Amanda Lee Bailey

Array ( [id] => 6807153 [patent_doc_number] => 20030197092 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2003-10-23 [patent_title] => 'Speed regulated model airplane with double motor' [patent_app_type] => new [patent_app_number] => 10/390035 [patent_app_country] => US [patent_app_date] => 2003-03-18 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 3 [patent_figures_cnt] => 3 [patent_no_of_words] => 1769 [patent_no_of_claims] => 6 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 159 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] => publications/A1/0197/20030197092.pdf [firstpage_image] =>[orig_patent_app_number] => 10390035 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 6727531 [patent_doc_number] => 20030183721 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2003-10-02 [patent_title] => 'Freebird' [patent_app_type] => new [patent_app_number] => 10/390109 [patent_app_country] => US [patent_app_date] => 2003-03-17 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 2 [patent_figures_cnt] => 2 [patent_no_of_words] => 887 [patent_no_of_claims] => 20 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 44 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] => publications/A1/0183/20030183721.pdf [firstpage_image] =>[orig_patent_app_number] => 10390109 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 636231 [patent_doc_number] => 07124981 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2006-10-24 [patent_title] => 'Thrust reverser utilizing integrated structural bypass duct' [patent_app_type] => utility [patent_app_number] => 10/379029 [patent_app_country] => US [patent_app_date] => 2003-03-04 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 5 [patent_figures_cnt] => 6 [patent_no_of_words] => 2905 [patent_no_of_claims] => 12 [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/07/124/07124981.pdf [firstpage_image] =>[orig_patent_app_number] => 10379029 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 667557 [patent_doc_number] => 07093792 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2006-08-22 [patent_title] => 'Laminar-flow airfoil' [patent_app_type] => utility [patent_app_number] => 10/373694 [patent_app_country] => US [patent_app_date] => 2003-02-27 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 7 [patent_figures_cnt] => 7 [patent_no_of_words] => 4307 [patent_no_of_claims] => 22 [patent_no_of_ind_claims] => 4 [patent_words_short_claim] => 239 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/07/093/07093792.pdf [firstpage_image] =>[orig_patent_app_number] => 10373694 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 6854059 [patent_doc_number] => 20030127560 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2003-07-10 [patent_title] => 'Flat balloon' [patent_app_type] => new [patent_app_number] => 10/364711 [patent_app_country] => US [patent_app_date] => 2003-02-11 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 2 [patent_figures_cnt] => 2 [patent_no_of_words] => 2119 [patent_no_of_claims] => 12 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 59 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] => publications/A1/0127/20030127560.pdf [firstpage_image] =>[orig_patent_app_number] => 10364711 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 6626040 [patent_doc_number] => 20030102406 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2003-06-05 [patent_title] => 'Aircraft noise reduction apparatus' [patent_app_type] => new [patent_app_number] => 10/300916 [patent_app_country] => US [patent_app_date] => 2003-02-06 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 8 [patent_figures_cnt] => 8 [patent_no_of_words] => 4421 [patent_no_of_claims] => 21 [patent_no_of_ind_claims] => 7 [patent_words_short_claim] => 11 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] => publications/A1/0102/20030102406.pdf [firstpage_image] =>[orig_patent_app_number] => 10300916 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 1228014 [patent_doc_number] => 06691953 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2004-02-17 [patent_title] => 'Ejectable door for aircraft' [patent_app_type] => B2 [patent_app_number] => 10/355803 [patent_app_country] => US [patent_app_date] => 2003-01-30 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 3 [patent_figures_cnt] => 5 [patent_no_of_words] => 2670 [patent_no_of_claims] => 9 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 147 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/06/691/06691953.pdf [firstpage_image] =>[orig_patent_app_number] => 10355803 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 109355 [patent_doc_number] => 07717370 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2010-05-18 [patent_title] => 'L-tail (featuring parabrakes)' [patent_app_type] => utility [patent_app_number] => 10/349791 [patent_app_country] => US [patent_app_date] => 2003-01-23 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 29 [patent_figures_cnt] => 41 [patent_no_of_words] => 3803 [patent_no_of_claims] => 7 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 171 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/07/717/07717370.pdf [firstpage_image] =>[orig_patent_app_number] => 10349791 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 7304738 [patent_doc_number] => 20040140397 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2004-07-22 [patent_title] => 'Scarf nozzle for a jet engine and method of using the same' [patent_app_type] => new [patent_app_number] => 10/351159 [patent_app_country] => US [patent_app_date] => 2003-01-22 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 6 [patent_figures_cnt] => 6 [patent_no_of_words] => 3693 [patent_no_of_claims] => 37 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 56 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] => publications/A1/0140/20040140397.pdf [firstpage_image] =>[orig_patent_app_number] => 10351159 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 6655521 [patent_doc_number] => 20030132350 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2003-07-17 [patent_title] => 'Orbit transfer vehicle with support services' [patent_app_type] => new [patent_app_number] => 10/348365 [patent_app_country] => US [patent_app_date] => 2003-01-21 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 5 [patent_figures_cnt] => 5 [patent_no_of_words] => 4059 [patent_no_of_claims] => 15 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 76 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] => publications/A1/0132/20030132350.pdf [firstpage_image] =>[orig_patent_app_number] => 10348365 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 987072 [patent_doc_number] => 06921050 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2005-07-26 [patent_title] => 'Solar torque control using thin film directionally reflective, emissive, absorptive and transmissive surfaces' [patent_app_type] => utility [patent_app_number] => 10/346888 [patent_app_country] => US [patent_app_date] => 2003-01-17 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 5 [patent_figures_cnt] => 12 [patent_no_of_words] => 5564 [patent_no_of_claims] => 21 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 45 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/06/921/06921050.pdf [firstpage_image] =>[orig_patent_app_number] => 10346888 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 6626064 [patent_doc_number] => 20030102409 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2003-06-05 [patent_title] => 'Method for placing payload in orbit by multifunctional launch vehicle of combined scheme with cruise liquid rocket engine system (LRES), multifunctional launch vehicle of combined scheme with cruise LRES and method for refining it' [patent_app_type] => new [patent_app_number] => 10/336810 [patent_app_country] => US [patent_app_date] => 2003-01-06 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 10 [patent_figures_cnt] => 10 [patent_no_of_words] => 8236 [patent_no_of_claims] => 8 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 164 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] => publications/A1/0102/20030102409.pdf [firstpage_image] =>[orig_patent_app_number] => 10336810 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 1206413 [patent_doc_number] => 06712319 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2004-03-30 [patent_title] => 'METHOD FOR PLACING PAYLOAD IN ORBIT BY MULTIFUNCTIONAL LAUNCH VEHICLE OF COMBINED SCHEME WITH CRUISE LIQUID ROCKET ENGINE SYSTEM (LRES), MULTIFUNCTIONAL LAUNCH VEHICLE OF COMBINED SCHEME WITH CRUISE LRES AND METHOD OF REFINING IT' [patent_app_type] => B2 [patent_app_number] => 10/336813 [patent_app_country] => US [patent_app_date] => 2003-01-06 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 9 [patent_figures_cnt] => 11 [patent_no_of_words] => 8194 [patent_no_of_claims] => 1 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 184 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/06/712/06712319.pdf [firstpage_image] =>[orig_patent_app_number] => 10336813 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 7328515 [patent_doc_number] => 20040129838 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2004-07-08 [patent_title] => 'Flow control device and method of controlling flow' [patent_app_type] => new [patent_app_number] => 10/336114 [patent_app_country] => US [patent_app_date] => 2003-01-03 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 6 [patent_figures_cnt] => 6 [patent_no_of_words] => 6060 [patent_no_of_claims] => 20 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 48 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] => publications/A1/0129/20040129838.pdf [firstpage_image] =>[orig_patent_app_number] => 10336114 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 1154937 [patent_doc_number] => 06758444 [patent_country] => US [patent_kind] => B1 [patent_issue_date] => 2004-07-06 [patent_title] => 'Momentum control system and method' [patent_app_type] => B1 [patent_app_number] => 10/334202 [patent_app_country] => US [patent_app_date] => 2002-12-30 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 6 [patent_figures_cnt] => 10 [patent_no_of_words] => 3896 [patent_no_of_claims] => 20 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 118 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/06/758/06758444.pdf [firstpage_image] =>[orig_patent_app_number] => 10334202 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 1156896 [patent_doc_number] => 06755377 [patent_country] => US [patent_kind] => B1 [patent_issue_date] => 2004-06-29 [patent_title] => 'Apparatus for observing and stabilizing electrodynamic tethers' [patent_app_type] => B1 [patent_app_number] => 10/325224 [patent_app_country] => US [patent_app_date] => 2002-12-20 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 3 [patent_figures_cnt] => 4 [patent_no_of_words] => 6845 [patent_no_of_claims] => 8 [patent_no_of_ind_claims] => 4 [patent_words_short_claim] => 97 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/06/755/06755377.pdf [firstpage_image] =>[orig_patent_app_number] => 10325224 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 7197634 [patent_doc_number] => 20050051667 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2005-03-10 [patent_title] => 'Micro-rotorcraft surveillance system' [patent_app_type] => utility [patent_app_number] => 10/499530 [patent_app_country] => US [patent_app_date] => 2002-12-19 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 28 [patent_figures_cnt] => 28 [patent_no_of_words] => 11164 [patent_no_of_claims] => 37 [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/A1/0051/20050051667.pdf [firstpage_image] =>[orig_patent_app_number] => 10499530 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 7139774 [patent_doc_number] => 20050116098 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2005-06-02 [patent_title] => 'Flight deck security system' [patent_app_type] => utility [patent_app_number] => 10/500728 [patent_app_country] => US [patent_app_date] => 2002-12-13 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 15 [patent_figures_cnt] => 15 [patent_no_of_words] => 8754 [patent_no_of_claims] => 71 [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/A1/0116/20050116098.pdf [firstpage_image] =>[orig_patent_app_number] => 10500728 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 7301011 [patent_doc_number] => 20040113021 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2004-06-17 [patent_title] => 'Method and computer program product for controlling the control effectors of an aerodynamic vehicle' [patent_app_type] => new [patent_app_number] => 10/317370 [patent_app_country] => US [patent_app_date] => 2002-12-12 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 3 [patent_figures_cnt] => 3 [patent_no_of_words] => 7981 [patent_no_of_claims] => 48 [patent_no_of_ind_claims] => 4 [patent_words_short_claim] => 121 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] => publications/A1/0113/20040113021.pdf [firstpage_image] =>[orig_patent_app_number] => 10317370 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 1243664 [patent_doc_number] => 06676076 [patent_country] => US [patent_kind] => B1 [patent_issue_date] => 2004-01-13 [patent_title] => 'Two stage shock strut' [patent_app_type] => B1 [patent_app_number] => 10/317334 [patent_app_country] => US [patent_app_date] => 2002-12-12 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 4 [patent_figures_cnt] => 6 [patent_no_of_words] => 4656 [patent_no_of_claims] => 16 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 123 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/06/676/06676076.pdf [firstpage_image] =>[orig_patent_app_number] => 10317334 [rel_patent_id] =>[rel_patent_doc_number] =>)