Medhat Badawi

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Array ( [id] => 8373909 [patent_doc_number] => 08256703 [patent_country] => US [patent_kind] => B1 [patent_issue_date] => 2012-09-04 [patent_title] => 'Aircraft ground maintenance tether asssembly' [patent_app_type] => utility [patent_app_number] => 12/819326 [patent_app_country] => US [patent_app_date] => 2010-06-21 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 6 [patent_figures_cnt] => 6 [patent_no_of_words] => 2274 [patent_no_of_claims] => 6 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 214 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 12819326 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 9400050 [patent_doc_number] => 08690096 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2014-04-08 [patent_title] => 'Aircraft with dual flight regimes' [patent_app_type] => utility [patent_app_number] => 12/802104 [patent_app_country] => US [patent_app_date] => 2010-05-29 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 8 [patent_figures_cnt] => 17 [patent_no_of_words] => 5283 [patent_no_of_claims] => 9 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 205 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 12802104 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 8811769 [patent_doc_number] => 20130112814 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2013-05-09 [patent_title] => 'DROOP PANEL LINKAGE' [patent_app_type] => utility [patent_app_number] => 13/699025 [patent_app_country] => US [patent_app_date] => 2010-05-21 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 5 [patent_figures_cnt] => 5 [patent_no_of_words] => 2392 [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] =>[firstpage_image] =>[orig_patent_app_number] => 13699025 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 7805079 [patent_doc_number] => 20120056031 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2012-03-08 [patent_title] => 'Method for Compensation of Gyroscopic Forces of a Rotor in a Helicopter' [patent_app_type] => utility [patent_app_number] => 13/318484 [patent_app_country] => US [patent_app_date] => 2010-05-05 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 9 [patent_figures_cnt] => 9 [patent_no_of_words] => 5930 [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/A1/0056/20120056031.pdf [firstpage_image] =>[orig_patent_app_number] => 13318484 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 8439434 [patent_doc_number] => 20120256050 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2012-10-11 [patent_title] => 'BOGIE STOP BLOCK' [patent_app_type] => utility [patent_app_number] => 13/503265 [patent_app_country] => US [patent_app_date] => 2010-04-30 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 11 [patent_figures_cnt] => 11 [patent_no_of_words] => 4049 [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] =>[firstpage_image] =>[orig_patent_app_number] => 13503265 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 7772731 [patent_doc_number] => 20120037755 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2012-02-16 [patent_title] => 'WING STRUCTURE' [patent_app_type] => utility [patent_app_number] => 13/263215 [patent_app_country] => US [patent_app_date] => 2010-03-31 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 5 [patent_figures_cnt] => 5 [patent_no_of_words] => 3910 [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/A1/0037/20120037755.pdf [firstpage_image] =>[orig_patent_app_number] => 13263215 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 8907971 [patent_doc_number] => 08480025 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2013-07-09 [patent_title] => 'Rear part of an aircraft including an engine support structure assembled so as to oscillate on the fuselage' [patent_app_type] => utility [patent_app_number] => 13/257628 [patent_app_country] => US [patent_app_date] => 2010-03-29 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 8 [patent_figures_cnt] => 12 [patent_no_of_words] => 6879 [patent_no_of_claims] => 10 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 253 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13257628 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 8231437 [patent_doc_number] => 08196858 [patent_country] => US [patent_kind] => B1 [patent_issue_date] => 2012-06-12 [patent_title] => 'Aircraft configured for flight in an atmosphere having low density' [patent_app_type] => utility [patent_app_number] => 12/721833 [patent_app_country] => US [patent_app_date] => 2010-03-11 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 30 [patent_figures_cnt] => 32 [patent_no_of_words] => 15107 [patent_no_of_claims] => 19 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 116 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/08/196/08196858.pdf [firstpage_image] =>[orig_patent_app_number] => 12721833 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 6285464 [patent_doc_number] => 20100237188 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2010-09-23 [patent_title] => 'Movable main undercarriage for an aircraft' [patent_app_type] => utility [patent_app_number] => 12/721083 [patent_app_country] => US [patent_app_date] => 2010-03-10 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 6 [patent_figures_cnt] => 6 [patent_no_of_words] => 4772 [patent_no_of_claims] => 10 [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/A1/0237/20100237188.pdf [firstpage_image] =>[orig_patent_app_number] => 12721083 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 5962630 [patent_doc_number] => 20110147519 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2011-06-23 [patent_title] => 'BRAKE DISC PACK FOR AIRCRAFT' [patent_app_type] => utility [patent_app_number] => 12/720091 [patent_app_country] => US [patent_app_date] => 2010-03-09 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 5 [patent_figures_cnt] => 5 [patent_no_of_words] => 4117 [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/A1/0147/20110147519.pdf [firstpage_image] =>[orig_patent_app_number] => 12720091 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 8036551 [patent_doc_number] => 20120068009 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2012-03-22 [patent_title] => 'SUBMERSIBLE TRANSPORT AND LAUNCH CANISTER' [patent_app_type] => utility [patent_app_number] => 12/716731 [patent_app_country] => US [patent_app_date] => 2010-03-03 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 7 [patent_figures_cnt] => 7 [patent_no_of_words] => 5582 [patent_no_of_claims] => 20 [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/A1/0068/20120068009.pdf [firstpage_image] =>[orig_patent_app_number] => 12716731 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 8256355 [patent_doc_number] => 08205829 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2012-06-26 [patent_title] => 'Submersible transport and launch canister and methods for the use thereof' [patent_app_type] => utility [patent_app_number] => 12/716735 [patent_app_country] => US [patent_app_date] => 2010-03-03 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 6 [patent_figures_cnt] => 6 [patent_no_of_words] => 5747 [patent_no_of_claims] => 19 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 111 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 12716735 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 6626503 [patent_doc_number] => 20100311417 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2010-12-09 [patent_title] => 'METHODS FOR OPTIMIZING THE PERFORMANCE, COST AND CONSTELLATION DESIGN OF SATELLITES FOR FULL AND PARTIAL EARTH COVERAGE' [patent_app_type] => utility [patent_app_number] => 12/708482 [patent_app_country] => US [patent_app_date] => 2010-02-18 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 21 [patent_figures_cnt] => 21 [patent_no_of_words] => 23484 [patent_no_of_claims] => 36 [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/A1/0311/20100311417.pdf [firstpage_image] =>[orig_patent_app_number] => 12708482 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 8338688 [patent_doc_number] => 08240608 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2012-08-14 [patent_title] => 'Device for installing windshield panes' [patent_app_type] => utility [patent_app_number] => 12/707202 [patent_app_country] => US [patent_app_date] => 2010-02-17 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 2 [patent_figures_cnt] => 3 [patent_no_of_words] => 1422 [patent_no_of_claims] => 9 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 61 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 12707202 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 8243855 [patent_doc_number] => 08201776 [patent_country] => US [patent_kind] => B1 [patent_issue_date] => 2012-06-19 [patent_title] => 'Airfoils and method for constructing airfoils' [patent_app_type] => utility [patent_app_number] => 12/707168 [patent_app_country] => US [patent_app_date] => 2010-02-17 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 11 [patent_figures_cnt] => 11 [patent_no_of_words] => 3952 [patent_no_of_claims] => 20 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 153 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/08/201/08201776.pdf [firstpage_image] =>[orig_patent_app_number] => 12707168 [rel_patent_id] =>[rel_patent_doc_number] =>)

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Array ( [id] => 8980511 [patent_doc_number] => 08511620 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2013-08-20 [patent_title] => 'Aircraft wing load alleviation system' [patent_app_type] => utility [patent_app_number] => 13/138162 [patent_app_country] => US [patent_app_date] => 2010-02-16 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 6 [patent_figures_cnt] => 8 [patent_no_of_words] => 2790 [patent_no_of_claims] => 16 [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] => 13138162 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 7762362 [patent_doc_number] => 20120032029 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2012-02-09 [patent_title] => 'SPACE LAUNCH VEHICLE USING MAGNETIC LEVITATION' [patent_app_type] => utility [patent_app_number] => 13/265218 [patent_app_country] => US [patent_app_date] => 2010-02-12 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 5 [patent_figures_cnt] => 5 [patent_no_of_words] => 1362 [patent_no_of_claims] => 2 [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/A1/0032/20120032029.pdf [firstpage_image] =>[orig_patent_app_number] => 13265218 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 8615119 [patent_doc_number] => 20130020431 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2013-01-24 [patent_title] => 'STEERABLE AXLE' [patent_app_type] => utility [patent_app_number] => 13/578096 [patent_app_country] => US [patent_app_date] => 2010-02-10 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 3 [patent_figures_cnt] => 3 [patent_no_of_words] => 3697 [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] =>[firstpage_image] =>[orig_patent_app_number] => 13578096 [rel_patent_id] =>[rel_patent_doc_number] =>)