Medhat Badawi

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Array ( [id] => 6239666 [patent_doc_number] => 20100133382 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2010-06-03 [patent_title] => 'WING-FUSELAGE SECTION OF AN AIRCRAFT' [patent_app_type] => utility [patent_app_number] => 12/597250 [patent_app_country] => US [patent_app_date] => 2008-04-21 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 13 [patent_figures_cnt] => 13 [patent_no_of_words] => 3266 [patent_no_of_claims] => 24 [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/A1/0133/20100133382.pdf [firstpage_image] =>[orig_patent_app_number] => 12597250 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 8079089 [patent_doc_number] => 08146856 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2012-04-03 [patent_title] => 'Device for attaching an aircraft engine and aircraft comprising at least one such device' [patent_app_type] => utility [patent_app_number] => 12/596555 [patent_app_country] => US [patent_app_date] => 2008-04-18 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 4 [patent_figures_cnt] => 5 [patent_no_of_words] => 5117 [patent_no_of_claims] => 9 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 216 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/08/146/08146856.pdf [firstpage_image] =>[orig_patent_app_number] => 12596555 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 6271218 [patent_doc_number] => 20100116926 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2010-05-13 [patent_title] => 'DEVICE FOR ATTACHING AN AIRCRAFT ENGINE AND AIRCRAFT COMPRISING AT LEAST ONE SUCH DEVICE' [patent_app_type] => utility [patent_app_number] => 12/594455 [patent_app_country] => US [patent_app_date] => 2008-04-11 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 5 [patent_figures_cnt] => 5 [patent_no_of_words] => 4610 [patent_no_of_claims] => 11 [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/A1/0116/20100116926.pdf [firstpage_image] =>[orig_patent_app_number] => 12594455 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 6391144 [patent_doc_number] => 20100163685 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2010-07-01 [patent_title] => 'WING' [patent_app_type] => utility [patent_app_number] => 12/449886 [patent_app_country] => US [patent_app_date] => 2008-03-07 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 29 [patent_figures_cnt] => 29 [patent_no_of_words] => 4845 [patent_no_of_claims] => 20 [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/A1/0163/20100163685.pdf [firstpage_image] =>[orig_patent_app_number] => 12449886 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 6445190 [patent_doc_number] => 20100038473 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2010-02-18 [patent_title] => 'Aircraft Propeller Device, Method for Driving an Aircraft Propeller, Use of a Bearing for an Aircraft Propeller Drive and Use of an Electric Machine' [patent_app_type] => utility [patent_app_number] => 12/448900 [patent_app_country] => US [patent_app_date] => 2008-01-14 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 9 [patent_figures_cnt] => 9 [patent_no_of_words] => 8391 [patent_no_of_claims] => 34 [patent_no_of_ind_claims] => 5 [patent_words_short_claim] => 0 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] => publications/A1/0038/20100038473.pdf [firstpage_image] =>[orig_patent_app_number] => 12448900 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 8673934 [patent_doc_number] => 08382038 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2013-02-26 [patent_title] => 'Device, in particular connection rod, for bracing a fuselage structure of an aircraft and/or for fastening a component' [patent_app_type] => utility [patent_app_number] => 12/521247 [patent_app_country] => US [patent_app_date] => 2008-01-11 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 6 [patent_figures_cnt] => 10 [patent_no_of_words] => 3685 [patent_no_of_claims] => 13 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 171 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 12521247 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 8570187 [patent_doc_number] => 08336823 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2012-12-25 [patent_title] => 'Aircraft fuselage' [patent_app_type] => utility [patent_app_number] => 12/520881 [patent_app_country] => US [patent_app_date] => 2007-12-21 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 6 [patent_figures_cnt] => 19 [patent_no_of_words] => 3557 [patent_no_of_claims] => 12 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 105 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 12520881 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 6230878 [patent_doc_number] => 20100264267 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2010-10-21 [patent_title] => 'FIXING RAIL FOR ATTACHING LOADING DEVICES TO THE LOADING DECK OF AN AIRCRAFT' [patent_app_type] => utility [patent_app_number] => 11/961819 [patent_app_country] => US [patent_app_date] => 2007-12-20 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 9 [patent_figures_cnt] => 9 [patent_no_of_words] => 2829 [patent_no_of_claims] => 12 [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/A1/0264/20100264267.pdf [firstpage_image] =>[orig_patent_app_number] => 11961819 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 5955393 [patent_doc_number] => 20110180669 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2011-07-28 [patent_title] => 'Inflatable nested toroid structure' [patent_app_type] => utility [patent_app_number] => 11/956826 [patent_app_country] => US [patent_app_date] => 2007-12-14 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 12 [patent_figures_cnt] => 12 [patent_no_of_words] => 6758 [patent_no_of_claims] => 18 [patent_no_of_ind_claims] => 5 [patent_words_short_claim] => 0 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] => publications/A1/0180/20110180669.pdf [firstpage_image] =>[orig_patent_app_number] => 11956826 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 8268976 [patent_doc_number] => 08210477 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2012-07-03 [patent_title] => 'Vibrations damper for fastenings elements in aircrafts' [patent_app_type] => utility [patent_app_number] => 12/518065 [patent_app_country] => US [patent_app_date] => 2007-12-06 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 4 [patent_figures_cnt] => 7 [patent_no_of_words] => 3513 [patent_no_of_claims] => 3 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 198 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 12518065 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 6476488 [patent_doc_number] => 20100213318 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2010-08-26 [patent_title] => 'CONDUCTIVE BODIES' [patent_app_type] => utility [patent_app_number] => 12/514702 [patent_app_country] => US [patent_app_date] => 2007-11-13 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 4 [patent_figures_cnt] => 4 [patent_no_of_words] => 3261 [patent_no_of_claims] => 20 [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/A1/0213/20100213318.pdf [firstpage_image] =>[orig_patent_app_number] => 12514702 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 6505523 [patent_doc_number] => 20100219299 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2010-09-02 [patent_title] => 'HIGH-LIFT SYSTEM ON THE WING OF AN AIRCRAFT, AND METHOD FOR ITS OPERATION' [patent_app_type] => utility [patent_app_number] => 12/514379 [patent_app_country] => US [patent_app_date] => 2007-11-12 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 4 [patent_figures_cnt] => 4 [patent_no_of_words] => 5775 [patent_no_of_claims] => 40 [patent_no_of_ind_claims] => 16 [patent_words_short_claim] => 0 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] => publications/A1/0219/20100219299.pdf [firstpage_image] =>[orig_patent_app_number] => 12514379 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 6468732 [patent_doc_number] => 20100206983 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2010-08-19 [patent_title] => 'Crash Attenuation System for Aircraft' [patent_app_type] => utility [patent_app_number] => 12/679563 [patent_app_country] => US [patent_app_date] => 2007-10-22 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 12 [patent_figures_cnt] => 12 [patent_no_of_words] => 3160 [patent_no_of_claims] => 20 [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/A1/0206/20100206983.pdf [firstpage_image] =>[orig_patent_app_number] => 12679563 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 5561425 [patent_doc_number] => 20090134277 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2009-05-28 [patent_title] => 'LIFESAVING PARACHUTE' [patent_app_type] => utility [patent_app_number] => 12/279488 [patent_app_country] => US [patent_app_date] => 2007-10-16 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 4 [patent_figures_cnt] => 4 [patent_no_of_words] => 1947 [patent_no_of_claims] => 3 [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/A1/0134/20090134277.pdf [firstpage_image] =>[orig_patent_app_number] => 12279488 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 8338692 [patent_doc_number] => 08240612 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2012-08-14 [patent_title] => 'Device for controlling the heat flows in a spacecraft and spacecraft equipped with such a device' [patent_app_type] => utility [patent_app_number] => 12/440575 [patent_app_country] => US [patent_app_date] => 2007-09-11 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 7 [patent_figures_cnt] => 20 [patent_no_of_words] => 6819 [patent_no_of_claims] => 15 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 108 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 12440575 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 6461464 [patent_doc_number] => 20100006695 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2010-01-14 [patent_title] => 'VERTICAL TAKE-OFF AND LANDING VEHICLE WHICH DOES NOT HAVE A ROTARY WING' [patent_app_type] => utility [patent_app_number] => 12/442778 [patent_app_country] => US [patent_app_date] => 2007-09-10 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 5 [patent_figures_cnt] => 5 [patent_no_of_words] => 1997 [patent_no_of_claims] => 7 [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/A1/0006/20100006695.pdf [firstpage_image] =>[orig_patent_app_number] => 12442778 [rel_patent_id] =>[rel_patent_doc_number] =>)

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Array ( [id] => 7985295 [patent_doc_number] => 08074940 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2011-12-13 [patent_title] => 'Control stick adapted for use in a fly-by-wire flight control system, and linkage for use therein' [patent_app_type] => utility [patent_app_number] => 12/311125 [patent_app_country] => US [patent_app_date] => 2007-08-08 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 5 [patent_figures_cnt] => 10 [patent_no_of_words] => 6809 [patent_no_of_claims] => 15 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 185 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/08/074/08074940.pdf [firstpage_image] =>[orig_patent_app_number] => 12311125 [rel_patent_id] =>[rel_patent_doc_number] =>)

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