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Array ( [id] => 6233092 [patent_doc_number] => 20100185346 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2010-07-22 [patent_title] => 'AERIAL PAYLOAD DEPLOYMENT METHOD' [patent_app_type] => utility [patent_app_number] => 12/690840 [patent_app_country] => US [patent_app_date] => 2010-01-20 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 10 [patent_figures_cnt] => 10 [patent_no_of_words] => 10849 [patent_no_of_claims] => 21 [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/A1/0185/20100185346.pdf [firstpage_image] =>[orig_patent_app_number] => 12690840 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 6207915 [patent_doc_number] => 20110133023 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2011-06-09 [patent_title] => 'COLLAPSIBLE AERIAL PAYLOAD DEPLOYMENT SYSTEM AND METHOD' [patent_app_type] => utility [patent_app_number] => 12/690835 [patent_app_country] => US [patent_app_date] => 2010-01-20 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 10 [patent_figures_cnt] => 10 [patent_no_of_words] => 10900 [patent_no_of_claims] => 21 [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/A1/0133/20110133023.pdf [firstpage_image] =>[orig_patent_app_number] => 12690835 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 10025793 [patent_doc_number] => 09067677 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2015-06-30 [patent_title] => 'Dismountable helicopter' [patent_app_type] => utility [patent_app_number] => 13/513722 [patent_app_country] => US [patent_app_date] => 2009-12-02 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 8 [patent_figures_cnt] => 9 [patent_no_of_words] => 3179 [patent_no_of_claims] => 12 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 233 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13513722 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 8621713 [patent_doc_number] => 08354627 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2013-01-15 [patent_title] => 'Torsion stop deployment system for airborne object' [patent_app_type] => utility [patent_app_number] => 12/579970 [patent_app_country] => US [patent_app_date] => 2009-10-15 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 3 [patent_figures_cnt] => 4 [patent_no_of_words] => 3638 [patent_no_of_claims] => 20 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 34 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 12579970 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 6294306 [patent_doc_number] => 20100065689 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2010-03-18 [patent_title] => 'LOAD INTRODUCING ELEMENT' [patent_app_type] => utility [patent_app_number] => 12/560980 [patent_app_country] => US [patent_app_date] => 2009-09-16 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 8 [patent_figures_cnt] => 8 [patent_no_of_words] => 4133 [patent_no_of_claims] => 16 [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/A1/0065/20100065689.pdf [firstpage_image] =>[orig_patent_app_number] => 12560980 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 9587629 [patent_doc_number] => 08777163 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2014-07-15 [patent_title] => 'Ice protection system and method' [patent_app_type] => utility [patent_app_number] => 12/553481 [patent_app_country] => US [patent_app_date] => 2009-09-03 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 4 [patent_figures_cnt] => 7 [patent_no_of_words] => 5178 [patent_no_of_claims] => 20 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 147 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 12553481 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 9573546 [patent_doc_number] => 08763955 [patent_country] => US [patent_kind] => B1 [patent_issue_date] => 2014-07-01 [patent_title] => 'Method and apparatus for controlling a refueling drogue' [patent_app_type] => utility [patent_app_number] => 12/551177 [patent_app_country] => US [patent_app_date] => 2009-08-31 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 4 [patent_figures_cnt] => 4 [patent_no_of_words] => 5732 [patent_no_of_claims] => 9 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 219 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 12551177 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 8100913 [patent_doc_number] => 08152102 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2012-04-10 [patent_title] => 'Module for accommodation of crew members having a stowage bin usable from inside the module' [patent_app_type] => utility [patent_app_number] => 12/547223 [patent_app_country] => US [patent_app_date] => 2009-08-25 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 7 [patent_figures_cnt] => 17 [patent_no_of_words] => 5952 [patent_no_of_claims] => 19 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 82 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/08/152/08152102.pdf [firstpage_image] =>[orig_patent_app_number] => 12547223 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 8192381 [patent_doc_number] => 20120119027 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2012-05-17 [patent_title] => 'FLOOR ELEMENT FOR A LOADING DECK OF AN AIRCRAFT' [patent_app_type] => utility [patent_app_number] => 13/386325 [patent_app_country] => US [patent_app_date] => 2009-07-21 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 2 [patent_figures_cnt] => 2 [patent_no_of_words] => 2114 [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/A1/0119/20120119027.pdf [firstpage_image] =>[orig_patent_app_number] => 13386325 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 5940500 [patent_doc_number] => 20110101157 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2011-05-05 [patent_title] => 'INTEGRAL POWERED WING AIRCRAFT' [patent_app_type] => utility [patent_app_number] => 12/501971 [patent_app_country] => US [patent_app_date] => 2009-07-13 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 12 [patent_figures_cnt] => 12 [patent_no_of_words] => 4088 [patent_no_of_claims] => 22 [patent_no_of_ind_claims] => 13 [patent_words_short_claim] => 0 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] => publications/A1/0101/20110101157.pdf [firstpage_image] =>[orig_patent_app_number] => 12501971 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 6105374 [patent_doc_number] => 20110186679 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2011-08-04 [patent_title] => 'AIRCRAFT WITH AT LEAST TWO PROPELLER DRIVES ARRANGED AT A DISTANCE FROM ONE ANOTHER IN THE SPAN WIDTH DIRECTION OF THE WINGS' [patent_app_type] => utility [patent_app_number] => 13/003501 [patent_app_country] => US [patent_app_date] => 2009-07-13 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 2 [patent_figures_cnt] => 2 [patent_no_of_words] => 3080 [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/A1/0186/20110186679.pdf [firstpage_image] =>[orig_patent_app_number] => 13003501 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 8192383 [patent_doc_number] => 20120119026 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2012-05-17 [patent_title] => 'LOCKING ELEMENT' [patent_app_type] => utility [patent_app_number] => 13/379947 [patent_app_country] => US [patent_app_date] => 2009-06-22 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 8 [patent_figures_cnt] => 8 [patent_no_of_words] => 2870 [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/A1/0119/20120119026.pdf [firstpage_image] =>[orig_patent_app_number] => 13379947 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 4594063 [patent_doc_number] => 07980509 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2011-07-19 [patent_title] => 'Aircraft taxiing systems' [patent_app_type] => utility [patent_app_number] => 12/399854 [patent_app_country] => US [patent_app_date] => 2009-03-06 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 6 [patent_figures_cnt] => 14 [patent_no_of_words] => 3692 [patent_no_of_claims] => 23 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 145 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/07/980/07980509.pdf [firstpage_image] =>[orig_patent_app_number] => 12399854 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 6442078 [patent_doc_number] => 20100282898 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2010-11-11 [patent_title] => 'AIRCRAFT STRUCTURE WITH MODIFIED CONTROL DEVICE HINGE LINE' [patent_app_type] => utility [patent_app_number] => 12/811231 [patent_app_country] => US [patent_app_date] => 2009-01-22 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 4 [patent_figures_cnt] => 4 [patent_no_of_words] => 1901 [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/A1/0282/20100282898.pdf [firstpage_image] =>[orig_patent_app_number] => 12811231 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 6442113 [patent_doc_number] => 20100282902 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2010-11-11 [patent_title] => 'VEHICLE OCCUPANT SUPPORT' [patent_app_type] => utility [patent_app_number] => 12/735146 [patent_app_country] => US [patent_app_date] => 2009-01-21 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 28 [patent_figures_cnt] => 28 [patent_no_of_words] => 38606 [patent_no_of_claims] => 74 [patent_no_of_ind_claims] => 54 [patent_words_short_claim] => 0 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] => publications/A1/0282/20100282902.pdf [firstpage_image] =>[orig_patent_app_number] => 12735146 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 6415554 [patent_doc_number] => 20100276548 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2010-11-04 [patent_title] => 'ACOUSTIC PROCESSING STRUCTURE PARTICULARLY ADAPTED TO THE AIR INLET OF AN AIRCRAFT NACELLE' [patent_app_type] => utility [patent_app_number] => 12/809742 [patent_app_country] => US [patent_app_date] => 2008-12-16 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 5 [patent_figures_cnt] => 5 [patent_no_of_words] => 3817 [patent_no_of_claims] => 8 [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/A1/0276/20100276548.pdf [firstpage_image] =>[orig_patent_app_number] => 12809742 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 6255468 [patent_doc_number] => 20100294880 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2010-11-25 [patent_title] => 'ENGINE-PROPELLER DRIVE SYSTEM' [patent_app_type] => utility [patent_app_number] => 12/812702 [patent_app_country] => US [patent_app_date] => 2008-12-09 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 2 [patent_figures_cnt] => 2 [patent_no_of_words] => 1089 [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/A1/0294/20100294880.pdf [firstpage_image] =>[orig_patent_app_number] => 12812702 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 8795864 [patent_doc_number] => 08434724 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2013-05-07 [patent_title] => 'Air outlet system for aircraft leading edge' [patent_app_type] => utility [patent_app_number] => 12/745950 [patent_app_country] => US [patent_app_date] => 2008-12-01 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 3 [patent_figures_cnt] => 10 [patent_no_of_words] => 2976 [patent_no_of_claims] => 20 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 180 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 12745950 [rel_patent_id] =>[rel_patent_doc_number] =>)

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