
Michael A. Fabula
Examiner (ID: 11158, Phone: (571)270-7772 , Office: P/3647 )
| Most Active Art Unit | 3647 |
| Art Unit(s) | 3645, 3644, 3647 |
| Total Applications | 591 |
| Issued Applications | 403 |
| Pending Applications | 4 |
| Abandoned Applications | 187 |
Applications
| Application number | Title of the application | Filing Date | Status |
|---|---|---|---|
Array
(
[id] => 8582542
[patent_doc_number] => 20130001363
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2013-01-03
[patent_title] => 'FILLER PANELS FOR THE SKINS OF AIRCRAFT FUEL TANKS'
[patent_app_type] => utility
[patent_app_number] => 13/339101
[patent_app_country] => US
[patent_app_date] => 2011-12-28
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
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[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13339101
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/339101 | FILLER PANELS FOR THE SKINS OF AIRCRAFT FUEL TANKS | Dec 27, 2011 | Abandoned |
Array
(
[id] => 9316307
[patent_doc_number] => 20140048645
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2014-02-20
[patent_title] => 'LANDING GEAR ASSEMBLY'
[patent_app_type] => utility
[patent_app_number] => 13/978790
[patent_app_country] => US
[patent_app_date] => 2011-12-21
[patent_effective_date] => 0000-00-00
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[rel_patent_id] =>[rel_patent_doc_number] =>) 13/978790 | Landing gear steering using eccentric bearings | Dec 20, 2011 | Issued |
Array
(
[id] => 8651794
[patent_doc_number] => 08371536
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[patent_kind] => B2
[patent_issue_date] => 2013-02-12
[patent_title] => 'Aircraft electrical power transfer assembly'
[patent_app_type] => utility
[patent_app_number] => 13/328164
[patent_app_country] => US
[patent_app_date] => 2011-12-16
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[rel_patent_id] =>[rel_patent_doc_number] =>) 13/328164 | Aircraft electrical power transfer assembly | Dec 15, 2011 | Issued |
Array
(
[id] => 14912957
[patent_doc_number] => 10427784
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2019-10-01
[patent_title] => System and method for improving transition lift-fan performance
[patent_app_type] => utility
[patent_app_number] => 13/311295
[patent_app_country] => US
[patent_app_date] => 2011-12-05
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[rel_patent_id] =>[rel_patent_doc_number] =>) 13/311295 | System and method for improving transition lift-fan performance | Dec 4, 2011 | Issued |
Array
(
[id] => 8224530
[patent_doc_number] => 20120138737
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[patent_kind] => A1
[patent_issue_date] => 2012-06-07
[patent_title] => 'AIRCRAFT POWER DISTRIBUTION ARCHITECTURE'
[patent_app_type] => utility
[patent_app_number] => 13/305941
[patent_app_country] => US
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[rel_patent_id] =>[rel_patent_doc_number] =>) 13/305941 | AIRCRAFT POWER DISTRIBUTION ARCHITECTURE | Nov 28, 2011 | Abandoned |
Array
(
[id] => 10050468
[patent_doc_number] => 09090331
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2015-07-28
[patent_title] => 'Aircraft floor support strut with design failure point'
[patent_app_type] => utility
[patent_app_number] => 13/301908
[patent_app_country] => US
[patent_app_date] => 2011-11-22
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[rel_patent_id] =>[rel_patent_doc_number] =>) 13/301908 | Aircraft floor support strut with design failure point | Nov 21, 2011 | Issued |
Array
(
[id] => 8204643
[patent_doc_number] => 20120126059
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2012-05-24
[patent_title] => 'SEALING DEVICE BETWEEN A CROSS MEMBER AND INSULATION BLANKET PROVIDED AT AN AIRCRAFT FUSELAGE'
[patent_app_type] => utility
[patent_app_number] => 13/302165
[patent_app_country] => US
[patent_app_date] => 2011-11-22
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[firstpage_image] =>[orig_patent_app_number] => 13302165
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/302165 | Sealing device between a cross member and insulation blanket provided at an aircraft fuselage | Nov 21, 2011 | Issued |
Array
(
[id] => 8216887
[patent_doc_number] => 20120132741
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2012-05-31
[patent_title] => 'METHOD OF CONTROLLING A BUOYANCY SYSTEM FOR AN AIRCRAFT, A BUOYANCY SYSTEM IMPLEMENTING SAID METHOD, AND AN AIRCRAFT'
[patent_app_type] => utility
[patent_app_number] => 13/300704
[patent_app_country] => US
[patent_app_date] => 2011-11-21
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
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[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13300704
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/300704 | Method of controlling a buoyancy system for an aircraft, a buoyancy system implementing said method, and an aircraft | Nov 20, 2011 | Issued |
Array
(
[id] => 7805084
[patent_doc_number] => 20120056036
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2012-03-08
[patent_title] => 'MONUMENT WITH AN AUTONOMOUS WATER MODULE'
[patent_app_type] => utility
[patent_app_number] => 13/298792
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[rel_patent_id] =>[rel_patent_doc_number] =>) 13/298792 | Monument with an autonomous water module | Nov 16, 2011 | Issued |
Array
(
[id] => 8204646
[patent_doc_number] => 20120126062
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2012-05-24
[patent_title] => 'INLET NOSE COWL WITH UNINTERRUPTED AIRFLOW SURFACE'
[patent_app_type] => utility
[patent_app_number] => 13/299314
[patent_app_country] => US
[patent_app_date] => 2011-11-17
[patent_effective_date] => 0000-00-00
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[firstpage_image] =>[orig_patent_app_number] => 13299314
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/299314 | Inlet nose cowl with a locally thickened fastening portion to enable an uninterrupted airflow surface | Nov 16, 2011 | Issued |
Array
(
[id] => 8818146
[patent_doc_number] => 20130119191
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2013-05-16
[patent_title] => 'LOAD-BEARING STRUCTURES FOR AIRCRAFT ENGINES AND PROCESSES THEREFOR'
[patent_app_type] => utility
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[rel_patent_id] =>[rel_patent_doc_number] =>) 13/293677 | LOAD-BEARING STRUCTURES FOR AIRCRAFT ENGINES AND PROCESSES THEREFOR | Nov 9, 2011 | Abandoned |
Array
(
[id] => 8462309
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[patent_title] => 'Valve stem access system for aircraft'
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[rel_patent_id] =>[rel_patent_doc_number] =>) 13/200939 | Valve stem access system for aircraft | Oct 4, 2011 | Abandoned |
Array
(
[id] => 9298504
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[patent_title] => 'Marine vessel-towable aerovehicle system with automated tow line release'
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[rel_patent_id] =>[rel_patent_doc_number] =>) 13/215034 | Marine vessel-towable aerovehicle system with automated tow line release | Aug 21, 2011 | Issued |
Array
(
[id] => 9709141
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[patent_title] => 'Overhead luggage compartment for vehicle cabin'
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[rel_patent_id] =>[rel_patent_doc_number] =>) 13/207912 | Overhead luggage compartment for vehicle cabin | Aug 10, 2011 | Issued |
Array
(
[id] => 7805081
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[patent_kind] => A1
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[patent_title] => 'PYLON FOR ATTACHING AN AIRCRAFT TURBINE ENGINE COMPRISING ALIGNED FRONT WING TIES'
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[rel_patent_id] =>[rel_patent_doc_number] =>) 13/205995 | Pylon for attaching an aircraft turbine engine comprising aligned front wing ties | Aug 8, 2011 | Issued |
Array
(
[id] => 9508538
[patent_doc_number] => 20140145029
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[patent_title] => 'RUDDER BIAS GAIN CHANGER'
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[rel_patent_id] =>[rel_patent_doc_number] =>) 14/232408 | Rudder bias gain changer | Jul 25, 2011 | Issued |
Array
(
[id] => 5930111
[patent_doc_number] => 20110209319
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[patent_title] => 'PHOTOSENSITIVE COCKPIT WINDSHIELD'
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[rel_patent_id] =>[rel_patent_doc_number] =>) 13/107949 | PHOTOSENSITIVE COCKPIT WINDSHIELD | May 14, 2011 | Abandoned |
Array
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Array
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Array
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[rel_patent_id] =>[rel_patent_doc_number] =>) 13/042568 | KITE MESSENGER | Mar 7, 2011 | Abandoned |