Amanda Lee Bailey

Array ( [id] => 393077 [patent_doc_number] => 07296767 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2007-11-20 [patent_title] => 'Variable speed transmission for a rotary wing aircraft' [patent_app_type] => utility [patent_app_number] => 11/141631 [patent_app_country] => US [patent_app_date] => 2005-05-31 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 5 [patent_figures_cnt] => 6 [patent_no_of_words] => 3310 [patent_no_of_claims] => 21 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 115 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/07/296/07296767.pdf [firstpage_image] =>[orig_patent_app_number] => 11141631 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 5060143 [patent_doc_number] => 20070221779 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2007-09-27 [patent_title] => 'Aircraft Produced by Fixing Rapid Airflow Generation Wind Direction Changing Device Directly and Firmly to Side Surface or Wall Thereof' [patent_app_type] => utility [patent_app_number] => 11/631416 [patent_app_country] => US [patent_app_date] => 2005-05-27 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 16 [patent_figures_cnt] => 16 [patent_no_of_words] => 8322 [patent_no_of_claims] => 2 [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/A1/0221/20070221779.pdf [firstpage_image] =>[orig_patent_app_number] => 11631416 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 100131 [patent_doc_number] => 07721988 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2010-05-25 [patent_title] => 'Unmanned helicopter' [patent_app_type] => utility [patent_app_number] => 10/572023 [patent_app_country] => US [patent_app_date] => 2005-05-27 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 3 [patent_figures_cnt] => 4 [patent_no_of_words] => 979 [patent_no_of_claims] => 5 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 75 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/07/721/07721988.pdf [firstpage_image] =>[orig_patent_app_number] => 10572023 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 5723980 [patent_doc_number] => 20060054740 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2006-03-16 [patent_title] => 'Aircraft having integrated electrochemical supply system' [patent_app_type] => utility [patent_app_number] => 11/137231 [patent_app_country] => US [patent_app_date] => 2005-05-25 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 3 [patent_figures_cnt] => 3 [patent_no_of_words] => 3836 [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/A1/0054/20060054740.pdf [firstpage_image] =>[orig_patent_app_number] => 11137231 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 900558 [patent_doc_number] => 07334755 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2008-02-26 [patent_title] => 'Tandem rotor wing and tandem fixed wing aircraft' [patent_app_type] => utility [patent_app_number] => 11/136825 [patent_app_country] => US [patent_app_date] => 2005-05-25 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 7 [patent_figures_cnt] => 7 [patent_no_of_words] => 4498 [patent_no_of_claims] => 8 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 241 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/07/334/07334755.pdf [firstpage_image] =>[orig_patent_app_number] => 11136825 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 200416 [patent_doc_number] => 07631836 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2009-12-15 [patent_title] => 'Jet engine nacelle for a supersonic aircraft' [patent_app_type] => utility [patent_app_number] => 11/133326 [patent_app_country] => US [patent_app_date] => 2005-05-20 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 3 [patent_figures_cnt] => 6 [patent_no_of_words] => 2181 [patent_no_of_claims] => 9 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 264 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/07/631/07631836.pdf [firstpage_image] =>[orig_patent_app_number] => 11133326 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 389427 [patent_doc_number] => 07300021 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2007-11-27 [patent_title] => 'Aerospace vehicle fairing systems and associated methods' [patent_app_type] => utility [patent_app_number] => 11/134019 [patent_app_country] => US [patent_app_date] => 2005-05-20 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 5 [patent_figures_cnt] => 7 [patent_no_of_words] => 4859 [patent_no_of_claims] => 8 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 168 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/07/300/07300021.pdf [firstpage_image] =>[orig_patent_app_number] => 11134019 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 7016184 [patent_doc_number] => 20050218266 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2005-10-06 [patent_title] => 'Avionic door lock system' [patent_app_type] => utility [patent_app_number] => 11/128809 [patent_app_country] => US [patent_app_date] => 2005-05-13 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 5 [patent_figures_cnt] => 5 [patent_no_of_words] => 4286 [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/A1/0218/20050218266.pdf [firstpage_image] =>[orig_patent_app_number] => 11128809 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 216187 [patent_doc_number] => 07611092 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2009-11-03 [patent_title] => 'Internet linked environmental data collection system and method' [patent_app_type] => utility [patent_app_number] => 11/125148 [patent_app_country] => US [patent_app_date] => 2005-05-10 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 23 [patent_figures_cnt] => 32 [patent_no_of_words] => 11542 [patent_no_of_claims] => 79 [patent_no_of_ind_claims] => 8 [patent_words_short_claim] => 215 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/07/611/07611092.pdf [firstpage_image] =>[orig_patent_app_number] => 11125148 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 4839200 [patent_doc_number] => 20080279685 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2008-11-13 [patent_title] => 'Helicopter Rotor Control System with Individual Blade Control' [patent_app_type] => utility [patent_app_number] => 11/579281 [patent_app_country] => US [patent_app_date] => 2005-05-06 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 9 [patent_figures_cnt] => 9 [patent_no_of_words] => 9748 [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/A1/0279/20080279685.pdf [firstpage_image] =>[orig_patent_app_number] => 11579281 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 5659026 [patent_doc_number] => 20060249622 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2006-11-09 [patent_title] => 'Autonomous Environmental Control System and Method For Post-Capture and Pre-Launch Management of an Unmanned Air Vehicle' [patent_app_type] => utility [patent_app_number] => 10/908255 [patent_app_country] => US [patent_app_date] => 2005-05-04 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 5 [patent_figures_cnt] => 5 [patent_no_of_words] => 3323 [patent_no_of_claims] => 41 [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/A1/0249/20060249622.pdf [firstpage_image] =>[orig_patent_app_number] => 10908255 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 848238 [patent_doc_number] => 07380752 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2008-06-03 [patent_title] => 'Aircraft interior architecture' [patent_app_type] => utility [patent_app_number] => 10/908140 [patent_app_country] => US [patent_app_date] => 2005-04-28 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 6 [patent_figures_cnt] => 14 [patent_no_of_words] => 3475 [patent_no_of_claims] => 10 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 164 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/07/380/07380752.pdf [firstpage_image] =>[orig_patent_app_number] => 10908140 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 5796307 [patent_doc_number] => 20060032984 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2006-02-16 [patent_title] => 'Steerable parachute control system and method' [patent_app_type] => utility [patent_app_number] => 11/114616 [patent_app_country] => US [patent_app_date] => 2005-04-26 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 5 [patent_figures_cnt] => 5 [patent_no_of_words] => 6220 [patent_no_of_claims] => 28 [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/A1/0032/20060032984.pdf [firstpage_image] =>[orig_patent_app_number] => 11114616 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 219685 [patent_doc_number] => 07607614 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2009-10-27 [patent_title] => 'Transition shim between structure for fastening a wing to a fuselage of an aircraft, and aircraft having such a shim' [patent_app_type] => utility [patent_app_number] => 11/114659 [patent_app_country] => US [patent_app_date] => 2005-04-26 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 2 [patent_figures_cnt] => 4 [patent_no_of_words] => 2969 [patent_no_of_claims] => 9 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 219 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/07/607/07607614.pdf [firstpage_image] =>[orig_patent_app_number] => 11114659 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 564875 [patent_doc_number] => 07455263 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2008-11-25 [patent_title] => 'Airplane interior systems' [patent_app_type] => utility [patent_app_number] => 10/907990 [patent_app_country] => US [patent_app_date] => 2005-04-22 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 11 [patent_figures_cnt] => 23 [patent_no_of_words] => 4503 [patent_no_of_claims] => 11 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 219 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/07/455/07455263.pdf [firstpage_image] =>[orig_patent_app_number] => 10907990 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 6963626 [patent_doc_number] => 20050230523 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2005-10-20 [patent_title] => 'Flapping apparatus' [patent_app_type] => utility [patent_app_number] => 11/107064 [patent_app_country] => US [patent_app_date] => 2005-04-15 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 19 [patent_figures_cnt] => 19 [patent_no_of_words] => 11096 [patent_no_of_claims] => 19 [patent_no_of_ind_claims] => 11 [patent_words_short_claim] => 0 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] => publications/A1/0230/20050230523.pdf [firstpage_image] =>[orig_patent_app_number] => 11107064 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 5854359 [patent_doc_number] => 20060226292 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2006-10-12 [patent_title] => 'Dual-channel deicing system for a rotary wing aircraft' [patent_app_type] => utility [patent_app_number] => 11/101269 [patent_app_country] => US [patent_app_date] => 2005-04-06 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 8 [patent_figures_cnt] => 8 [patent_no_of_words] => 4008 [patent_no_of_claims] => 27 [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/A1/0226/20060226292.pdf [firstpage_image] =>[orig_patent_app_number] => 11101269 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 208510 [patent_doc_number] => 07624946 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2009-12-01 [patent_title] => 'Reservoir for cryogenic fuels and vehicles' [patent_app_type] => utility [patent_app_number] => 11/092307 [patent_app_country] => US [patent_app_date] => 2005-03-29 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 2 [patent_figures_cnt] => 4 [patent_no_of_words] => 2008 [patent_no_of_claims] => 15 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 154 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/07/624/07624946.pdf [firstpage_image] =>[orig_patent_app_number] => 11092307 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 427639 [patent_doc_number] => 07267302 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2007-09-11 [patent_title] => 'Window airflow damper' [patent_app_type] => utility [patent_app_number] => 11/092040 [patent_app_country] => US [patent_app_date] => 2005-03-29 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 3 [patent_figures_cnt] => 5 [patent_no_of_words] => 1245 [patent_no_of_claims] => 10 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 80 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/07/267/07267302.pdf [firstpage_image] =>[orig_patent_app_number] => 11092040 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 472574 [patent_doc_number] => 07226016 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2007-06-05 [patent_title] => 'Method and arrangement for low or non-rotating artillery shells' [patent_app_type] => utility [patent_app_number] => 10/907301 [patent_app_country] => US [patent_app_date] => 2005-03-28 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 7 [patent_figures_cnt] => 10 [patent_no_of_words] => 3843 [patent_no_of_claims] => 11 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 174 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/07/226/07226016.pdf [firstpage_image] =>[orig_patent_app_number] => 10907301 [rel_patent_id] =>[rel_patent_doc_number] =>)