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Array ( [id] => 4782358 [patent_doc_number] => 20080135687 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2008-06-12 [patent_title] => 'UNIVERSAL LAUNCH VEHICLE PAYLOAD ADAPTER' [patent_app_type] => utility [patent_app_number] => 11/608231 [patent_app_country] => US [patent_app_date] => 2006-12-07 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 11 [patent_figures_cnt] => 11 [patent_no_of_words] => 3174 [patent_no_of_claims] => 21 [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/A1/0135/20080135687.pdf [firstpage_image] =>[orig_patent_app_number] => 11608231 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 4782356 [patent_doc_number] => 20080135685 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2008-06-12 [patent_title] => 'POWER OPTIMIZED SYSTEM FOR ELECTRIC PROPULSION STATIONKEEPING GEOSYNCHRONOUS SPACECRAFT' [patent_app_type] => utility [patent_app_number] => 11/608229 [patent_app_country] => US [patent_app_date] => 2006-12-07 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 4 [patent_figures_cnt] => 4 [patent_no_of_words] => 3867 [patent_no_of_claims] => 21 [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/A1/0135/20080135685.pdf [firstpage_image] =>[orig_patent_app_number] => 11608229 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 5123322 [patent_doc_number] => 20070235592 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2007-10-11 [patent_title] => 'Minimum time or thrust separation trajectory for spacecraft emergency separation' [patent_app_type] => utility [patent_app_number] => 11/633910 [patent_app_country] => US [patent_app_date] => 2006-12-05 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 9 [patent_figures_cnt] => 9 [patent_no_of_words] => 4582 [patent_no_of_claims] => 25 [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/A1/0235/20070235592.pdf [firstpage_image] =>[orig_patent_app_number] => 11633910 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 5268314 [patent_doc_number] => 20090072089 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2009-03-19 [patent_title] => 'AIRCRAFT DOOR ASSEMBLY, AND AIRCRAFT FUSELAGE COMPRISING SUCH AN AIRCRAFT DOOR ASSEMBLY' [patent_app_type] => utility [patent_app_number] => 12/158317 [patent_app_country] => US [patent_app_date] => 2006-12-02 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 6 [patent_figures_cnt] => 6 [patent_no_of_words] => 6109 [patent_no_of_claims] => 25 [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/A1/0072/20090072089.pdf [firstpage_image] =>[orig_patent_app_number] => 12158317 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 8651791 [patent_doc_number] => 08371533 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2013-02-12 [patent_title] => 'Aircraft auxiliary fuel tank system and method' [patent_app_type] => utility [patent_app_number] => 12/158061 [patent_app_country] => US [patent_app_date] => 2006-12-01 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 4 [patent_figures_cnt] => 4 [patent_no_of_words] => 5097 [patent_no_of_claims] => 11 [patent_no_of_ind_claims] => 5 [patent_words_short_claim] => 36 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 12158061 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 5002467 [patent_doc_number] => 20070200032 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2007-08-30 [patent_title] => 'RADIO FREQUENCY EMITTING HOOK SYSTEM FOR A ROTARY-WING AIRCRAFT EXTERNAL LOAD HANDLING' [patent_app_type] => utility [patent_app_number] => 11/565697 [patent_app_country] => US [patent_app_date] => 2006-12-01 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 6 [patent_figures_cnt] => 6 [patent_no_of_words] => 2964 [patent_no_of_claims] => 24 [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/A1/0200/20070200032.pdf [firstpage_image] =>[orig_patent_app_number] => 11565697 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 4828839 [patent_doc_number] => 20080128554 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2008-06-05 [patent_title] => 'COMPOSITE SHEAR TIE' [patent_app_type] => utility [patent_app_number] => 11/564964 [patent_app_country] => US [patent_app_date] => 2006-11-30 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 12 [patent_figures_cnt] => 12 [patent_no_of_words] => 4933 [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/A1/0128/20080128554.pdf [firstpage_image] =>[orig_patent_app_number] => 11564964 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 4775667 [patent_doc_number] => 20080283665 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2008-11-20 [patent_title] => 'Aircraft Ventral Fairing Partition Wall and Aircraft Equipped with a Ventral Fairing' [patent_app_type] => utility [patent_app_number] => 12/096459 [patent_app_country] => US [patent_app_date] => 2006-11-23 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 6 [patent_figures_cnt] => 6 [patent_no_of_words] => 4955 [patent_no_of_claims] => 10 [patent_no_of_ind_claims] => 7 [patent_words_short_claim] => 0 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] => publications/A1/0283/20080283665.pdf [firstpage_image] =>[orig_patent_app_number] => 12096459 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 4896708 [patent_doc_number] => 20080116321 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2008-05-22 [patent_title] => 'Lift spoiler for parked aircraft' [patent_app_type] => utility [patent_app_number] => 11/602592 [patent_app_country] => US [patent_app_date] => 2006-11-22 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 5 [patent_figures_cnt] => 5 [patent_no_of_words] => 2580 [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/A1/0116/20080116321.pdf [firstpage_image] =>[orig_patent_app_number] => 11602592 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 4707911 [patent_doc_number] => 20080296437 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2008-12-04 [patent_title] => 'Method and Device to Generate a Transverse Casimir Force for Propulsion, Guidance and Maneuvering of a Space Vehicle' [patent_app_type] => utility [patent_app_number] => 11/561839 [patent_app_country] => US [patent_app_date] => 2006-11-20 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 5 [patent_figures_cnt] => 5 [patent_no_of_words] => 3868 [patent_no_of_claims] => 19 [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/A1/0296/20080296437.pdf [firstpage_image] =>[orig_patent_app_number] => 11561839 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 4962963 [patent_doc_number] => 20080105783 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2008-05-08 [patent_title] => 'Fuselage design for sonic boom suppression of supersonic aircraft' [patent_app_type] => utility [patent_app_number] => 11/592546 [patent_app_country] => US [patent_app_date] => 2006-11-03 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 11 [patent_figures_cnt] => 11 [patent_no_of_words] => 3055 [patent_no_of_claims] => 10 [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/A1/0105/20080105783.pdf [firstpage_image] =>[orig_patent_app_number] => 11592546 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 4673189 [patent_doc_number] => 20080210817 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2008-09-04 [patent_title] => 'Energy-absorbing Square Tube Composite Stanchion' [patent_app_type] => utility [patent_app_number] => 11/553391 [patent_app_country] => US [patent_app_date] => 2006-10-26 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 5 [patent_figures_cnt] => 5 [patent_no_of_words] => 1380 [patent_no_of_claims] => 15 [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/A1/0210/20080210817.pdf [firstpage_image] =>[orig_patent_app_number] => 11553391 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 4890536 [patent_doc_number] => 20080099632 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2008-05-01 [patent_title] => 'Aircraft airframe architectures' [patent_app_type] => utility [patent_app_number] => 11/586175 [patent_app_country] => US [patent_app_date] => 2006-10-25 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 5 [patent_figures_cnt] => 5 [patent_no_of_words] => 1957 [patent_no_of_claims] => 11 [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/A1/0099/20080099632.pdf [firstpage_image] =>[orig_patent_app_number] => 11586175 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 5092722 [patent_doc_number] => 20070114331 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2007-05-24 [patent_title] => 'Helicopter collapsible deck' [patent_app_type] => utility [patent_app_number] => 11/584463 [patent_app_country] => US [patent_app_date] => 2006-10-20 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 6 [patent_figures_cnt] => 6 [patent_no_of_words] => 2935 [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/A1/0114/20070114331.pdf [firstpage_image] =>[orig_patent_app_number] => 11584463 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 4638220 [patent_doc_number] => 08016245 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2011-09-13 [patent_title] => 'Dynamic bumps for drag reduction at transonic-supersonic speeds' [patent_app_type] => utility [patent_app_number] => 11/583140 [patent_app_country] => US [patent_app_date] => 2006-10-18 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 10 [patent_figures_cnt] => 15 [patent_no_of_words] => 5114 [patent_no_of_claims] => 10 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 323 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/08/016/08016245.pdf [firstpage_image] =>[orig_patent_app_number] => 11583140 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 5116632 [patent_doc_number] => 20070138345 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2007-06-21 [patent_title] => 'Method and System For Aviation Navigation' [patent_app_type] => utility [patent_app_number] => 11/550391 [patent_app_country] => US [patent_app_date] => 2006-10-17 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 3 [patent_figures_cnt] => 3 [patent_no_of_words] => 4824 [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/A1/0138/20070138345.pdf [firstpage_image] =>[orig_patent_app_number] => 11550391 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 4531813 [patent_doc_number] => 07874513 [patent_country] => US [patent_kind] => B1 [patent_issue_date] => 2011-01-25 [patent_title] => 'Apparatus and method for vertical take-off and landing aircraft' [patent_app_type] => utility [patent_app_number] => 11/581321 [patent_app_country] => US [patent_app_date] => 2006-10-16 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 9 [patent_figures_cnt] => 11 [patent_no_of_words] => 8604 [patent_no_of_claims] => 15 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 188 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/07/874/07874513.pdf [firstpage_image] =>[orig_patent_app_number] => 11581321 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 4954761 [patent_doc_number] => 20080187785 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2008-08-07 [patent_title] => 'Fuel system for an aircraft including a fuel tank inerting system' [patent_app_type] => utility [patent_app_number] => 11/527009 [patent_app_country] => US [patent_app_date] => 2006-09-26 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 7 [patent_figures_cnt] => 7 [patent_no_of_words] => 3006 [patent_no_of_claims] => 22 [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/A1/0187/20080187785.pdf [firstpage_image] =>[orig_patent_app_number] => 11527009 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 6310304 [patent_doc_number] => 20100193627 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2010-08-05 [patent_title] => 'ASSEMBLY FOR AN AIRCRAFT INCLUDING A WING ELEMENT AND A SUSPENSION PYLON' [patent_app_type] => utility [patent_app_number] => 11/525018 [patent_app_country] => US [patent_app_date] => 2006-09-22 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 4 [patent_figures_cnt] => 4 [patent_no_of_words] => 2987 [patent_no_of_claims] => 8 [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/A1/0193/20100193627.pdf [firstpage_image] =>[orig_patent_app_number] => 11525018 [rel_patent_id] =>[rel_patent_doc_number] =>)