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] => 5868814
[patent_doc_number] => 20060163431
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2006-07-27
[patent_title] => 'Cover skin for a variable-shape aerodynamic area'
[patent_app_type] => utility
[patent_app_number] => 11/286834
[patent_app_country] => US
[patent_app_date] => 2005-11-23
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
[patent_figures_cnt] => 5
[patent_no_of_words] => 3769
[patent_no_of_claims] => 28
[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/A1/0163/20060163431.pdf
[firstpage_image] =>[orig_patent_app_number] => 11286834
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/286834 | Cover skin for a variable-shape aerodynamic area | Nov 22, 2005 | Issued |
Array
(
[id] => 5092720
[patent_doc_number] => 20070114329
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2007-05-24
[patent_title] => 'Aircraft trailing edge devices, including devices with non-parallel motion paths, and associated methods'
[patent_app_type] => utility
[patent_app_number] => 11/284247
[patent_app_country] => US
[patent_app_date] => 2005-11-21
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 8
[patent_figures_cnt] => 8
[patent_no_of_words] => 6116
[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/A1/0114/20070114329.pdf
[firstpage_image] =>[orig_patent_app_number] => 11284247
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/284247 | Aircraft trailing edge devices, including devices with non-parallel motion paths, and associated methods | Nov 20, 2005 | Issued |
Array
(
[id] => 5628529
[patent_doc_number] => 20060144997
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2006-07-06
[patent_title] => 'Method and system for health monitoring of aircraft landing gear'
[patent_app_type] => utility
[patent_app_number] => 11/281504
[patent_app_country] => US
[patent_app_date] => 2005-11-18
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 10
[patent_figures_cnt] => 10
[patent_no_of_words] => 6912
[patent_no_of_claims] => 50
[patent_no_of_ind_claims] => 7
[patent_words_short_claim] => 0
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0144/20060144997.pdf
[firstpage_image] =>[orig_patent_app_number] => 11281504
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/281504 | Method and system for health monitoring of aircraft landing gear | Nov 17, 2005 | Abandoned |
Array
(
[id] => 149418
[patent_doc_number] => 07677492
[patent_country] => US
[patent_kind] => B1
[patent_issue_date] => 2010-03-16
[patent_title] => 'Automatic mechanical control of rotor blade collective pitch'
[patent_app_type] => utility
[patent_app_number] => 11/280036
[patent_app_country] => US
[patent_app_date] => 2005-11-16
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
[patent_figures_cnt] => 5
[patent_no_of_words] => 3519
[patent_no_of_claims] => 13
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 241
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/07/677/07677492.pdf
[firstpage_image] =>[orig_patent_app_number] => 11280036
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/280036 | Automatic mechanical control of rotor blade collective pitch | Nov 15, 2005 | Issued |
Array
(
[id] => 4967275
[patent_doc_number] => 20070107277
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2007-05-17
[patent_title] => 'SEAT IDENTIFICATION SYSTEM'
[patent_app_type] => utility
[patent_app_number] => 11/164200
[patent_app_country] => US
[patent_app_date] => 2005-11-14
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 4
[patent_no_of_words] => 2566
[patent_no_of_claims] => 27
[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/A1/0107/20070107277.pdf
[firstpage_image] =>[orig_patent_app_number] => 11164200
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/164200 | SEAT IDENTIFICATION SYSTEM | Nov 13, 2005 | Abandoned |
Array
(
[id] => 5031438
[patent_doc_number] => 20070095977
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2007-05-03
[patent_title] => 'Mesh fender for protecting an aircraft against damage from foreign objects'
[patent_app_type] => utility
[patent_app_number] => 11/263511
[patent_app_country] => US
[patent_app_date] => 2005-10-31
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 7
[patent_figures_cnt] => 7
[patent_no_of_words] => 2857
[patent_no_of_claims] => 17
[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/A1/0095/20070095977.pdf
[firstpage_image] =>[orig_patent_app_number] => 11263511
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/263511 | Mesh fender for protecting an aircraft against damage from foreign objects | Oct 30, 2005 | Abandoned |
Array
(
[id] => 5031445
[patent_doc_number] => 20070095984
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2007-05-03
[patent_title] => 'Window assembly retaining system'
[patent_app_type] => utility
[patent_app_number] => 11/262361
[patent_app_country] => US
[patent_app_date] => 2005-10-28
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 7
[patent_figures_cnt] => 7
[patent_no_of_words] => 2535
[patent_no_of_claims] => 29
[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/A1/0095/20070095984.pdf
[firstpage_image] =>[orig_patent_app_number] => 11262361
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/262361 | Window assembly retaining system | Oct 27, 2005 | Issued |
Array
(
[id] => 5213491
[patent_doc_number] => 20070102571
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2007-05-10
[patent_title] => 'Airship for lifting heavy loads & methods of operation'
[patent_app_type] => utility
[patent_app_number] => 11/253753
[patent_app_country] => US
[patent_app_date] => 2005-10-20
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 3
[patent_no_of_words] => 5160
[patent_no_of_claims] => 24
[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/A1/0102/20070102571.pdf
[firstpage_image] =>[orig_patent_app_number] => 11253753
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/253753 | Airship for lifting heavy loads & methods of operation | Oct 19, 2005 | Abandoned |
Array
(
[id] => 4896707
[patent_doc_number] => 20080116320
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2008-05-22
[patent_title] => 'Aircraft With Wings Whose Maximum Lift Can Be Altered By Controllable Wing Components'
[patent_app_type] => utility
[patent_app_number] => 11/663055
[patent_app_country] => US
[patent_app_date] => 2005-09-21
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 3
[patent_no_of_words] => 1747
[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/A1/0116/20080116320.pdf
[firstpage_image] =>[orig_patent_app_number] => 11663055
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/663055 | Aircraft With Wings Whose Maximum Lift Can Be Altered By Controllable Wing Components | Sep 20, 2005 | Abandoned |
Array
(
[id] => 372563
[patent_doc_number] => 07472865
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2009-01-06
[patent_title] => 'Dehumidification system for an airship'
[patent_app_type] => utility
[patent_app_number] => 11/228652
[patent_app_country] => US
[patent_app_date] => 2005-09-15
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 3
[patent_no_of_words] => 3804
[patent_no_of_claims] => 2
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 102
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/07/472/07472865.pdf
[firstpage_image] =>[orig_patent_app_number] => 11228652
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/228652 | Dehumidification system for an airship | Sep 14, 2005 | Issued |
Array
(
[id] => 5222774
[patent_doc_number] => 20070252040
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2007-11-01
[patent_title] => 'Seal assemblies for use with drooped spoilers and other control surfaces on aircraft'
[patent_app_type] => utility
[patent_app_number] => 11/220446
[patent_app_country] => US
[patent_app_date] => 2005-09-07
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 8
[patent_figures_cnt] => 8
[patent_no_of_words] => 3321
[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] => publications/A1/0252/20070252040.pdf
[firstpage_image] =>[orig_patent_app_number] => 11220446
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/220446 | Seal assemblies for use with drooped spoilers and other control surfaces on aircraft | Sep 6, 2005 | Issued |
Array
(
[id] => 4610300
[patent_doc_number] => 07988096
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2011-08-02
[patent_title] => 'Space manufacturing module system and method'
[patent_app_type] => utility
[patent_app_number] => 11/217649
[patent_app_country] => US
[patent_app_date] => 2005-09-01
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 6
[patent_figures_cnt] => 6
[patent_no_of_words] => 6493
[patent_no_of_claims] => 14
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 188
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/07/988/07988096.pdf
[firstpage_image] =>[orig_patent_app_number] => 11217649
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/217649 | Space manufacturing module system and method | Aug 31, 2005 | Issued |
Array
(
[id] => 5145412
[patent_doc_number] => 20070045466
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2007-03-01
[patent_title] => 'Foldable, lockable control surface and method of using same'
[patent_app_type] => utility
[patent_app_number] => 11/216355
[patent_app_country] => US
[patent_app_date] => 2005-08-31
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 9
[patent_figures_cnt] => 9
[patent_no_of_words] => 4356
[patent_no_of_claims] => 22
[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/A1/0045/20070045466.pdf
[firstpage_image] =>[orig_patent_app_number] => 11216355
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/216355 | Foldable, lockable control surface and method of using same | Aug 30, 2005 | Abandoned |
Array
(
[id] => 571462
[patent_doc_number] => 07448577
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2008-11-11
[patent_title] => 'Apparatus for providing velocity differential between parachute and payload to reduce shock load'
[patent_app_type] => utility
[patent_app_number] => 11/217848
[patent_app_country] => US
[patent_app_date] => 2005-08-23
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
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[patent_no_of_words] => 3087
[patent_no_of_claims] => 2
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 443
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/07/448/07448577.pdf
[firstpage_image] =>[orig_patent_app_number] => 11217848
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/217848 | Apparatus for providing velocity differential between parachute and payload to reduce shock load | Aug 22, 2005 | Issued |
Array
(
[id] => 5898009
[patent_doc_number] => 20060043242
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2006-03-02
[patent_title] => 'Aircraft flight control surface actuation system communication architecture'
[patent_app_type] => utility
[patent_app_number] => 11/207250
[patent_app_country] => US
[patent_app_date] => 2005-08-19
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
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[patent_no_of_words] => 3997
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[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0043/20060043242.pdf
[firstpage_image] =>[orig_patent_app_number] => 11207250
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/207250 | Aircraft flight control surface actuation system communication architecture | Aug 18, 2005 | Issued |
Array
(
[id] => 5227990
[patent_doc_number] => 20070290097
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2007-12-20
[patent_title] => 'Vertical take-off and landing aircraft'
[patent_app_type] => utility
[patent_app_number] => 11/206909
[patent_app_country] => US
[patent_app_date] => 2005-08-19
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 14
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[patent_no_of_words] => 5979
[patent_no_of_claims] => 6
[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/A1/0290/20070290097.pdf
[firstpage_image] =>[orig_patent_app_number] => 11206909
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/206909 | Vertical take-off and landing aircraft | Aug 18, 2005 | Abandoned |
Array
(
[id] => 200420
[patent_doc_number] => 07631839
[patent_country] => US
[patent_kind] => B1
[patent_issue_date] => 2009-12-15
[patent_title] => 'Enhanced multiple instrument distributed aperture sensor'
[patent_app_type] => utility
[patent_app_number] => 11/205012
[patent_app_country] => US
[patent_app_date] => 2005-08-17
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 7
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[patent_no_of_words] => 6088
[patent_no_of_claims] => 40
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[patent_words_short_claim] => 202
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/07/631/07631839.pdf
[firstpage_image] =>[orig_patent_app_number] => 11205012
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/205012 | Enhanced multiple instrument distributed aperture sensor | Aug 16, 2005 | Issued |
Array
(
[id] => 5615745
[patent_doc_number] => 20060185277
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2006-08-24
[patent_title] => 'Modular platform system'
[patent_app_type] => utility
[patent_app_number] => 11/205347
[patent_app_country] => US
[patent_app_date] => 2005-08-16
[patent_effective_date] => 0000-00-00
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[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0185/20060185277.pdf
[firstpage_image] =>[orig_patent_app_number] => 11205347
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/205347 | Modular platform system | Aug 15, 2005 | Abandoned |
Array
(
[id] => 5151867
[patent_doc_number] => 20070034749
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2007-02-15
[patent_title] => 'Deployable airfoil assembly for aircraft'
[patent_app_type] => utility
[patent_app_number] => 11/202494
[patent_app_country] => US
[patent_app_date] => 2005-08-12
[patent_effective_date] => 0000-00-00
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[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0034/20070034749.pdf
[firstpage_image] =>[orig_patent_app_number] => 11202494
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/202494 | Deployable airfoil assembly for aircraft | Aug 11, 2005 | Abandoned |
Array
(
[id] => 5151862
[patent_doc_number] => 20070034744
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2007-02-15
[patent_title] => 'Multi-grommet retained slider for parachutes'
[patent_app_type] => utility
[patent_app_number] => 11/201186
[patent_app_country] => US
[patent_app_date] => 2005-08-11
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 6
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[patent_no_of_words] => 6111
[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] => publications/A1/0034/20070034744.pdf
[firstpage_image] =>[orig_patent_app_number] => 11201186
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/201186 | Multi-grommet retained slider for parachutes | Aug 10, 2005 | Issued |