Amanda Lee Bailey

Array ( [id] => 5019222 [patent_doc_number] => 20070145187 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2007-06-28 [patent_title] => 'AIRCRAFT PASSENGER ACCOMMODATION UNIT WITH DEPLOYABLE BED' [patent_app_type] => utility [patent_app_number] => 11/684443 [patent_app_country] => US [patent_app_date] => 2007-03-09 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 9 [patent_figures_cnt] => 9 [patent_no_of_words] => 3145 [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/A1/0145/20070145187.pdf [firstpage_image] =>[orig_patent_app_number] => 11684443 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 5334269 [patent_doc_number] => 20090050733 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2009-02-26 [patent_title] => 'SIMPLE VTOL FLYING MACHINE' [patent_app_type] => utility [patent_app_number] => 11/679874 [patent_app_country] => US [patent_app_date] => 2007-02-28 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 9 [patent_figures_cnt] => 9 [patent_no_of_words] => 1364 [patent_no_of_claims] => 12 [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/A1/0050/20090050733.pdf [firstpage_image] =>[orig_patent_app_number] => 11679874 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 5043526 [patent_doc_number] => 20070262197 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2007-11-15 [patent_title] => 'Ultralight coaxial rotor aircraft' [patent_app_type] => utility [patent_app_number] => 11/712838 [patent_app_country] => US [patent_app_date] => 2007-02-28 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 15 [patent_figures_cnt] => 15 [patent_no_of_words] => 9305 [patent_no_of_claims] => 25 [patent_no_of_ind_claims] => 10 [patent_words_short_claim] => 0 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] => publications/A1/0262/20070262197.pdf [firstpage_image] =>[orig_patent_app_number] => 11712838 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 5185850 [patent_doc_number] => 20070164156 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2007-07-19 [patent_title] => 'Continuous power bus for seat power' [patent_app_type] => utility [patent_app_number] => 11/709548 [patent_app_country] => US [patent_app_date] => 2007-02-22 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 5 [patent_figures_cnt] => 5 [patent_no_of_words] => 5413 [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/A1/0164/20070164156.pdf [firstpage_image] =>[orig_patent_app_number] => 11709548 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 5195692 [patent_doc_number] => 20070295010 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2007-12-27 [patent_title] => 'Method and apparatus to generate thrust by inertial mass variance' [patent_app_type] => utility [patent_app_number] => 11/700307 [patent_app_country] => US [patent_app_date] => 2007-01-31 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 10 [patent_figures_cnt] => 10 [patent_no_of_words] => 16533 [patent_no_of_claims] => 48 [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/A1/0295/20070295010.pdf [firstpage_image] =>[orig_patent_app_number] => 11700307 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 109356 [patent_doc_number] => 07717371 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2010-05-18 [patent_title] => 'Resting deck in an aircraft with resting cabins' [patent_app_type] => utility [patent_app_number] => 11/627143 [patent_app_country] => US [patent_app_date] => 2007-01-25 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 4 [patent_figures_cnt] => 4 [patent_no_of_words] => 3694 [patent_no_of_claims] => 6 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 230 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/07/717/07717371.pdf [firstpage_image] =>[orig_patent_app_number] => 11627143 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 6407405 [patent_doc_number] => 20100140390 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2010-06-10 [patent_title] => ' Flying Wind Energy Conversion Apparatus' [patent_app_type] => utility [patent_app_number] => 12/223210 [patent_app_country] => US [patent_app_date] => 2007-01-24 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 19 [patent_figures_cnt] => 19 [patent_no_of_words] => 9812 [patent_no_of_claims] => 21 [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/A1/0140/20100140390.pdf [firstpage_image] =>[orig_patent_app_number] => 12223210 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 4748869 [patent_doc_number] => 20080156939 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2008-07-03 [patent_title] => 'Active pilot flight control stick system with passive electromagnetic feedback' [patent_app_type] => utility [patent_app_number] => 11/649011 [patent_app_country] => US [patent_app_date] => 2007-01-03 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 6 [patent_figures_cnt] => 6 [patent_no_of_words] => 4946 [patent_no_of_claims] => 18 [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/A1/0156/20080156939.pdf [firstpage_image] =>[orig_patent_app_number] => 11649011 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 5511853 [patent_doc_number] => 20090212157 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2009-08-27 [patent_title] => 'MICRO-ROTORCRAFT SURVEILLANCE SYSTEM' [patent_app_type] => utility [patent_app_number] => 11/616201 [patent_app_country] => US [patent_app_date] => 2006-12-26 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 28 [patent_figures_cnt] => 28 [patent_no_of_words] => 11162 [patent_no_of_claims] => 21 [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/A1/0212/20090212157.pdf [firstpage_image] =>[orig_patent_app_number] => 11616201 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 4875515 [patent_doc_number] => 20080148897 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2008-06-26 [patent_title] => 'METHODS AND APPARATUS FOR A CABLE RETRACTOR TO PREVENT CABLE DAMAGE AFTER CONNECTOR RELEASE' [patent_app_type] => utility [patent_app_number] => 11/615419 [patent_app_country] => US [patent_app_date] => 2006-12-22 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 8 [patent_figures_cnt] => 8 [patent_no_of_words] => 2059 [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/A1/0148/20080148897.pdf [firstpage_image] =>[orig_patent_app_number] => 11615419 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 5185852 [patent_doc_number] => 20070164158 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2007-07-19 [patent_title] => 'Aircraft Fuselage With Upper And Lower Deck' [patent_app_type] => utility [patent_app_number] => 11/614314 [patent_app_country] => US [patent_app_date] => 2006-12-21 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 2 [patent_figures_cnt] => 2 [patent_no_of_words] => 1147 [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/A1/0164/20070164158.pdf [firstpage_image] =>[orig_patent_app_number] => 11614314 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 5116629 [patent_doc_number] => 20070138342 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2007-06-21 [patent_title] => 'Cargo loading apparatus' [patent_app_type] => utility [patent_app_number] => 11/640002 [patent_app_country] => US [patent_app_date] => 2006-12-15 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 14 [patent_figures_cnt] => 14 [patent_no_of_words] => 4586 [patent_no_of_claims] => 18 [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/A1/0138/20070138342.pdf [firstpage_image] =>[orig_patent_app_number] => 11640002 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 139606 [patent_doc_number] => 07690600 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2010-04-06 [patent_title] => 'Aerially transportable tank for storing a composition for discharging in flight' [patent_app_type] => utility [patent_app_number] => 11/637917 [patent_app_country] => US [patent_app_date] => 2006-12-13 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 6 [patent_figures_cnt] => 16 [patent_no_of_words] => 3857 [patent_no_of_claims] => 20 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 358 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/07/690/07690600.pdf [firstpage_image] =>[orig_patent_app_number] => 11637917 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 5307301 [patent_doc_number] => 20090014582 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2009-01-15 [patent_title] => 'AIRCRAFT LANDING GEAR COMPRISING AN OPERATION STRUT DEVICE AND AIRCRAFT PROVIDED THEREWITH' [patent_app_type] => utility [patent_app_number] => 12/094385 [patent_app_country] => US [patent_app_date] => 2006-11-14 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 6 [patent_figures_cnt] => 6 [patent_no_of_words] => 2602 [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/A1/0014/20090014582.pdf [firstpage_image] =>[orig_patent_app_number] => 12094385 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 4901612 [patent_doc_number] => 20080111024 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2008-05-15 [patent_title] => 'Composite Aircraft Structures With Hat Stiffeners' [patent_app_type] => utility [patent_app_number] => 11/558735 [patent_app_country] => US [patent_app_date] => 2006-11-10 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 4 [patent_figures_cnt] => 4 [patent_no_of_words] => 5168 [patent_no_of_claims] => 23 [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/A1/0111/20080111024.pdf [firstpage_image] =>[orig_patent_app_number] => 11558735 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 4836451 [patent_doc_number] => 20080277526 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2008-11-13 [patent_title] => 'Aircraft Cooling Duct' [patent_app_type] => utility [patent_app_number] => 12/093157 [patent_app_country] => US [patent_app_date] => 2006-11-07 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 9 [patent_figures_cnt] => 9 [patent_no_of_words] => 5206 [patent_no_of_claims] => 14 [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/A1/0277/20080277526.pdf [firstpage_image] =>[orig_patent_app_number] => 12093157 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 8256366 [patent_doc_number] => 08205839 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2012-06-26 [patent_title] => 'Methods and apparatus for node-synchronous eccentricity control' [patent_app_type] => utility [patent_app_number] => 11/556934 [patent_app_country] => US [patent_app_date] => 2006-11-06 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 9 [patent_figures_cnt] => 12 [patent_no_of_words] => 4632 [patent_no_of_claims] => 22 [patent_no_of_ind_claims] => 4 [patent_words_short_claim] => 91 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 11556934 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 2152 [patent_doc_number] => 07810757 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2010-10-12 [patent_title] => 'Mounting device for an aircraft' [patent_app_type] => utility [patent_app_number] => 11/556125 [patent_app_country] => US [patent_app_date] => 2006-11-02 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 7 [patent_figures_cnt] => 10 [patent_no_of_words] => 3393 [patent_no_of_claims] => 27 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 136 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/07/810/07810757.pdf [firstpage_image] =>[orig_patent_app_number] => 11556125 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 4890503 [patent_doc_number] => 20080099599 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2008-05-01 [patent_title] => 'Fuel Efficient Fixed Wing Aircraft' [patent_app_type] => utility [patent_app_number] => 11/553016 [patent_app_country] => US [patent_app_date] => 2006-10-26 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 6 [patent_figures_cnt] => 6 [patent_no_of_words] => 3669 [patent_no_of_claims] => 15 [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/A1/0099/20080099599.pdf [firstpage_image] =>[orig_patent_app_number] => 11553016 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 8362243 [patent_doc_number] => 08251306 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2012-08-28 [patent_title] => 'Turbofan engine for stol aircraft' [patent_app_type] => utility [patent_app_number] => 12/091289 [patent_app_country] => US [patent_app_date] => 2006-10-25 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 15 [patent_figures_cnt] => 16 [patent_no_of_words] => 15943 [patent_no_of_claims] => 24 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 199 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 12091289 [rel_patent_id] =>[rel_patent_doc_number] =>)