Medhat Badawi

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Array ( [id] => 8547775 [patent_doc_number] => 08322651 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2012-12-04 [patent_title] => 'Aircraft engine mount structure comprising two thrust links with transverse fitting' [patent_app_type] => utility [patent_app_number] => 12/304772 [patent_app_country] => US [patent_app_date] => 2007-07-09 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 9 [patent_figures_cnt] => 12 [patent_no_of_words] => 4457 [patent_no_of_claims] => 10 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 217 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 12304772 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 8256362 [patent_doc_number] => 08205837 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2012-06-26 [patent_title] => 'Drogue assembly for in-flight refuelling' [patent_app_type] => utility [patent_app_number] => 12/307183 [patent_app_country] => US [patent_app_date] => 2007-06-27 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 5 [patent_figures_cnt] => 6 [patent_no_of_words] => 2295 [patent_no_of_claims] => 26 [patent_no_of_ind_claims] => 4 [patent_words_short_claim] => 121 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 12307183 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 5940508 [patent_doc_number] => 20110101163 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2011-05-05 [patent_title] => 'TAIL STRUCTURE FOR AN AIRCRAFT OR SPACECRAFT' [patent_app_type] => utility [patent_app_number] => 12/300667 [patent_app_country] => US [patent_app_date] => 2007-06-13 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 7 [patent_figures_cnt] => 7 [patent_no_of_words] => 2881 [patent_no_of_claims] => 7 [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/A1/0101/20110101163.pdf [firstpage_image] =>[orig_patent_app_number] => 12300667 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 11230669 [patent_doc_number] => 09457888 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2016-10-04 [patent_title] => 'Method for piloting an aircraft in approach phase' [patent_app_type] => utility [patent_app_number] => 12/304456 [patent_app_country] => US [patent_app_date] => 2007-06-07 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 5 [patent_figures_cnt] => 5 [patent_no_of_words] => 2367 [patent_no_of_claims] => 10 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 303 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 12304456 [rel_patent_id] =>[rel_patent_doc_number] =>)

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Array ( [id] => 8620567 [patent_doc_number] => 08353477 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2013-01-15 [patent_title] => 'Device for the improvement of individual comfort in an airplane' [patent_app_type] => utility [patent_app_number] => 12/301898 [patent_app_country] => US [patent_app_date] => 2007-05-23 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 3 [patent_figures_cnt] => 6 [patent_no_of_words] => 3063 [patent_no_of_claims] => 23 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 106 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 12301898 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 7701864 [patent_doc_number] => 08087614 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2012-01-03 [patent_title] => 'Stringer for an aircraft wing and a method of forming thereof' [patent_app_type] => utility [patent_app_number] => 12/300355 [patent_app_country] => US [patent_app_date] => 2007-05-23 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 3 [patent_figures_cnt] => 5 [patent_no_of_words] => 1806 [patent_no_of_claims] => 21 [patent_no_of_ind_claims] => 4 [patent_words_short_claim] => 119 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/08/087/08087614.pdf [firstpage_image] =>[orig_patent_app_number] => 12300355 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 5425580 [patent_doc_number] => 20090084890 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2009-04-02 [patent_title] => 'Aircraft' [patent_app_type] => utility [patent_app_number] => 12/226650 [patent_app_country] => US [patent_app_date] => 2007-04-25 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 5 [patent_figures_cnt] => 5 [patent_no_of_words] => 3888 [patent_no_of_claims] => 17 [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/A1/0084/20090084890.pdf [firstpage_image] =>[orig_patent_app_number] => 12226650 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 4707908 [patent_doc_number] => 20080296434 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2008-12-04 [patent_title] => 'Parachute-Landing Device for Whole Airplane' [patent_app_type] => utility [patent_app_number] => 12/092266 [patent_app_country] => US [patent_app_date] => 2006-12-31 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 6 [patent_figures_cnt] => 6 [patent_no_of_words] => 2897 [patent_no_of_claims] => 11 [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/A1/0296/20080296434.pdf [firstpage_image] =>[orig_patent_app_number] => 12092266 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 6531240 [patent_doc_number] => 20100270434 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2010-10-28 [patent_title] => 'CONTROLLING THE BOUNDARY LAYER OF AN AIRFOIL' [patent_app_type] => utility [patent_app_number] => 12/096113 [patent_app_country] => US [patent_app_date] => 2006-12-01 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 3 [patent_figures_cnt] => 3 [patent_no_of_words] => 3017 [patent_no_of_claims] => 32 [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/A1/0270/20100270434.pdf [firstpage_image] =>[orig_patent_app_number] => 12096113 [rel_patent_id] =>[rel_patent_doc_number] =>)

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