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] => 5268272
[patent_doc_number] => 20090072047
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2009-03-19
[patent_title] => 'AIRCRAFT DEFENSE SYSTEM AND METHOD'
[patent_app_type] => utility
[patent_app_number] => 11/427499
[patent_app_country] => US
[patent_app_date] => 2006-06-29
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 2
[patent_figures_cnt] => 2
[patent_no_of_words] => 1849
[patent_no_of_claims] => 9
[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/A1/0072/20090072047.pdf
[firstpage_image] =>[orig_patent_app_number] => 11427499
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/427499 | AIRCRAFT DEFENSE SYSTEM AND METHOD | Jun 28, 2006 | Abandoned |
Array
(
[id] => 4505971
[patent_doc_number] => 07909261
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2011-03-22
[patent_title] => 'Device and an aircraft anti-icing system comprising such a device'
[patent_app_type] => utility
[patent_app_number] => 11/424544
[patent_app_country] => US
[patent_app_date] => 2006-06-16
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 2
[patent_figures_cnt] => 6
[patent_no_of_words] => 4329
[patent_no_of_claims] => 16
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 299
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/07/909/07909261.pdf
[firstpage_image] =>[orig_patent_app_number] => 11424544
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/424544 | Device and an aircraft anti-icing system comprising such a device | Jun 15, 2006 | Issued |
11/422554 | RAM BOOSTER | Jun 5, 2006 | Abandoned |
Array
(
[id] => 9580517
[patent_doc_number] => 08770514
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2014-07-08
[patent_title] => 'Landing gear'
[patent_app_type] => utility
[patent_app_number] => 11/421726
[patent_app_country] => US
[patent_app_date] => 2006-06-01
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
[patent_figures_cnt] => 5
[patent_no_of_words] => 3652
[patent_no_of_claims] => 16
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 104
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 11421726
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/421726 | Landing gear | May 31, 2006 | Issued |
Array
(
[id] => 6335082
[patent_doc_number] => 20100019085
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2010-01-28
[patent_title] => 'DEVICE AND METHOD FOR RECOVERING UNMANNED AIRBORNE VEHICLES'
[patent_app_type] => utility
[patent_app_number] => 12/300396
[patent_app_country] => US
[patent_app_date] => 2006-05-11
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
[patent_figures_cnt] => 5
[patent_no_of_words] => 3672
[patent_no_of_claims] => 22
[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/A1/0019/20100019085.pdf
[firstpage_image] =>[orig_patent_app_number] => 12300396
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/300396 | DEVICE AND METHOD FOR RECOVERING UNMANNED AIRBORNE VEHICLES | May 10, 2006 | Abandoned |
Array
(
[id] => 255529
[patent_doc_number] => 07575193
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2009-08-18
[patent_title] => 'Anti-crash method and system, an undercarriage, and an aircraft'
[patent_app_type] => utility
[patent_app_number] => 11/429255
[patent_app_country] => US
[patent_app_date] => 2006-05-08
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 6
[patent_figures_cnt] => 20
[patent_no_of_words] => 14847
[patent_no_of_claims] => 13
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 249
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/07/575/07575193.pdf
[firstpage_image] =>[orig_patent_app_number] => 11429255
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/429255 | Anti-crash method and system, an undercarriage, and an aircraft | May 7, 2006 | Issued |
Array
(
[id] => 5425590
[patent_doc_number] => 20090084900
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2009-04-02
[patent_title] => 'Window element for insertion in a window cutout in an outer skin of an aircraft'
[patent_app_type] => utility
[patent_app_number] => 11/990366
[patent_app_country] => US
[patent_app_date] => 2006-04-26
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 4
[patent_no_of_words] => 4322
[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] => publications/A1/0084/20090084900.pdf
[firstpage_image] =>[orig_patent_app_number] => 11990366
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/990366 | Window element for insertion in a window cutout in an outer skin of an aircraft | Apr 25, 2006 | Issued |
Array
(
[id] => 4556028
[patent_doc_number] => 07857253
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2010-12-28
[patent_title] => 'Ducted fan VTOL vehicles'
[patent_app_type] => utility
[patent_app_number] => 11/411243
[patent_app_country] => US
[patent_app_date] => 2006-04-26
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 53
[patent_figures_cnt] => 96
[patent_no_of_words] => 15683
[patent_no_of_claims] => 18
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 167
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/07/857/07857253.pdf
[firstpage_image] =>[orig_patent_app_number] => 11411243
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/411243 | Ducted fan VTOL vehicles | Apr 25, 2006 | Issued |
Array
(
[id] => 5244995
[patent_doc_number] => 20070241229
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2007-10-18
[patent_title] => 'Inlet distortion and recovery control system'
[patent_app_type] => utility
[patent_app_number] => 11/403252
[patent_app_country] => US
[patent_app_date] => 2006-04-12
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 13
[patent_figures_cnt] => 13
[patent_no_of_words] => 4096
[patent_no_of_claims] => 40
[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/A1/0241/20070241229.pdf
[firstpage_image] =>[orig_patent_app_number] => 11403252
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/403252 | Inlet distortion and recovery control system | Apr 11, 2006 | Issued |
Array
(
[id] => 7554331
[patent_doc_number] => 08066228
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2011-11-29
[patent_title] => 'Single slotted flap with sliding deflector flap and lowerable spoiler'
[patent_app_type] => utility
[patent_app_number] => 11/911124
[patent_app_country] => US
[patent_app_date] => 2006-04-07
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 1
[patent_figures_cnt] => 3
[patent_no_of_words] => 3288
[patent_no_of_claims] => 13
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 29
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/08/066/08066228.pdf
[firstpage_image] =>[orig_patent_app_number] => 11911124
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/911124 | Single slotted flap with sliding deflector flap and lowerable spoiler | Apr 6, 2006 | Issued |
Array
(
[id] => 5088581
[patent_doc_number] => 20070228220
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2007-10-04
[patent_title] => 'Two part spacecraft servicing vehicle system with adaptors, tools, and attachment mechanisms'
[patent_app_type] => utility
[patent_app_number] => 11/394743
[patent_app_country] => US
[patent_app_date] => 2006-03-31
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 12
[patent_figures_cnt] => 12
[patent_no_of_words] => 7675
[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/A1/0228/20070228220.pdf
[firstpage_image] =>[orig_patent_app_number] => 11394743
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/394743 | Two part spacecraft servicing vehicle system with adaptors, tools, and attachment mechanisms | Mar 30, 2006 | Issued |
Array
(
[id] => 5088580
[patent_doc_number] => 20070228219
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2007-10-04
[patent_title] => 'Two part spacecraft servicing vehicle system with universal docking adaptor'
[patent_app_type] => utility
[patent_app_number] => 11/394742
[patent_app_country] => US
[patent_app_date] => 2006-03-31
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 12
[patent_figures_cnt] => 12
[patent_no_of_words] => 7675
[patent_no_of_claims] => 19
[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/A1/0228/20070228219.pdf
[firstpage_image] =>[orig_patent_app_number] => 11394742
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/394742 | Two part spacecraft servicing vehicle system with universal docking adaptor | Mar 30, 2006 | Issued |
Array
(
[id] => 5098483
[patent_doc_number] => 20070181743
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2007-08-09
[patent_title] => 'Method for streamline traced external compression inlet'
[patent_app_type] => utility
[patent_app_number] => 11/349656
[patent_app_country] => US
[patent_app_date] => 2006-02-08
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 12
[patent_figures_cnt] => 12
[patent_no_of_words] => 4181
[patent_no_of_claims] => 26
[patent_no_of_ind_claims] => 8
[patent_words_short_claim] => 0
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0181/20070181743.pdf
[firstpage_image] =>[orig_patent_app_number] => 11349656
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/349656 | Method for streamline traced external compression inlet | Feb 7, 2006 | Abandoned |
Array
(
[id] => 4638208
[patent_doc_number] => 08016233
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2011-09-13
[patent_title] => 'Aircraft configuration'
[patent_app_type] => utility
[patent_app_number] => 11/307271
[patent_app_country] => US
[patent_app_date] => 2006-01-30
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 10
[patent_figures_cnt] => 13
[patent_no_of_words] => 3205
[patent_no_of_claims] => 50
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 143
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/08/016/08016233.pdf
[firstpage_image] =>[orig_patent_app_number] => 11307271
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/307271 | Aircraft configuration | Jan 29, 2006 | Issued |
Array
(
[id] => 5703000
[patent_doc_number] => 20060192047
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2006-08-31
[patent_title] => 'Double ducted hovering air-vehicle'
[patent_app_type] => utility
[patent_app_number] => 11/338558
[patent_app_country] => US
[patent_app_date] => 2006-01-24
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 18
[patent_figures_cnt] => 18
[patent_no_of_words] => 4198
[patent_no_of_claims] => 19
[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/A1/0192/20060192047.pdf
[firstpage_image] =>[orig_patent_app_number] => 11338558
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/338558 | Double ducted hovering air-vehicle | Jan 23, 2006 | Issued |
Array
(
[id] => 276828
[patent_doc_number] => 07555893
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2009-07-07
[patent_title] => 'Aircraft propulsion system'
[patent_app_type] => utility
[patent_app_number] => 11/336828
[patent_app_country] => US
[patent_app_date] => 2006-01-23
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 6
[patent_figures_cnt] => 6
[patent_no_of_words] => 7993
[patent_no_of_claims] => 9
[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/07/555/07555893.pdf
[firstpage_image] =>[orig_patent_app_number] => 11336828
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/336828 | Aircraft propulsion system | Jan 22, 2006 | Issued |
11/340817 | Magnetic capture docking mechanism | Jan 19, 2006 | Abandoned |
Array
(
[id] => 5884993
[patent_doc_number] => 20060273928
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2006-12-07
[patent_title] => 'Flight management process for an aircraft'
[patent_app_type] => utility
[patent_app_number] => 11/334548
[patent_app_country] => US
[patent_app_date] => 2006-01-19
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 3
[patent_no_of_words] => 4884
[patent_no_of_claims] => 11
[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/A1/0273/20060273928.pdf
[firstpage_image] =>[orig_patent_app_number] => 11334548
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/334548 | Flight management process for an aircraft | Jan 18, 2006 | Issued |
Array
(
[id] => 5868816
[patent_doc_number] => 20060163433
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2006-07-27
[patent_title] => 'Lighter than air kite'
[patent_app_type] => utility
[patent_app_number] => 11/334108
[patent_app_country] => US
[patent_app_date] => 2006-01-17
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 7
[patent_figures_cnt] => 7
[patent_no_of_words] => 1779
[patent_no_of_claims] => 5
[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/A1/0163/20060163433.pdf
[firstpage_image] =>[orig_patent_app_number] => 11334108
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/334108 | Lighter than air kite | Jan 16, 2006 | Abandoned |
Array
(
[id] => 5185845
[patent_doc_number] => 20070164151
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2007-07-19
[patent_title] => 'Aircraft shock strut and improved bearings therefor'
[patent_app_type] => utility
[patent_app_number] => 11/331506
[patent_app_country] => US
[patent_app_date] => 2006-01-13
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 6
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[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0164/20070164151.pdf
[firstpage_image] =>[orig_patent_app_number] => 11331506
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/331506 | Aircraft shock strut and improved bearings therefor | Jan 12, 2006 | Abandoned |