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] => 8662814
[patent_doc_number] => 08376270
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2013-02-19
[patent_title] => 'Structural dynamic stability for an aircraft'
[patent_app_type] => utility
[patent_app_number] => 13/323471
[patent_app_country] => US
[patent_app_date] => 2011-12-12
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
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[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13323471
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/323471 | Structural dynamic stability for an aircraft | Dec 11, 2011 | Issued |
Array
(
[id] => 8089919
[patent_doc_number] => 20120080563
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2012-04-05
[patent_title] => 'ROBOTIC SATELLITE REFUELING TOOL'
[patent_app_type] => utility
[patent_app_number] => 13/323472
[patent_app_country] => US
[patent_app_date] => 2011-12-12
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 17
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[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0080/20120080563.pdf
[firstpage_image] =>[orig_patent_app_number] => 13323472
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/323472 | Robotic satellite refueling tool | Dec 11, 2011 | Issued |
Array
(
[id] => 9231281
[patent_doc_number] => 08596581
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2013-12-03
[patent_title] => 'Power generating and distribution system and method'
[patent_app_type] => utility
[patent_app_number] => 13/323585
[patent_app_country] => US
[patent_app_date] => 2011-12-12
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 16
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[rel_patent_id] =>[rel_patent_doc_number] =>) 13/323585 | Power generating and distribution system and method | Dec 11, 2011 | Issued |
Array
(
[id] => 7781868
[patent_doc_number] => 20120043424
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2012-02-23
[patent_title] => 'DROGUE DEPLOYING/RETRIEVAL METHOD'
[patent_app_type] => utility
[patent_app_number] => 13/286207
[patent_app_country] => US
[patent_app_date] => 2011-10-31
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 10
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[patent_no_of_words] => 3345
[patent_no_of_claims] => 20
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[pdf_file] => publications/A1/0043/20120043424.pdf
[firstpage_image] =>[orig_patent_app_number] => 13286207
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/286207 | Drogue deploying/retrieval method | Oct 30, 2011 | Issued |
Array
(
[id] => 7784053
[patent_doc_number] => 20120045609
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2012-02-23
[patent_title] => 'COMPOSITE STRINGER WITH WEB TRANSITION'
[patent_app_type] => utility
[patent_app_number] => 13/284927
[patent_app_country] => US
[patent_app_date] => 2011-10-30
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 28
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[pdf_file] => publications/A1/0045/20120045609.pdf
[firstpage_image] =>[orig_patent_app_number] => 13284927
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/284927 | Composite stringer with web transition | Oct 29, 2011 | Issued |
Array
(
[id] => 8549662
[patent_doc_number] => 08324545
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2012-12-04
[patent_title] => 'Foldable and deployable panel'
[patent_app_type] => utility
[patent_app_number] => 13/283048
[patent_app_country] => US
[patent_app_date] => 2011-10-27
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
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[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13283048
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/283048 | Foldable and deployable panel | Oct 26, 2011 | Issued |
Array
(
[id] => 8384626
[patent_doc_number] => 08262019
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2012-09-11
[patent_title] => 'Method and system for health monitoring of aircraft landing gear'
[patent_app_type] => utility
[patent_app_number] => 13/271468
[patent_app_country] => US
[patent_app_date] => 2011-10-12
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 9
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[patent_no_of_claims] => 27
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[patent_maintenance] => 1
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[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13271468
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/271468 | Method and system for health monitoring of aircraft landing gear | Oct 11, 2011 | Issued |
Array
(
[id] => 8350650
[patent_doc_number] => 08245969
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2012-08-21
[patent_title] => 'Plug-n-play power system for an accessory in an aircraft'
[patent_app_type] => utility
[patent_app_number] => 13/253787
[patent_app_country] => US
[patent_app_date] => 2011-10-05
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 10
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[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13253787
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/253787 | Plug-n-play power system for an accessory in an aircraft | Oct 4, 2011 | Issued |
Array
(
[id] => 7666542
[patent_doc_number] => 20110315811
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2011-12-29
[patent_title] => 'LIGHTER-THAN-AIR VEHICLE FOR SHADING'
[patent_app_type] => utility
[patent_app_number] => 13/226382
[patent_app_country] => US
[patent_app_date] => 2011-09-06
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 13
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[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13226382
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/226382 | Lighter-than-air vehicle for shading | Sep 5, 2011 | Issued |
Array
(
[id] => 10896493
[patent_doc_number] => 08919694
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2014-12-30
[patent_title] => 'Skid landing gear system'
[patent_app_type] => utility
[patent_app_number] => 13/700020
[patent_app_country] => US
[patent_app_date] => 2011-08-02
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 8
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[patent_no_of_words] => 3238
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[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13700020
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/700020 | Skid landing gear system | Aug 1, 2011 | Issued |
Array
(
[id] => 8179655
[patent_doc_number] => 20120112009
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2012-05-10
[patent_title] => 'SATELLITE REFUELLING SYSTEM AND METHOD'
[patent_app_type] => utility
[patent_app_number] => 13/196750
[patent_app_country] => US
[patent_app_date] => 2011-08-02
[patent_effective_date] => 0000-00-00
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[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0112/20120112009.pdf
[firstpage_image] =>[orig_patent_app_number] => 13196750
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/196750 | Satellite refuelling system and method | Aug 1, 2011 | Issued |
Array
(
[id] => 8937206
[patent_doc_number] => 20130187003
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2013-07-25
[patent_title] => 'Headrest Assembly'
[patent_app_type] => utility
[patent_app_number] => 13/813403
[patent_app_country] => US
[patent_app_date] => 2011-07-29
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[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13813403
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/813403 | Headrest assembly | Jul 28, 2011 | Issued |
Array
(
[id] => 8519500
[patent_doc_number] => 20120318908
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2012-12-20
[patent_title] => 'VTOL twin fuselage amphibious aircraft with tilt-center wing, engine and rotor'
[patent_app_type] => utility
[patent_app_number] => 13/134864
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[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13134864
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/134864 | VTOL twin fuselage amphibious aircraft with tilt-center wing, engine and rotor | Jun 19, 2011 | Issued |
Array
(
[id] => 7700245
[patent_doc_number] => 20110226345
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2011-09-22
[patent_title] => 'Deployable Aerodynamic Devices with Reduced Actuator Loads'
[patent_app_type] => utility
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[firstpage_image] =>[orig_patent_app_number] => 13150334
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/150334 | Deployable aerodynamic devices with reduced actuator loads | May 31, 2011 | Issued |
Array
(
[id] => 9215252
[patent_doc_number] => 08628046
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2014-01-14
[patent_title] => 'Control system'
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[rel_patent_id] =>[rel_patent_doc_number] =>) 13/116117 | Control system | May 25, 2011 | Issued |
Array
(
[id] => 7659932
[patent_doc_number] => 20110309201
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[patent_kind] => A1
[patent_issue_date] => 2011-12-22
[patent_title] => 'ACTIVE FLOW CONTROL FOR TRANSONIC FLIGHT'
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[pdf_file] => publications/A1/0309/20110309201.pdf
[firstpage_image] =>[orig_patent_app_number] => 13114006
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/114006 | Active flow control for transonic flight | May 22, 2011 | Issued |
Array
(
[id] => 8402924
[patent_doc_number] => 20120234978
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[patent_kind] => A1
[patent_issue_date] => 2012-09-20
[patent_title] => 'LOAD TRANSFER DEVICES AT A STRINGER RUN-OUT'
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[rel_patent_id] =>[rel_patent_doc_number] =>) 13/112269 | LOAD TRANSFER DEVICES AT A STRINGER RUN-OUT | May 19, 2011 | Abandoned |
Array
(
[id] => 9215248
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[patent_issue_date] => 2014-01-14
[patent_title] => 'Electrical power supply and control device for equipment of a rotor, and an aircraft fitted with such a device'
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Array
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Array
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[rel_patent_id] =>[rel_patent_doc_number] =>) 13/097237 | Circumferential stiffener for an aircraft fuselage | Apr 28, 2011 | Issued |