
Michael A. Fabula
Examiner (ID: 7653, 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] => 6505452
[patent_doc_number] => 20100219291
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2010-09-02
[patent_title] => 'AIRCRAFT HOLD INTENDED TO ACCOMMODATE BAGGAGE'
[patent_app_type] => utility
[patent_app_number] => 12/597990
[patent_app_country] => US
[patent_app_date] => 2008-06-13
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 4
[patent_no_of_words] => 4009
[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] => publication
[pdf_file] => publications/A1/0219/20100219291.pdf
[firstpage_image] =>[orig_patent_app_number] => 12597990
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/597990 | Aircraft hold with deployable bench to accommodate baggage stowage | Jun 12, 2008 | Issued |
Array
(
[id] => 6160710
[patent_doc_number] => 20110192933
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2011-08-11
[patent_title] => 'MAST FOR SECURING AN ENGINE TO AN AIRCRAFT WING'
[patent_app_type] => utility
[patent_app_number] => 12/601650
[patent_app_country] => US
[patent_app_date] => 2008-05-15
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
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[patent_no_of_words] => 3075
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[pdf_file] => publications/A1/0192/20110192933.pdf
[firstpage_image] =>[orig_patent_app_number] => 12601650
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/601650 | Mast having modifiable geometry for securing an engine to an aircraft wing | May 14, 2008 | Issued |
Array
(
[id] => 8553669
[patent_doc_number] => 08328136
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2012-12-11
[patent_title] => 'Aircraft applying multisystem connection devices'
[patent_app_type] => utility
[patent_app_number] => 12/598210
[patent_app_country] => US
[patent_app_date] => 2008-04-29
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 8
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[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 12598210
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/598210 | Aircraft applying multisystem connection devices | Apr 28, 2008 | Issued |
Array
(
[id] => 6279308
[patent_doc_number] => 20100155531
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2010-06-24
[patent_title] => 'AIRCRAFT TOILET FACILITY'
[patent_app_type] => utility
[patent_app_number] => 12/596985
[patent_app_country] => US
[patent_app_date] => 2008-04-23
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 9
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[patent_no_of_words] => 2496
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[pdf_file] => publications/A1/0155/20100155531.pdf
[firstpage_image] =>[orig_patent_app_number] => 12596985
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/596985 | Aircraft toilet facility | Apr 22, 2008 | Issued |
Array
(
[id] => 8150755
[patent_doc_number] => 08167238
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2012-05-01
[patent_title] => 'Pylon caisson attachment on a wing, gripping a lateral panel of the caisson'
[patent_app_type] => utility
[patent_app_number] => 12/596784
[patent_app_country] => US
[patent_app_date] => 2008-04-22
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
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[patent_no_of_words] => 3745
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[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/08/167/08167238.pdf
[firstpage_image] =>[orig_patent_app_number] => 12596784
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/596784 | Pylon caisson attachment on a wing, gripping a lateral panel of the caisson | Apr 21, 2008 | Issued |
Array
(
[id] => 6546380
[patent_doc_number] => 20100127117
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2010-05-27
[patent_title] => 'ATTACHMENT PYLON FOR AIRCRAFT HAVING A REAR ENGINE ATTACHMENT BEAM OFFSET FROM THE CAISSON'
[patent_app_type] => utility
[patent_app_number] => 12/596501
[patent_app_country] => US
[patent_app_date] => 2008-04-18
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 9
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[pdf_file] => publications/A1/0127/20100127117.pdf
[firstpage_image] =>[orig_patent_app_number] => 12596501
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/596501 | Attachment pylon for aircraft having a rear engine attachment beam offset from the caisson | Apr 17, 2008 | Issued |
Array
(
[id] => 8243842
[patent_doc_number] => 08201772
[patent_country] => US
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[patent_issue_date] => 2012-06-19
[patent_title] => 'Method for suppressing vibration and acoustic signature in a tiltrotor aircraft'
[patent_app_type] => utility
[patent_app_number] => 12/595286
[patent_app_country] => US
[patent_app_date] => 2008-04-11
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
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[patent_no_of_words] => 1579
[patent_no_of_claims] => 4
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[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/08/201/08201772.pdf
[firstpage_image] =>[orig_patent_app_number] => 12595286
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/595286 | Method for suppressing vibration and acoustic signature in a tiltrotor aircraft | Apr 10, 2008 | Issued |
Array
(
[id] => 6303470
[patent_doc_number] => 20100108822
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2010-05-06
[patent_title] => 'Method for Suppressing Vibration in a Tiltrotor Aircraft'
[patent_app_type] => utility
[patent_app_number] => 12/595295
[patent_app_country] => US
[patent_app_date] => 2008-04-11
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 6
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[patent_no_of_words] => 1708
[patent_no_of_claims] => 9
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[pdf_file] => publications/A1/0108/20100108822.pdf
[firstpage_image] =>[orig_patent_app_number] => 12595295
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/595295 | Method for suppressing vibration in a tiltrotor aircraft | Apr 10, 2008 | Issued |
Array
(
[id] => 9624905
[patent_doc_number] => 08794574
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2014-08-05
[patent_title] => 'Micro-array surface for passive drag modification'
[patent_app_type] => utility
[patent_app_number] => 12/593667
[patent_app_country] => US
[patent_app_date] => 2008-03-31
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[rel_patent_id] =>[rel_patent_doc_number] =>) 12/593667 | Micro-array surface for passive drag modification | Mar 30, 2008 | Issued |
Array
(
[id] => 6319885
[patent_doc_number] => 20100243813
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2010-09-30
[patent_title] => 'SYSTEM FOR TRANSPORTATION OF GOODS IN A LOADING SPACE'
[patent_app_type] => utility
[patent_app_number] => 12/593278
[patent_app_country] => US
[patent_app_date] => 2008-03-19
[patent_effective_date] => 0000-00-00
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[firstpage_image] =>[orig_patent_app_number] => 12593278
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/593278 | System for transportation of goods in a loading space | Mar 18, 2008 | Issued |
Array
(
[id] => 6215395
[patent_doc_number] => 20100051743
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2010-03-04
[patent_title] => 'REAR LOWER AERODYNAMIC FAIRING FOR THE ATTACHMENT DEVICE OF AN AIRCRAFT ENGINE'
[patent_app_type] => utility
[patent_app_number] => 12/528646
[patent_app_country] => US
[patent_app_date] => 2008-03-13
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
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[pdf_file] => publications/A1/0051/20100051743.pdf
[firstpage_image] =>[orig_patent_app_number] => 12528646
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/528646 | Rear lower aerodynamic fairing for the attachment device of an aircraft engine | Mar 12, 2008 | Issued |
Array
(
[id] => 9284673
[patent_doc_number] => 08640992
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[patent_issue_date] => 2014-02-04
[patent_title] => 'Drill-elastic and flexurally rigid rod element for the support and guidance of a movable flap relative to a wing of an aircraft'
[patent_app_type] => utility
[patent_app_number] => 12/530913
[patent_app_country] => US
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[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 12530913
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/530913 | Drill-elastic and flexurally rigid rod element for the support and guidance of a movable flap relative to a wing of an aircraft | Mar 4, 2008 | Issued |
Array
(
[id] => 9310219
[patent_doc_number] => 08651430
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[patent_issue_date] => 2014-02-18
[patent_title] => 'Spoiler for an aerodynamic body of an aircraft'
[patent_app_type] => utility
[patent_app_number] => 12/449705
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[rel_patent_id] =>[rel_patent_doc_number] =>) 12/449705 | Spoiler for an aerodynamic body of an aircraft | Feb 24, 2008 | Issued |
Array
(
[id] => 8012363
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[patent_title] => 'Control inceptor systems and associated methods'
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[pdf_file] => patents/08/100/08100029.pdf
[firstpage_image] =>[orig_patent_app_number] => 12029435
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/029435 | Control inceptor systems and associated methods | Feb 10, 2008 | Issued |
Array
(
[id] => 10896500
[patent_doc_number] => 08919701
[patent_country] => US
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[patent_issue_date] => 2014-12-30
[patent_title] => 'Inflatable delta-shaped traction kite'
[patent_app_type] => utility
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[rel_patent_id] =>[rel_patent_doc_number] =>) 12/525153 | Inflatable delta-shaped traction kite | Jan 30, 2008 | Issued |
Array
(
[id] => 6246783
[patent_doc_number] => 20100025532
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2010-02-04
[patent_title] => 'SHELL ELEMENT AS PART OF AN AIRCRFAFT FUSELAGE'
[patent_app_type] => utility
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[pdf_file] => publications/A1/0025/20100025532.pdf
[firstpage_image] =>[orig_patent_app_number] => 12520890
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/520890 | SHELL ELEMENT AS PART OF AN AIRCRFAFT FUSELAGE | Jan 22, 2008 | Abandoned |
Array
(
[id] => 6455487
[patent_doc_number] => 20100090061
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2010-04-15
[patent_title] => 'FUSELAGE OF AN AIRCRAFT OR SPACECRAFT OF CRP/METAL HYBRID CONSTRUCTION WITH A METAL FRAMEWORK'
[patent_app_type] => utility
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Array
(
[id] => 6445280
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Array
(
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[rel_patent_id] =>[rel_patent_doc_number] =>) 12/522739 | COATING OF AN AIRCRAFT SEAT MOUNTING RAIL OR A AIRCRAFT SEAT STUD | Jan 10, 2008 | Abandoned |
Array
(
[id] => 9018876
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[patent_issue_date] => 2013-09-10
[patent_title] => 'Translatable jet engine thrust reverser configuration providing improved maintenance access'
[patent_app_type] => utility
[patent_app_number] => 12/517299
[patent_app_country] => US
[patent_app_date] => 2007-11-19
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[rel_patent_id] =>[rel_patent_doc_number] =>) 12/517299 | Translatable jet engine thrust reverser configuration providing improved maintenance access | Nov 18, 2007 | Issued |