Search

Amanda Lee Bailey

Examiner (ID: 4785)

Most Active Art Unit
3673
Art Unit(s)
3673
Total Applications
468
Issued Applications
245
Pending Applications
48
Abandoned Applications
191

Applications

Application numberTitle of the applicationFiling DateStatus
Array ( [id] => 1008544 [patent_doc_number] => 06899300 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2005-05-31 [patent_title] => 'Process for the loading of fuel into an aircraft on the ground' [patent_app_type] => utility [patent_app_number] => 10/720151 [patent_app_country] => US [patent_app_date] => 2003-11-25 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 5 [patent_figures_cnt] => 8 [patent_no_of_words] => 3247 [patent_no_of_claims] => 8 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 145 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/06/899/06899300.pdf [firstpage_image] =>[orig_patent_app_number] => 10720151 [rel_patent_id] =>[rel_patent_doc_number] =>)
10/720151
Process for the loading of fuel into an aircraft on the ground Nov 24, 2003 Issued
Array ( [id] => 6936318 [patent_doc_number] => 20050109879 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2005-05-26 [patent_title] => 'Method and apparatus for quantum vortex implosion propulsion and species' [patent_app_type] => utility [patent_app_number] => 10/719717 [patent_app_country] => US [patent_app_date] => 2003-11-21 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 25 [patent_figures_cnt] => 25 [patent_no_of_words] => 26010 [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/A1/0109/20050109879.pdf [firstpage_image] =>[orig_patent_app_number] => 10719717 [rel_patent_id] =>[rel_patent_doc_number] =>)
10/719717
Method and apparatus for quantum vortex implosion propulsion and species Nov 20, 2003 Abandoned
Array ( [id] => 7139768 [patent_doc_number] => 20050116092 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2005-06-02 [patent_title] => 'Blended leading and trailing edge wing planform' [patent_app_type] => utility [patent_app_number] => 10/717366 [patent_app_country] => US [patent_app_date] => 2003-11-19 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 2 [patent_figures_cnt] => 2 [patent_no_of_words] => 1348 [patent_no_of_claims] => 14 [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/A1/0116/20050116092.pdf [firstpage_image] =>[orig_patent_app_number] => 10717366 [rel_patent_id] =>[rel_patent_doc_number] =>)
10/717366
Blended leading and trailing edge wing planform Nov 18, 2003 Abandoned
Array ( [id] => 7139793 [patent_doc_number] => 20050116112 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2005-06-02 [patent_title] => 'High energy electric feed drive system' [patent_app_type] => utility [patent_app_number] => 10/717848 [patent_app_country] => US [patent_app_date] => 2003-11-19 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 5 [patent_figures_cnt] => 5 [patent_no_of_words] => 2862 [patent_no_of_claims] => 20 [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/A1/0116/20050116112.pdf [firstpage_image] =>[orig_patent_app_number] => 10717848 [rel_patent_id] =>[rel_patent_doc_number] =>)
10/717848
High energy electric feed drive system Nov 18, 2003 Abandoned
Array ( [id] => 382240 [patent_doc_number] => 07306188 [patent_country] => US [patent_kind] => B1 [patent_issue_date] => 2007-12-11 [patent_title] => 'Non-pyrotechnic remote-controlled parachute jettison device' [patent_app_type] => utility [patent_app_number] => 10/715243 [patent_app_country] => US [patent_app_date] => 2003-11-18 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 4 [patent_figures_cnt] => 4 [patent_no_of_words] => 1208 [patent_no_of_claims] => 6 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 106 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/07/306/07306188.pdf [firstpage_image] =>[orig_patent_app_number] => 10715243 [rel_patent_id] =>[rel_patent_doc_number] =>)
10/715243
Non-pyrotechnic remote-controlled parachute jettison device Nov 17, 2003 Issued
Array ( [id] => 1051835 [patent_doc_number] => 06857597 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2005-02-22 [patent_title] => 'Control system for vertical take off and land (VTOL) aircraft' [patent_app_type] => utility [patent_app_number] => 10/717213 [patent_app_country] => US [patent_app_date] => 2003-11-18 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 13 [patent_figures_cnt] => 14 [patent_no_of_words] => 2497 [patent_no_of_claims] => 19 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 158 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/06/857/06857597.pdf [firstpage_image] =>[orig_patent_app_number] => 10717213 [rel_patent_id] =>[rel_patent_doc_number] =>)
10/717213
Control system for vertical take off and land (VTOL) aircraft Nov 17, 2003 Issued
Array ( [id] => 7218774 [patent_doc_number] => 20040155146 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2004-08-12 [patent_title] => 'Method of controlling a landing guide path of an aircraft' [patent_app_type] => new [patent_app_number] => 10/713160 [patent_app_country] => US [patent_app_date] => 2003-11-17 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 3 [patent_figures_cnt] => 3 [patent_no_of_words] => 3258 [patent_no_of_claims] => 16 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 27 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] => publications/A1/0155/20040155146.pdf [firstpage_image] =>[orig_patent_app_number] => 10713160 [rel_patent_id] =>[rel_patent_doc_number] =>)
10/713160
Method of controlling a landing guide path of an aircraft Nov 16, 2003 Abandoned
Array ( [id] => 703088 [patent_doc_number] => 07059034 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2006-06-13 [patent_title] => 'One-piece closed-shape structure and method of forming same' [patent_app_type] => utility [patent_app_number] => 10/712041 [patent_app_country] => US [patent_app_date] => 2003-11-14 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 65 [patent_figures_cnt] => 79 [patent_no_of_words] => 17576 [patent_no_of_claims] => 4 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 66 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/07/059/07059034.pdf [firstpage_image] =>[orig_patent_app_number] => 10712041 [rel_patent_id] =>[rel_patent_doc_number] =>)
10/712041
One-piece closed-shape structure and method of forming same Nov 13, 2003 Issued
Array ( [id] => 8878272 [patent_doc_number] => 08473254 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2013-06-25 [patent_title] => 'Methods for configuring aircraft to meet performance goals and shock wave disturbance constraints' [patent_app_type] => utility [patent_app_number] => 10/714276 [patent_app_country] => US [patent_app_date] => 2003-11-14 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 10 [patent_figures_cnt] => 21 [patent_no_of_words] => 8042 [patent_no_of_claims] => 22 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 69 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 10714276 [rel_patent_id] =>[rel_patent_doc_number] =>)
10/714276
Methods for configuring aircraft to meet performance goals and shock wave disturbance constraints Nov 13, 2003 Issued
Array ( [id] => 601482 [patent_doc_number] => 07431239 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2008-10-07 [patent_title] => 'One-piece closed-shape structure and method of forming same' [patent_app_type] => utility [patent_app_number] => 10/712042 [patent_app_country] => US [patent_app_date] => 2003-11-14 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 66 [patent_figures_cnt] => 79 [patent_no_of_words] => 17571 [patent_no_of_claims] => 22 [patent_no_of_ind_claims] => 7 [patent_words_short_claim] => 172 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/07/431/07431239.pdf [firstpage_image] =>[orig_patent_app_number] => 10712042 [rel_patent_id] =>[rel_patent_doc_number] =>)
10/712042
One-piece closed-shape structure and method of forming same Nov 13, 2003 Issued
Array ( [id] => 7139764 [patent_doc_number] => 20050116088 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2005-06-02 [patent_title] => 'Shock and vibration isolation system' [patent_app_type] => utility [patent_app_number] => 10/713760 [patent_app_country] => US [patent_app_date] => 2003-11-13 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 10 [patent_figures_cnt] => 10 [patent_no_of_words] => 3312 [patent_no_of_claims] => 29 [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/A1/0116/20050116088.pdf [firstpage_image] =>[orig_patent_app_number] => 10713760 [rel_patent_id] =>[rel_patent_doc_number] =>)
10/713760
Shock and vibration isolation system Nov 12, 2003 Issued
Array ( [id] => 7139761 [patent_doc_number] => 20050116086 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2005-06-02 [patent_title] => 'Wing assemblies for aircraft' [patent_app_type] => utility [patent_app_number] => 10/705529 [patent_app_country] => US [patent_app_date] => 2003-11-12 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 4 [patent_figures_cnt] => 4 [patent_no_of_words] => 1843 [patent_no_of_claims] => 20 [patent_no_of_ind_claims] => 6 [patent_words_short_claim] => 0 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] => publications/A1/0116/20050116086.pdf [firstpage_image] =>[orig_patent_app_number] => 10705529 [rel_patent_id] =>[rel_patent_doc_number] =>)
10/705529
Wing assemblies for aircraft Nov 11, 2003 Abandoned
Array ( [id] => 7139797 [patent_doc_number] => 20050116116 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2005-06-02 [patent_title] => 'Wing employing leading edge flaps and winglets to achieve improved aerodynamic performance' [patent_app_type] => utility [patent_app_number] => 10/706671 [patent_app_country] => US [patent_app_date] => 2003-11-11 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 24 [patent_figures_cnt] => 24 [patent_no_of_words] => 10016 [patent_no_of_claims] => 36 [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/A1/0116/20050116116.pdf [firstpage_image] =>[orig_patent_app_number] => 10706671 [rel_patent_id] =>[rel_patent_doc_number] =>)
10/706671
Wing employing leading edge flaps and winglets to achieve improved aerodynamic performance Nov 10, 2003 Abandoned
Array ( [id] => 1019507 [patent_doc_number] => 06886774 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2005-05-03 [patent_title] => 'Method for piloting a spinning projectile' [patent_app_type] => utility [patent_app_number] => 10/703428 [patent_app_country] => US [patent_app_date] => 2003-11-10 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 7 [patent_figures_cnt] => 7 [patent_no_of_words] => 7090 [patent_no_of_claims] => 5 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 345 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/06/886/06886774.pdf [firstpage_image] =>[orig_patent_app_number] => 10703428 [rel_patent_id] =>[rel_patent_doc_number] =>)
10/703428
Method for piloting a spinning projectile Nov 9, 2003 Issued
Array ( [id] => 7101208 [patent_doc_number] => 20050103934 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2005-05-19 [patent_title] => 'Cargo oriented personal aircraft' [patent_app_type] => utility [patent_app_number] => 10/701146 [patent_app_country] => US [patent_app_date] => 2003-11-04 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 5 [patent_figures_cnt] => 5 [patent_no_of_words] => 2532 [patent_no_of_claims] => 11 [patent_no_of_ind_claims] => 8 [patent_words_short_claim] => 0 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] => publications/A1/0103/20050103934.pdf [firstpage_image] =>[orig_patent_app_number] => 10701146 [rel_patent_id] =>[rel_patent_doc_number] =>)
10/701146
Cargo oriented personal aircraft Nov 3, 2003 Issued
Array ( [id] => 7295622 [patent_doc_number] => 20040124312 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2004-07-01 [patent_title] => 'System and method for use of external secondary payloads' [patent_app_type] => new [patent_app_number] => 10/698261 [patent_app_country] => US [patent_app_date] => 2003-10-31 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 8 [patent_figures_cnt] => 8 [patent_no_of_words] => 9764 [patent_no_of_claims] => 70 [patent_no_of_ind_claims] => 4 [patent_words_short_claim] => 75 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] => publications/A1/0124/20040124312.pdf [firstpage_image] =>[orig_patent_app_number] => 10698261 [rel_patent_id] =>[rel_patent_doc_number] =>)
10/698261
System for use of external secondary payloads Oct 30, 2003 Issued
Array ( [id] => 7439883 [patent_doc_number] => 20040195451 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2004-10-07 [patent_title] => 'Seat-mounting systems and methods' [patent_app_type] => new [patent_app_number] => 10/694241 [patent_app_country] => US [patent_app_date] => 2003-10-27 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 9 [patent_figures_cnt] => 9 [patent_no_of_words] => 1217 [patent_no_of_claims] => 13 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 26 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] => publications/A1/0195/20040195451.pdf [firstpage_image] =>[orig_patent_app_number] => 10694241 [rel_patent_id] =>[rel_patent_doc_number] =>)
10/694241
Seat-mounting systems and methods Oct 26, 2003 Abandoned
Array ( [id] => 4595973 [patent_doc_number] => 07975465 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2011-07-12 [patent_title] => 'Hybrid engine accessory power system' [patent_app_type] => utility [patent_app_number] => 10/694645 [patent_app_country] => US [patent_app_date] => 2003-10-27 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 6 [patent_figures_cnt] => 10 [patent_no_of_words] => 3375 [patent_no_of_claims] => 9 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 132 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/07/975/07975465.pdf [firstpage_image] =>[orig_patent_app_number] => 10694645 [rel_patent_id] =>[rel_patent_doc_number] =>)
10/694645
Hybrid engine accessory power system Oct 26, 2003 Issued
Array ( [id] => 1063959 [patent_doc_number] => 06845939 [patent_country] => US [patent_kind] => B1 [patent_issue_date] => 2005-01-25 [patent_title] => 'Tailboom-stabilized VTOL aircraft' [patent_app_type] => utility [patent_app_number] => 10/693800 [patent_app_country] => US [patent_app_date] => 2003-10-24 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 9 [patent_figures_cnt] => 13 [patent_no_of_words] => 9546 [patent_no_of_claims] => 23 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 61 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/06/845/06845939.pdf [firstpage_image] =>[orig_patent_app_number] => 10693800 [rel_patent_id] =>[rel_patent_doc_number] =>)
10/693800
Tailboom-stabilized VTOL aircraft Oct 23, 2003 Issued
Array ( [id] => 7153955 [patent_doc_number] => 20050082425 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2005-04-21 [patent_title] => 'EMPENNAGE ASSEMBLY AND ATTACHMENT MECHANISM FOR A MODEL AIRPLANE' [patent_app_type] => utility [patent_app_number] => 10/690065 [patent_app_country] => US [patent_app_date] => 2003-10-21 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 4 [patent_figures_cnt] => 4 [patent_no_of_words] => 1984 [patent_no_of_claims] => 11 [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/A1/0082/20050082425.pdf [firstpage_image] =>[orig_patent_app_number] => 10690065 [rel_patent_id] =>[rel_patent_doc_number] =>)
10/690065
Empennage assembly and attachment mechanism for a model airplane Oct 20, 2003 Issued
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