Amanda Lee Bailey

Array ( [id] => 3757285 [patent_doc_number] => 05806798 [patent_country] => US [patent_kind] => NA [patent_issue_date] => 1998-09-15 [patent_title] => 'Bending beam type structural component especially aircraft component' [patent_app_type] => 1 [patent_app_number] => 8/614796 [patent_app_country] => US [patent_app_date] => 1996-03-07 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 1 [patent_figures_cnt] => 3 [patent_no_of_words] => 1784 [patent_no_of_claims] => 10 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 64 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/05/806/05806798.pdf [firstpage_image] =>[orig_patent_app_number] => 614796 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 4167614 [patent_doc_number] => 06019319 [patent_country] => US [patent_kind] => NA [patent_issue_date] => 2000-02-01 [patent_title] => 'Momentum wheel energy storage system using magnetic bearings' [patent_app_type] => 1 [patent_app_number] => 8/598346 [patent_app_country] => US [patent_app_date] => 1996-02-08 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 3 [patent_figures_cnt] => 4 [patent_no_of_words] => 1458 [patent_no_of_claims] => 11 [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] => patents/06/019/06019319.pdf [firstpage_image] =>[orig_patent_app_number] => 598346 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 3945901 [patent_doc_number] => 05899411 [patent_country] => US [patent_kind] => NA [patent_issue_date] => 1999-05-04 [patent_title] => 'Aircraft electrical system providing emergency power and electric starting of propulsion engines' [patent_app_type] => 1 [patent_app_number] => 8/589235 [patent_app_country] => US [patent_app_date] => 1996-01-22 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 5 [patent_figures_cnt] => 5 [patent_no_of_words] => 8838 [patent_no_of_claims] => 12 [patent_no_of_ind_claims] => 5 [patent_words_short_claim] => 118 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/05/899/05899411.pdf [firstpage_image] =>[orig_patent_app_number] => 589235 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 3864185 [patent_doc_number] => 05727757 [patent_country] => US [patent_kind] => NA [patent_issue_date] => 1998-03-17 [patent_title] => 'Slotted cam control system' [patent_app_type] => 1 [patent_app_number] => 8/587666 [patent_app_country] => US [patent_app_date] => 1996-01-17 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 3 [patent_figures_cnt] => 6 [patent_no_of_words] => 2692 [patent_no_of_claims] => 29 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 207 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/05/727/05727757.pdf [firstpage_image] =>[orig_patent_app_number] => 587666 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 3732497 [patent_doc_number] => 05716031 [patent_country] => US [patent_kind] => NA [patent_issue_date] => 1998-02-10 [patent_title] => 'Artificial satellite equipped with aerodynamic orientation rudders' [patent_app_type] => 1 [patent_app_number] => 8/535214 [patent_app_country] => US [patent_app_date] => 1996-01-16 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 7 [patent_figures_cnt] => 12 [patent_no_of_words] => 3457 [patent_no_of_claims] => 12 [patent_no_of_ind_claims] => 4 [patent_words_short_claim] => 29 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/05/716/05716031.pdf [firstpage_image] =>[orig_patent_app_number] => 535214 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 3683783 [patent_doc_number] => 05618011 [patent_country] => US [patent_kind] => NA [patent_issue_date] => 1997-04-08 [patent_title] => 'Load securing and releasing system' [patent_app_type] => 1 [patent_app_number] => 8/585066 [patent_app_country] => US [patent_app_date] => 1996-01-11 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 3 [patent_figures_cnt] => 5 [patent_no_of_words] => 2354 [patent_no_of_claims] => 12 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 131 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/05/618/05618011.pdf [firstpage_image] =>[orig_patent_app_number] => 585066 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 3821904 [patent_doc_number] => 05711495 [patent_country] => US [patent_kind] => NA [patent_issue_date] => 1998-01-27 [patent_title] => 'Deployment control for inflatable escape slide' [patent_app_type] => 1 [patent_app_number] => 8/581954 [patent_app_country] => US [patent_app_date] => 1996-01-02 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 6 [patent_figures_cnt] => 9 [patent_no_of_words] => 4001 [patent_no_of_claims] => 19 [patent_no_of_ind_claims] => 5 [patent_words_short_claim] => 133 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/05/711/05711495.pdf [firstpage_image] =>[orig_patent_app_number] => 581954 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 3712078 [patent_doc_number] => 05681013 [patent_country] => US [patent_kind] => NA [patent_issue_date] => 1997-10-28 [patent_title] => 'Vortex leading edge flap assembly for supersonic airplanes' [patent_app_type] => 1 [patent_app_number] => 8/577966 [patent_app_country] => US [patent_app_date] => 1995-12-26 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 9 [patent_figures_cnt] => 10 [patent_no_of_words] => 8265 [patent_no_of_claims] => 15 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 209 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/05/681/05681013.pdf [firstpage_image] =>[orig_patent_app_number] => 577966 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 3971390 [patent_doc_number] => 05984236 [patent_country] => US [patent_kind] => NA [patent_issue_date] => 1999-11-16 [patent_title] => 'Momentum unloading using gimbaled thrusters' [patent_app_type] => 1 [patent_app_number] => 8/577444 [patent_app_country] => US [patent_app_date] => 1995-12-22 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 6 [patent_figures_cnt] => 10 [patent_no_of_words] => 5603 [patent_no_of_claims] => 21 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 150 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/05/984/05984236.pdf [firstpage_image] =>[orig_patent_app_number] => 577444 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 3783481 [patent_doc_number] => 05826830 [patent_country] => US [patent_kind] => NA [patent_issue_date] => 1998-10-27 [patent_title] => 'Dual-half system, full torque reaction control thruster configuration for three-axis stabilized spacecraft' [patent_app_type] => 1 [patent_app_number] => 8/577594 [patent_app_country] => US [patent_app_date] => 1995-12-22 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 3 [patent_figures_cnt] => 4 [patent_no_of_words] => 2551 [patent_no_of_claims] => 19 [patent_no_of_ind_claims] => 4 [patent_words_short_claim] => 185 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/05/826/05826830.pdf [firstpage_image] =>[orig_patent_app_number] => 577594 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 3857032 [patent_doc_number] => 05823477 [patent_country] => US [patent_kind] => NA [patent_issue_date] => 1998-10-20 [patent_title] => 'Device and method for minimizing radiator area required for heat dissipation on a spacecraft' [patent_app_type] => 1 [patent_app_number] => 8/577574 [patent_app_country] => US [patent_app_date] => 1995-12-22 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 2 [patent_figures_cnt] => 3 [patent_no_of_words] => 2161 [patent_no_of_claims] => 28 [patent_no_of_ind_claims] => 5 [patent_words_short_claim] => 13 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/05/823/05823477.pdf [firstpage_image] =>[orig_patent_app_number] => 577574 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 3771892 [patent_doc_number] => 05735489 [patent_country] => US [patent_kind] => NA [patent_issue_date] => 1998-04-07 [patent_title] => 'Heat transport system for spacecraft integration' [patent_app_type] => 1 [patent_app_number] => 8/577434 [patent_app_country] => US [patent_app_date] => 1995-12-22 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 2 [patent_figures_cnt] => 4 [patent_no_of_words] => 1811 [patent_no_of_claims] => 21 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 63 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/05/735/05735489.pdf [firstpage_image] =>[orig_patent_app_number] => 577434 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 3759148 [patent_doc_number] => 05816540 [patent_country] => US [patent_kind] => NA [patent_issue_date] => 1998-10-06 [patent_title] => 'Optimal solar tracking system' [patent_app_type] => 1 [patent_app_number] => 8/577436 [patent_app_country] => US [patent_app_date] => 1995-12-22 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 5 [patent_figures_cnt] => 11 [patent_no_of_words] => 4527 [patent_no_of_claims] => 20 [patent_no_of_ind_claims] => 4 [patent_words_short_claim] => 65 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/05/816/05816540.pdf [firstpage_image] =>[orig_patent_app_number] => 577436 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 3830935 [patent_doc_number] => 05765780 [patent_country] => US [patent_kind] => NA [patent_issue_date] => 1998-06-16 [patent_title] => 'Systematic vectored thrust calibration method for satellite momentum control' [patent_app_type] => 1 [patent_app_number] => 8/577595 [patent_app_country] => US [patent_app_date] => 1995-12-22 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 8 [patent_figures_cnt] => 19 [patent_no_of_words] => 5007 [patent_no_of_claims] => 14 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 82 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/05/765/05765780.pdf [firstpage_image] =>[orig_patent_app_number] => 577595 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 3757313 [patent_doc_number] => 05806800 [patent_country] => US [patent_kind] => NA [patent_issue_date] => 1998-09-15 [patent_title] => 'Dual function deployable radiator cover' [patent_app_type] => 1 [patent_app_number] => 8/577596 [patent_app_country] => US [patent_app_date] => 1995-12-22 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 3 [patent_figures_cnt] => 3 [patent_no_of_words] => 2366 [patent_no_of_claims] => 15 [patent_no_of_ind_claims] => 6 [patent_words_short_claim] => 20 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/05/806/05806800.pdf [firstpage_image] =>[orig_patent_app_number] => 577596 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 3726340 [patent_doc_number] => 05785276 [patent_country] => US [patent_kind] => NA [patent_issue_date] => 1998-07-28 [patent_title] => 'Actuated roll axis aerial refueling boom' [patent_app_type] => 1 [patent_app_number] => 8/577034 [patent_app_country] => US [patent_app_date] => 1995-12-22 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 8 [patent_figures_cnt] => 10 [patent_no_of_words] => 5604 [patent_no_of_claims] => 20 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 208 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/05/785/05785276.pdf [firstpage_image] =>[orig_patent_app_number] => 577034 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 3847172 [patent_doc_number] => 05794890 [patent_country] => US [patent_kind] => NA [patent_issue_date] => 1998-08-18 [patent_title] => 'Shielded radiator' [patent_app_type] => 1 [patent_app_number] => 8/577445 [patent_app_country] => US [patent_app_date] => 1995-12-22 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 3 [patent_figures_cnt] => 5 [patent_no_of_words] => 3282 [patent_no_of_claims] => 13 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 207 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/05/794/05794890.pdf [firstpage_image] =>[orig_patent_app_number] => 577445 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 3797231 [patent_doc_number] => 05788182 [patent_country] => US [patent_kind] => NA [patent_issue_date] => 1998-08-04 [patent_title] => 'Bidirectional antivibration suspension device for helicopter rotor' [patent_app_type] => 1 [patent_app_number] => 8/575365 [patent_app_country] => US [patent_app_date] => 1995-12-20 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 3 [patent_figures_cnt] => 6 [patent_no_of_words] => 6719 [patent_no_of_claims] => 14 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 71 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/05/788/05788182.pdf [firstpage_image] =>[orig_patent_app_number] => 575365 [rel_patent_id] =>[rel_patent_doc_number] =>)