent_doc_number] => 20070235593
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2007-10-11
[patent_title] => 'Flying control device for a rotorcraft'
[patent_app_type] => utility
[patent_app_number] => 11/730656
[patent_app_country] => US
[patent_app_date] => 2007-04-03
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 2
[patent_figures_cnt] => 2
[patent_no_of_words] => 2970
[patent_no_of_claims] => 6
[patent_no_of_ind_claims] => 1
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[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0235/20070235593.pdf
[firstpage_image] =>[orig_patent_app_number] => 11730656
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/730656 | Flying control device for a rotorcraft | Apr 2, 2007 | Issued |
Array
(
[id] => 4626275
[patent_doc_number] => 08005583
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2011-08-23
[patent_title] => 'Method and device for determining the air turbulence likely to be encountered by an aircraft'
[patent_app_type] => utility
[patent_app_number] => 11/693191
[patent_app_country] => US
[patent_app_date] => 2007-03-29
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 3
[patent_no_of_words] => 4381
[patent_no_of_claims] => 19
[patent_no_of_ind_claims] => 2
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[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/08/005/08005583.pdf
[firstpage_image] =>[orig_patent_app_number] => 11693191
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/693191 | Method and device for determining the air turbulence likely to be encountered by an aircraft | Mar 28, 2007 | Issued |
Array
(
[id] => 7810230
[patent_doc_number] => 08132759
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2012-03-13
[patent_title] => 'System and method for facilitating aerial refueling'
[patent_app_type] => utility
[patent_app_number] => 11/689280
[patent_app_country] => US
[patent_app_date] => 2007-03-21
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 3
[patent_no_of_words] => 2495
[patent_no_of_claims] => 7
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[patent_words_short_claim] => 382
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[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/08/132/08132759.pdf
[firstpage_image] =>[orig_patent_app_number] => 11689280
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/689280 | System and method for facilitating aerial refueling | Mar 20, 2007 | Issued |
Array
(
[id] => 139610
[patent_doc_number] => 07690604
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2010-04-06
[patent_title] => 'Rudder pedal assembly including non-parallel slide rails'
[patent_app_type] => utility
[patent_app_number] => 11/688701
[patent_app_country] => US
[patent_app_date] => 2007-03-20
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 6
[patent_figures_cnt] => 12
[patent_no_of_words] => 4118
[patent_no_of_claims] => 11
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 348
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/07/690/07690604.pdf
[firstpage_image] =>[orig_patent_app_number] => 11688701
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/688701 | Rudder pedal assembly including non-parallel slide rails | Mar 19, 2007 | Issued |
Array
(
[id] => 4737003
[patent_doc_number] => 20080230655
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2008-09-25
[patent_title] => 'Air barrier for use with an expandable structure'
[patent_app_type] => utility
[patent_app_number] => 11/723237
[patent_app_country] => US
[patent_app_date] => 2007-03-19
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 4
[patent_no_of_words] => 1205
[patent_no_of_claims] => 9
[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/A1/0230/20080230655.pdf
[firstpage_image] =>[orig_patent_app_number] => 11723237
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/723237 | Air barrier for use with an expandable structure | Mar 18, 2007 | Issued |
Array
(
[id] => 4816730
[patent_doc_number] => 20080223989
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2008-09-18
[patent_title] => 'Force Balancing Kite Control System'
[patent_app_type] => utility
[patent_app_number] => 11/686360
[patent_app_country] => US
[patent_app_date] => 2007-03-15
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 6
[patent_figures_cnt] => 6
[patent_no_of_words] => 3510
[patent_no_of_claims] => 5
[patent_no_of_ind_claims] => 1
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[patent_maintenance] => 1
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[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0223/20080223989.pdf
[firstpage_image] =>[orig_patent_app_number] => 11686360
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/686360 | Force balancing kite control system | Mar 14, 2007 | Issued |
Array
(
[id] => 5217184
[patent_doc_number] => 20070158495
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2007-07-12
[patent_title] => 'High lift and high strength aerofoil'
[patent_app_type] => utility
[patent_app_number] => 11/717283
[patent_app_country] => US
[patent_app_date] => 2007-03-14
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 7
[patent_figures_cnt] => 7
[patent_no_of_words] => 739
[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/A1/0158/20070158495.pdf
[firstpage_image] =>[orig_patent_app_number] => 11717283
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/717283 | High lift and high strength aerofoil | Mar 13, 2007 | Abandoned |
Array
(
[id] => 4816721
[patent_doc_number] => 20080223980
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2008-09-18
[patent_title] => 'BUBBLE GLIDER'
[patent_app_type] => utility
[patent_app_number] => 11/685233
[patent_app_country] => US
[patent_app_date] => 2007-03-13
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 2
[patent_figures_cnt] => 2
[patent_no_of_words] => 1546
[patent_no_of_claims] => 11
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 0
[patent_maintenance] => 1
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[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0223/20080223980.pdf
[firstpage_image] =>[orig_patent_app_number] => 11685233
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/685233 | BUBBLE GLIDER | Mar 12, 2007 | Abandoned |
Array
(
[id] => 6239661
[patent_doc_number] => 20100133379
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2010-06-03
[patent_title] => 'Landing gear strut extender'
[patent_app_type] => utility
[patent_app_number] => 11/717904
[patent_app_country] => US
[patent_app_date] => 2007-03-13
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 2
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[patent_no_of_words] => 1232
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[patent_no_of_ind_claims] => 3
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[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0133/20100133379.pdf
[firstpage_image] =>[orig_patent_app_number] => 11717904
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/717904 | Landing gear strut extender | Mar 12, 2007 | Issued |
Array
(
[id] => 4628055
[patent_doc_number] => 08006932
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2011-08-30
[patent_title] => 'Pivoting coupling system for a large dihedral empennage to the tail fuselage of an aircraft'
[patent_app_type] => utility
[patent_app_number] => 11/711758
[patent_app_country] => US
[patent_app_date] => 2007-02-28
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 16
[patent_figures_cnt] => 33
[patent_no_of_words] => 5346
[patent_no_of_claims] => 17
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 369
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/08/006/08006932.pdf
[firstpage_image] =>[orig_patent_app_number] => 11711758
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/711758 | Pivoting coupling system for a large dihedral empennage to the tail fuselage of an aircraft | Feb 27, 2007 | Issued |
Array
(
[id] => 4723677
[patent_doc_number] => 20080203218
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2008-08-28
[patent_title] => 'Systems And Methods For Reducing Pressure Loss Of Air Flowing From A First Area To A Second Area'
[patent_app_type] => utility
[patent_app_number] => 11/678899
[patent_app_country] => US
[patent_app_date] => 2007-02-26
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 7
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[patent_no_of_words] => 2848
[patent_no_of_claims] => 20
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[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0203/20080203218.pdf
[firstpage_image] =>[orig_patent_app_number] => 11678899
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/678899 | Systems And Methods For Reducing Pressure Loss Of Air Flowing From A First Area To A Second Area | Feb 25, 2007 | Abandoned |
Array
(
[id] => 11800276
[patent_doc_number] => 09541106
[patent_country] => US
[patent_kind] => B1
[patent_issue_date] => 2017-01-10
[patent_title] => 'Plasma optimized aerostructures for efficient flow control'
[patent_app_type] => utility
[patent_app_number] => 11/710750
[patent_app_country] => US
[patent_app_date] => 2007-02-26
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 9
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[patent_no_of_words] => 7922
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[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 11710750
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/710750 | Plasma optimized aerostructures for efficient flow control | Feb 25, 2007 | Issued |
Array
(
[id] => 7758971
[patent_doc_number] => 08113469
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2012-02-14
[patent_title] => 'Passive micro-roughness array for drag modification'
[patent_app_type] => utility
[patent_app_number] => 11/708897
[patent_app_country] => US
[patent_app_date] => 2007-02-21
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 7
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[patent_no_of_words] => 6991
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[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/08/113/08113469.pdf
[firstpage_image] =>[orig_patent_app_number] => 11708897
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/708897 | Passive micro-roughness array for drag modification | Feb 20, 2007 | Issued |
Array
(
[id] => 4648533
[patent_doc_number] => 20080035788
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2008-02-14
[patent_title] => 'Cellular support structures used for controlled actuation of fluid contact surfaces'
[patent_app_type] => utility
[patent_app_number] => 11/707052
[patent_app_country] => US
[patent_app_date] => 2007-02-16
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 14
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[patent_no_of_words] => 6599
[patent_no_of_claims] => 30
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[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0035/20080035788.pdf
[firstpage_image] =>[orig_patent_app_number] => 11707052
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/707052 | Cellular support structures used for controlled actuation of fluid contact surfaces | Feb 15, 2007 | Issued |
Array
(
[id] => 5123320
[patent_doc_number] => 20070235590
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2007-10-11
[patent_title] => 'VORTEX GENERATOR'
[patent_app_type] => utility
[patent_app_number] => 11/669463
[patent_app_country] => US
[patent_app_date] => 2007-01-31
[patent_effective_date] => 0000-00-00
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[pdf_file] => publications/A1/0235/20070235590.pdf
[firstpage_image] =>[orig_patent_app_number] => 11669463
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/669463 | VORTEX GENERATOR | Jan 30, 2007 | Abandoned |
Array
(
[id] => 4843045
[patent_doc_number] => 20080179453
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2008-07-31
[patent_title] => 'Modular airship system and method'
[patent_app_type] => utility
[patent_app_number] => 11/698969
[patent_app_country] => US
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[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0179/20080179453.pdf
[firstpage_image] =>[orig_patent_app_number] => 11698969
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/698969 | Modular airship system and method | Jan 25, 2007 | Abandoned |
Array
(
[id] => 4654722
[patent_doc_number] => 20080023582
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2008-01-31
[patent_title] => 'Composite anti-crash structure with controlled buckling for an aircraft'
[patent_app_type] => utility
[patent_app_number] => 11/698020
[patent_app_country] => US
[patent_app_date] => 2007-01-26
[patent_effective_date] => 0000-00-00
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[pdf_file] => publications/A1/0023/20080023582.pdf
[firstpage_image] =>[orig_patent_app_number] => 11698020
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/698020 | Composite anti-crash structure with controlled buckling for an aircraft | Jan 25, 2007 | Issued |
Array
(
[id] => 4556101
[patent_doc_number] => 07857260
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2010-12-28
[patent_title] => 'Fuel jettison system'
[patent_app_type] => utility
[patent_app_number] => 11/624754
[patent_app_country] => US
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[patent_effective_date] => 0000-00-00
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[pdf_file] => patents/07/857/07857260.pdf
[firstpage_image] =>[orig_patent_app_number] => 11624754
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/624754 | Fuel jettison system | Jan 18, 2007 | Issued |
Array
(
[id] => 5110257
[patent_doc_number] => 20070194172
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2007-08-23
[patent_title] => 'AIRCRAFT SHOCK STRUT HAVING IMPROVED CYLINDER AND BEARINGS'
[patent_app_type] => utility
[patent_app_number] => 11/622958
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[patent_effective_date] => 0000-00-00
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[pdf_file] => publications/A1/0194/20070194172.pdf
[firstpage_image] =>[orig_patent_app_number] => 11622958
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/622958 | AIRCRAFT SHOCK STRUT HAVING IMPROVED CYLINDER AND BEARINGS | Jan 11, 2007 | Abandoned |
Array
(
[id] => 9322212
[patent_doc_number] => 08657226
[patent_country] => US
[patent_kind] => B1
[patent_issue_date] => 2014-02-25
[patent_title] => 'Efficient control and stall prevention in advanced configuration aircraft'
[patent_app_type] => utility
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[patent_effective_date] => 0000-00-00
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[patent_maintenance] => 1
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[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 11623042
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/623042 | Efficient control and stall prevention in advanced configuration aircraft | Jan 11, 2007 | Issued |