Search

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 numberTitle of the applicationFiling DateStatus
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 [patent_words_short_claim] => 0 [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 [patent_figures_cnt] => 4 [patent_no_of_words] => 3075 [patent_no_of_claims] => 6 [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/A1/0192/20110192933.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 [patent_figures_cnt] => 24 [patent_no_of_words] => 3172 [patent_no_of_claims] => 5 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 319 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [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 [patent_figures_cnt] => 9 [patent_no_of_words] => 2496 [patent_no_of_claims] => 17 [patent_no_of_ind_claims] => 11 [patent_words_short_claim] => 0 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [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 [patent_figures_cnt] => 3 [patent_no_of_words] => 3745 [patent_no_of_claims] => 9 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 147 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [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 [patent_figures_cnt] => 9 [patent_no_of_words] => 7497 [patent_no_of_claims] => 15 [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/A1/0127/20100127117.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 [patent_kind] => B2 [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 [patent_figures_cnt] => 7 [patent_no_of_words] => 1579 [patent_no_of_claims] => 4 [patent_no_of_ind_claims] => 4 [patent_words_short_claim] => 179 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [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 [patent_figures_cnt] => 6 [patent_no_of_words] => 1708 [patent_no_of_claims] => 9 [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/A1/0108/20100108822.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 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 12 [patent_figures_cnt] => 27 [patent_no_of_words] => 14082 [patent_no_of_claims] => 20 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 295 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 12593667 [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 [patent_drawing_sheets_cnt] => 6 [patent_figures_cnt] => 6 [patent_no_of_words] => 3414 [patent_no_of_claims] => 18 [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/A1/0243/20100243813.pdf [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 [patent_figures_cnt] => 4 [patent_no_of_words] => 6591 [patent_no_of_claims] => 19 [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/A1/0051/20100051743.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 [patent_country] => US [patent_kind] => B2 [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 [patent_app_date] => 2008-03-05 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 4 [patent_figures_cnt] => 5 [patent_no_of_words] => 2670 [patent_no_of_claims] => 20 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 127 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [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 [patent_country] => US [patent_kind] => B2 [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 [patent_app_country] => US [patent_app_date] => 2008-02-25 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 3 [patent_figures_cnt] => 6 [patent_no_of_words] => 5600 [patent_no_of_claims] => 3 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 277 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 12449705 [rel_patent_id] =>[rel_patent_doc_number] =>)
12/449705
Spoiler for an aerodynamic body of an aircraft Feb 24, 2008 Issued
Array ( [id] => 8012363 [patent_doc_number] => 08100029 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2012-01-24 [patent_title] => 'Control inceptor systems and associated methods' [patent_app_type] => utility [patent_app_number] => 12/029435 [patent_app_country] => US [patent_app_date] => 2008-02-11 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 5 [patent_figures_cnt] => 5 [patent_no_of_words] => 6565 [patent_no_of_claims] => 33 [patent_no_of_ind_claims] => 4 [patent_words_short_claim] => 203 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [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 [patent_kind] => B2 [patent_issue_date] => 2014-12-30 [patent_title] => 'Inflatable delta-shaped traction kite' [patent_app_type] => utility [patent_app_number] => 12/525153 [patent_app_country] => US [patent_app_date] => 2008-01-31 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 4 [patent_figures_cnt] => 8 [patent_no_of_words] => 3191 [patent_no_of_claims] => 13 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 255 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 12525153 [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 [patent_app_number] => 12/520890 [patent_app_country] => US [patent_app_date] => 2008-01-23 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 3 [patent_figures_cnt] => 3 [patent_no_of_words] => 3410 [patent_no_of_claims] => 14 [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/A1/0025/20100025532.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 [patent_app_number] => 12/520893 [patent_app_country] => US [patent_app_date] => 2008-01-18 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 3 [patent_figures_cnt] => 3 [patent_no_of_words] => 2952 [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/A1/0090/20100090061.pdf [firstpage_image] =>[orig_patent_app_number] => 12520893 [rel_patent_id] =>[rel_patent_doc_number] =>)
12/520893
FUSELAGE OF AN AIRCRAFT OR SPACECRAFT OF CRP/METAL HYBRID CONSTRUCTION WITH A METAL FRAMEWORK Jan 17, 2008 Abandoned
Array ( [id] => 6445280 [patent_doc_number] => 20100038487 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2010-02-18 [patent_title] => 'FUSELAGE STRUCTURAL COMPONENT OF AN AIRCRAFT OR SPACECRAFT, WITH A FOAM LAYER AS THERMAL INSULATION' [patent_app_type] => utility [patent_app_number] => 12/520892 [patent_app_country] => US [patent_app_date] => 2008-01-18 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 2 [patent_figures_cnt] => 2 [patent_no_of_words] => 3301 [patent_no_of_claims] => 16 [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/A1/0038/20100038487.pdf [firstpage_image] =>[orig_patent_app_number] => 12520892 [rel_patent_id] =>[rel_patent_doc_number] =>)
12/520892
FUSELAGE STRUCTURAL COMPONENT OF AN AIRCRAFT OR SPACECRAFT, WITH A FOAM LAYER AS THERMAL INSULATION Jan 17, 2008 Abandoned
Array ( [id] => 6588546 [patent_doc_number] => 20100001126 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2010-01-07 [patent_title] => 'COATING OF AN AIRCRAFT SEAT MOUNTING RAIL OR A AIRCRAFT SEAT STUD' [patent_app_type] => utility [patent_app_number] => 12/522739 [patent_app_country] => US [patent_app_date] => 2008-01-11 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 6 [patent_figures_cnt] => 6 [patent_no_of_words] => 5606 [patent_no_of_claims] => 30 [patent_no_of_ind_claims] => 15 [patent_words_short_claim] => 0 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] => publications/A1/0001/20100001126.pdf [firstpage_image] =>[orig_patent_app_number] => 12522739 [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 [patent_doc_number] => 08528857 [patent_country] => US [patent_kind] => B2 [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 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 5 [patent_figures_cnt] => 10 [patent_no_of_words] => 3298 [patent_no_of_claims] => 7 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 146 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 12517299 [rel_patent_id] =>[rel_patent_doc_number] =>)
12/517299
Translatable jet engine thrust reverser configuration providing improved maintenance access Nov 18, 2007 Issued
Menu