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Array ( [id] => 4547901 [patent_doc_number] => 07841561 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2010-11-30 [patent_title] => 'Internal support structure for an airship' [patent_app_type] => utility [patent_app_number] => 11/383996 [patent_app_country] => US [patent_app_date] => 2006-05-18 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 1 [patent_figures_cnt] => 1 [patent_no_of_words] => 2673 [patent_no_of_claims] => 17 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 343 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/07/841/07841561.pdf [firstpage_image] =>[orig_patent_app_number] => 11383996 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 5133554 [patent_doc_number] => 20070075183 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2007-04-05 [patent_title] => 'Wing arrangement as well as a missile' [patent_app_type] => utility [patent_app_number] => 11/434712 [patent_app_country] => US [patent_app_date] => 2006-05-16 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 3 [patent_figures_cnt] => 3 [patent_no_of_words] => 2685 [patent_no_of_claims] => 10 [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/A1/0075/20070075183.pdf [firstpage_image] =>[orig_patent_app_number] => 11434712 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 6602784 [patent_doc_number] => 20100171002 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2010-07-08 [patent_title] => 'METHOD FOR REDUCING THE TURBULENCE AND GUST INFLUENCES ON THE FLYING CHARACTERISTICS OF AIRCRAFT, AND A CONTROL DEVICE FOR THIS PURPOSE' [patent_app_type] => utility [patent_app_number] => 11/381192 [patent_app_country] => US [patent_app_date] => 2006-05-02 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 5 [patent_figures_cnt] => 5 [patent_no_of_words] => 2756 [patent_no_of_claims] => 9 [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/A1/0171/20100171002.pdf [firstpage_image] =>[orig_patent_app_number] => 11381192 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 8111989 [patent_doc_number] => 08157208 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2012-04-17 [patent_title] => 'Landing flap drive system' [patent_app_type] => utility [patent_app_number] => 11/911231 [patent_app_country] => US [patent_app_date] => 2006-04-12 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 4 [patent_figures_cnt] => 9 [patent_no_of_words] => 3126 [patent_no_of_claims] => 11 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 277 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/08/157/08157208.pdf [firstpage_image] =>[orig_patent_app_number] => 11911231 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 355158 [patent_doc_number] => 07487937 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2009-02-10 [patent_title] => 'Airfoil for micro air vehicle' [patent_app_type] => utility [patent_app_number] => 11/394018 [patent_app_country] => US [patent_app_date] => 2006-03-30 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 5 [patent_figures_cnt] => 8 [patent_no_of_words] => 5301 [patent_no_of_claims] => 37 [patent_no_of_ind_claims] => 4 [patent_words_short_claim] => 249 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/07/487/07487937.pdf [firstpage_image] =>[orig_patent_app_number] => 11394018 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 5631235 [patent_doc_number] => 20060147704 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2006-07-06 [patent_title] => 'Method to eliminate undulations in a composite panel' [patent_app_type] => utility [patent_app_number] => 11/378791 [patent_app_country] => US [patent_app_date] => 2006-03-16 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 5 [patent_figures_cnt] => 5 [patent_no_of_words] => 2530 [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/A1/0147/20060147704.pdf [firstpage_image] =>[orig_patent_app_number] => 11378791 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 4691077 [patent_doc_number] => 20080083847 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2008-04-10 [patent_title] => 'Air Locomotion Method and Multi-Purpose Aircraft Having Inflatable Wings(S) Using Two Different Inflating Systems' [patent_app_type] => utility [patent_app_number] => 11/813584 [patent_app_country] => US [patent_app_date] => 2006-01-18 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 13 [patent_figures_cnt] => 13 [patent_no_of_words] => 9324 [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/A1/0083/20080083847.pdf [firstpage_image] =>[orig_patent_app_number] => 11813584 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 4506110 [patent_doc_number] => 07909287 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2011-03-22 [patent_title] => 'Super-transporter aircraft' [patent_app_type] => utility [patent_app_number] => 11/792759 [patent_app_country] => US [patent_app_date] => 2005-11-24 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 4 [patent_figures_cnt] => 10 [patent_no_of_words] => 4203 [patent_no_of_claims] => 7 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 278 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/07/909/07909287.pdf [firstpage_image] =>[orig_patent_app_number] => 11792759 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 4843042 [patent_doc_number] => 20080179450 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2008-07-31 [patent_title] => 'Lifting-Type Aeroplane Fuselage' [patent_app_type] => utility [patent_app_number] => 11/791082 [patent_app_country] => US [patent_app_date] => 2005-11-18 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 3 [patent_figures_cnt] => 3 [patent_no_of_words] => 2200 [patent_no_of_claims] => 4 [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/A1/0179/20080179450.pdf [firstpage_image] =>[orig_patent_app_number] => 11791082 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 5327650 [patent_doc_number] => 20090108127 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2009-04-30 [patent_title] => 'METHOD FOR FIXING AN ENGINE STRUT TO AN AIRPLANE WING' [patent_app_type] => utility [patent_app_number] => 11/719891 [patent_app_country] => US [patent_app_date] => 2005-11-17 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 7 [patent_figures_cnt] => 7 [patent_no_of_words] => 3379 [patent_no_of_claims] => 12 [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/A1/0108/20090108127.pdf [firstpage_image] =>[orig_patent_app_number] => 11719891 [rel_patent_id] =>[rel_patent_doc_number] =>)

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Array ( [id] => 30886 [patent_doc_number] => 07784733 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2010-08-31 [patent_title] => 'Turbojet pylon for aircraft' [patent_app_type] => utility [patent_app_number] => 11/632077 [patent_app_country] => US [patent_app_date] => 2005-08-03 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 8 [patent_figures_cnt] => 12 [patent_no_of_words] => 5907 [patent_no_of_claims] => 14 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 228 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/07/784/07784733.pdf [firstpage_image] =>[orig_patent_app_number] => 11632077 [rel_patent_id] =>[rel_patent_doc_number] =>)

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