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] => 7267633 [patent_doc_number] => 20040056151 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2004-03-25 [patent_title] => 'High temperature resistant airfoil apparatus for a hypersonic space vehicle' [patent_app_type] => new [patent_app_number] => 10/431414 [patent_app_country] => US [patent_app_date] => 2003-05-07 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 3 [patent_figures_cnt] => 3 [patent_no_of_words] => 2431 [patent_no_of_claims] => 19 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 90 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] => publications/A1/0056/20040056151.pdf [firstpage_image] =>[orig_patent_app_number] => 10431414 [rel_patent_id] =>[rel_patent_doc_number] =>)
10/431414
High temperature resistant airfoil apparatus for a hypersonic space vehicle May 6, 2003 Abandoned
Array ( [id] => 6803277 [patent_doc_number] => 20030230671 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2003-12-18 [patent_title] => 'Fuel cell powered electric aircraft' [patent_app_type] => new [patent_app_number] => 10/431052 [patent_app_country] => US [patent_app_date] => 2003-05-06 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 5 [patent_figures_cnt] => 5 [patent_no_of_words] => 5120 [patent_no_of_claims] => 18 [patent_no_of_ind_claims] => 4 [patent_words_short_claim] => 41 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] => publications/A1/0230/20030230671.pdf [firstpage_image] =>[orig_patent_app_number] => 10431052 [rel_patent_id] =>[rel_patent_doc_number] =>)
10/431052
Fuel cell powered electric aircraft May 5, 2003 Abandoned
Array ( [id] => 7318571 [patent_doc_number] => 20040135035 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2004-07-15 [patent_title] => 'Momentum stabilized launch vehicle upper stage' [patent_app_type] => new [patent_app_number] => 10/427111 [patent_app_country] => US [patent_app_date] => 2003-04-30 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 5 [patent_figures_cnt] => 5 [patent_no_of_words] => 5138 [patent_no_of_claims] => 34 [patent_no_of_ind_claims] => 5 [patent_words_short_claim] => 86 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] => publications/A1/0135/20040135035.pdf [firstpage_image] =>[orig_patent_app_number] => 10427111 [rel_patent_id] =>[rel_patent_doc_number] =>)
10/427111
Momentum stabilized launch vehicle upper stage Apr 29, 2003 Issued
Array ( [id] => 1096387 [patent_doc_number] => 06817578 [patent_country] => US [patent_kind] => B1 [patent_issue_date] => 2004-11-16 [patent_title] => 'Enhanced aerial delivery system (EADS) platform' [patent_app_type] => B1 [patent_app_number] => 10/425147 [patent_app_country] => US [patent_app_date] => 2003-04-28 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 13 [patent_figures_cnt] => 19 [patent_no_of_words] => 5708 [patent_no_of_claims] => 29 [patent_no_of_ind_claims] => 10 [patent_words_short_claim] => 117 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/06/817/06817578.pdf [firstpage_image] =>[orig_patent_app_number] => 10425147 [rel_patent_id] =>[rel_patent_doc_number] =>)
10/425147
Enhanced aerial delivery system (EADS) platform Apr 27, 2003 Issued
Array ( [id] => 7426695 [patent_doc_number] => 20040007644 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2004-01-15 [patent_title] => 'Rotor craft' [patent_app_type] => new [patent_app_number] => 10/423831 [patent_app_country] => US [patent_app_date] => 2003-04-25 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 11 [patent_figures_cnt] => 11 [patent_no_of_words] => 9245 [patent_no_of_claims] => 25 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 14 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] => publications/A1/0007/20040007644.pdf [firstpage_image] =>[orig_patent_app_number] => 10423831 [rel_patent_id] =>[rel_patent_doc_number] =>)
10/423831
Rotor craft Apr 24, 2003 Abandoned
Array ( [id] => 7337987 [patent_doc_number] => 20040245382 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2004-12-09 [patent_title] => 'Aircraft which employs hydrogen as fuel' [patent_app_type] => new [patent_app_number] => 10/419302 [patent_app_country] => US [patent_app_date] => 2003-04-22 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 3 [patent_figures_cnt] => 3 [patent_no_of_words] => 6756 [patent_no_of_claims] => 2 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 102 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] => publications/A1/0245/20040245382.pdf [firstpage_image] =>[orig_patent_app_number] => 10419302 [rel_patent_id] =>[rel_patent_doc_number] =>)
10/419302
Aircraft which employs hydrogen as fuel Apr 21, 2003 Abandoned
Array ( [id] => 7432704 [patent_doc_number] => 20040065781 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2004-04-08 [patent_title] => 'Satellite constellations using nodally-adjusted repeating ground track orbits' [patent_app_type] => new [patent_app_number] => 10/420279 [patent_app_country] => US [patent_app_date] => 2003-04-22 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 25 [patent_figures_cnt] => 25 [patent_no_of_words] => 8375 [patent_no_of_claims] => 30 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 64 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] => publications/A1/0065/20040065781.pdf [firstpage_image] =>[orig_patent_app_number] => 10420279 [rel_patent_id] =>[rel_patent_doc_number] =>)
10/420279
Satellite constellations using nodally-adjusted repeating ground track orbits Apr 21, 2003 Issued
Array ( [id] => 7410489 [patent_doc_number] => 20040206853 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2004-10-21 [patent_title] => 'Apparatus and methods of attaching panels to support structures' [patent_app_type] => new [patent_app_number] => 10/418400 [patent_app_country] => US [patent_app_date] => 2003-04-18 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 6 [patent_figures_cnt] => 6 [patent_no_of_words] => 3054 [patent_no_of_claims] => 37 [patent_no_of_ind_claims] => 4 [patent_words_short_claim] => 88 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] => publications/A1/0206/20040206853.pdf [firstpage_image] =>[orig_patent_app_number] => 10418400 [rel_patent_id] =>[rel_patent_doc_number] =>)
10/418400
Apparatus and methods of attaching panels to support structures Apr 17, 2003 Issued
Array ( [id] => 7132592 [patent_doc_number] => 20050178924 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2005-08-18 [patent_title] => 'Perforated skin structure for laminar-flow systems' [patent_app_type] => utility [patent_app_number] => 10/511930 [patent_app_country] => US [patent_app_date] => 2003-04-17 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 11 [patent_figures_cnt] => 11 [patent_no_of_words] => 8906 [patent_no_of_claims] => 31 [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/A1/0178/20050178924.pdf [firstpage_image] =>[orig_patent_app_number] => 10511930 [rel_patent_id] =>[rel_patent_doc_number] =>)
10/511930
Perforated skin structure for laminar-flow systems Apr 16, 2003 Issued
Array ( [id] => 1011754 [patent_doc_number] => 06896221 [patent_country] => US [patent_kind] => B1 [patent_issue_date] => 2005-05-24 [patent_title] => 'Vertical takeoff and landing aircraft' [patent_app_type] => utility [patent_app_number] => 10/414874 [patent_app_country] => US [patent_app_date] => 2003-04-16 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 5 [patent_figures_cnt] => 13 [patent_no_of_words] => 6609 [patent_no_of_claims] => 12 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 250 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/06/896/06896221.pdf [firstpage_image] =>[orig_patent_app_number] => 10414874 [rel_patent_id] =>[rel_patent_doc_number] =>)
10/414874
Vertical takeoff and landing aircraft Apr 15, 2003 Issued
Array ( [id] => 670534 [patent_doc_number] => 07090164 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2006-08-15 [patent_title] => 'Method for producing a lift and a horizontal thrust' [patent_app_type] => utility [patent_app_number] => 10/511780 [patent_app_country] => US [patent_app_date] => 2003-04-14 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 5 [patent_figures_cnt] => 5 [patent_no_of_words] => 1984 [patent_no_of_claims] => 2 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 148 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/07/090/07090164.pdf [firstpage_image] =>[orig_patent_app_number] => 10511780 [rel_patent_id] =>[rel_patent_doc_number] =>)
10/511780
Method for producing a lift and a horizontal thrust Apr 13, 2003 Issued
Array ( [id] => 1228000 [patent_doc_number] => 06691948 [patent_country] => US [patent_kind] => B1 [patent_issue_date] => 2004-02-17 [patent_title] => 'High torque rocket nozzle' [patent_app_type] => B1 [patent_app_number] => 10/413182 [patent_app_country] => US [patent_app_date] => 2003-04-10 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 1 [patent_figures_cnt] => 2 [patent_no_of_words] => 2907 [patent_no_of_claims] => 20 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 64 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/06/691/06691948.pdf [firstpage_image] =>[orig_patent_app_number] => 10413182 [rel_patent_id] =>[rel_patent_doc_number] =>)
10/413182
High torque rocket nozzle Apr 9, 2003 Issued
Array ( [id] => 1058016 [patent_doc_number] => 06851647 [patent_country] => US [patent_kind] => B1 [patent_issue_date] => 2005-02-08 [patent_title] => 'Portable catapult launcher for small aircraft' [patent_app_type] => utility [patent_app_number] => 10/417377 [patent_app_country] => US [patent_app_date] => 2003-04-03 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 16 [patent_figures_cnt] => 22 [patent_no_of_words] => 5207 [patent_no_of_claims] => 12 [patent_no_of_ind_claims] => 4 [patent_words_short_claim] => 227 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/06/851/06851647.pdf [firstpage_image] =>[orig_patent_app_number] => 10417377 [rel_patent_id] =>[rel_patent_doc_number] =>)
10/417377
Portable catapult launcher for small aircraft Apr 2, 2003 Issued
Array ( [id] => 7333588 [patent_doc_number] => 20040188563 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2004-09-30 [patent_title] => 'Efficient cargo liner installation' [patent_app_type] => new [patent_app_number] => 10/402508 [patent_app_country] => US [patent_app_date] => 2003-03-27 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 6 [patent_figures_cnt] => 6 [patent_no_of_words] => 5708 [patent_no_of_claims] => 73 [patent_no_of_ind_claims] => 4 [patent_words_short_claim] => 81 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] => publications/A1/0188/20040188563.pdf [firstpage_image] =>[orig_patent_app_number] => 10402508 [rel_patent_id] =>[rel_patent_doc_number] =>)
10/402508
Efficient cargo liner installation Mar 26, 2003 Issued
Array ( [id] => 7387607 [patent_doc_number] => 20040016846 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2004-01-29 [patent_title] => 'Launch vehicle payload carrier and related methods' [patent_app_type] => new [patent_app_number] => 10/397499 [patent_app_country] => US [patent_app_date] => 2003-03-26 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 22 [patent_figures_cnt] => 22 [patent_no_of_words] => 5168 [patent_no_of_claims] => 20 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 46 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] => publications/A1/0016/20040016846.pdf [firstpage_image] =>[orig_patent_app_number] => 10397499 [rel_patent_id] =>[rel_patent_doc_number] =>)
10/397499
Launch vehicle payload carrier and related methods Mar 25, 2003 Issued
Array ( [id] => 6702608 [patent_doc_number] => 20030225488 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2003-12-04 [patent_title] => 'Chemical application and flight guidance control system and method' [patent_app_type] => new [patent_app_number] => 10/397040 [patent_app_country] => US [patent_app_date] => 2003-03-25 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 6 [patent_figures_cnt] => 6 [patent_no_of_words] => 3453 [patent_no_of_claims] => 20 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 65 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] => publications/A1/0225/20030225488.pdf [firstpage_image] =>[orig_patent_app_number] => 10397040 [rel_patent_id] =>[rel_patent_doc_number] =>)
10/397040
Chemical application and flight guidance control system and method Mar 24, 2003 Issued
Array ( [id] => 1084610 [patent_doc_number] => 06830222 [patent_country] => US [patent_kind] => B1 [patent_issue_date] => 2004-12-14 [patent_title] => 'Balloon device for lowering space object orbits' [patent_app_type] => B1 [patent_app_number] => 10/394477 [patent_app_country] => US [patent_app_date] => 2003-03-21 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 9 [patent_figures_cnt] => 16 [patent_no_of_words] => 8071 [patent_no_of_claims] => 24 [patent_no_of_ind_claims] => 4 [patent_words_short_claim] => 64 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/06/830/06830222.pdf [firstpage_image] =>[orig_patent_app_number] => 10394477 [rel_patent_id] =>[rel_patent_doc_number] =>)
10/394477
Balloon device for lowering space object orbits Mar 20, 2003 Issued
Array ( [id] => 7132562 [patent_doc_number] => 20050178911 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2005-08-18 [patent_title] => 'Triple-fuselage aircraft and families of aircraft of said type' [patent_app_type] => utility [patent_app_number] => 10/504318 [patent_app_country] => US [patent_app_date] => 2003-03-21 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 6 [patent_figures_cnt] => 6 [patent_no_of_words] => 10476 [patent_no_of_claims] => 42 [patent_no_of_ind_claims] => 13 [patent_words_short_claim] => 0 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] => publications/A1/0178/20050178911.pdf [firstpage_image] =>[orig_patent_app_number] => 10504318 [rel_patent_id] =>[rel_patent_doc_number] =>)
10/504318
Triple-fuselage aircraft and families of aircraft of said type Mar 20, 2003 Issued
Array ( [id] => 6727532 [patent_doc_number] => 20030183722 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2003-10-02 [patent_title] => 'Device for controlling the pitch of the blades of a convertible aircraft rotor' [patent_app_type] => new [patent_app_number] => 10/392645 [patent_app_country] => US [patent_app_date] => 2003-03-20 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 6 [patent_figures_cnt] => 6 [patent_no_of_words] => 6370 [patent_no_of_claims] => 12 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 432 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] => publications/A1/0183/20030183722.pdf [firstpage_image] =>[orig_patent_app_number] => 10392645 [rel_patent_id] =>[rel_patent_doc_number] =>)
10/392645
Device for controlling the pitch of the blades of a convertible aircraft rotor Mar 19, 2003 Issued
Array ( [id] => 7419984 [patent_doc_number] => 20040182968 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2004-09-23 [patent_title] => 'Traction kite harness safety release' [patent_app_type] => new [patent_app_number] => 10/391916 [patent_app_country] => US [patent_app_date] => 2003-03-19 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 13 [patent_figures_cnt] => 13 [patent_no_of_words] => 11259 [patent_no_of_claims] => 16 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 71 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] => publications/A1/0182/20040182968.pdf [firstpage_image] =>[orig_patent_app_number] => 10391916 [rel_patent_id] =>[rel_patent_doc_number] =>)
10/391916
Traction kite harness safety release Mar 18, 2003 Abandoned
Menu