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] => 6747846 [patent_doc_number] => 20030042366 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2003-03-06 [patent_title] => 'Kite structure' [patent_app_type] => new [patent_app_number] => 10/042139 [patent_app_country] => US [patent_app_date] => 2002-01-11 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 7 [patent_figures_cnt] => 7 [patent_no_of_words] => 8224 [patent_no_of_claims] => 20 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 101 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] => publications/A1/0042/20030042366.pdf [firstpage_image] =>[orig_patent_app_number] => 10042139 [rel_patent_id] =>[rel_patent_doc_number] =>)
10/042139
Kite structure Jan 10, 2002 Abandoned
Array ( [id] => 5782617 [patent_doc_number] => 20020158166 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2002-10-31 [patent_title] => 'Device for precaution skyjacking and system' [patent_app_type] => new [patent_app_number] => 10/029951 [patent_app_country] => US [patent_app_date] => 2001-12-31 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 5 [patent_figures_cnt] => 5 [patent_no_of_words] => 5069 [patent_no_of_claims] => 9 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 82 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] => publications/A1/0158/20020158166.pdf [firstpage_image] =>[orig_patent_app_number] => 10029951 [rel_patent_id] =>[rel_patent_doc_number] =>)
10/029951
Device for precaution skyjacking and system Dec 30, 2001 Abandoned
09/980637 Method on regulating the air flow around the windmill wing and device for use in such method Dec 27, 2001 Abandoned
Array ( [id] => 1437813 [patent_doc_number] => 06494407 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2002-12-17 [patent_title] => 'Joint on a spacecraft' [patent_app_type] => B2 [patent_app_number] => 10/013841 [patent_app_country] => US [patent_app_date] => 2001-12-13 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 1 [patent_figures_cnt] => 1 [patent_no_of_words] => 1109 [patent_no_of_claims] => 5 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 172 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/06/494/06494407.pdf [firstpage_image] =>[orig_patent_app_number] => 10013841 [rel_patent_id] =>[rel_patent_doc_number] =>)
10/013841
Joint on a spacecraft Dec 12, 2001 Issued
Array ( [id] => 1358776 [patent_doc_number] => 06557802 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2003-05-06 [patent_title] => 'Device for separation of a plurality of axially arranged satellites' [patent_app_type] => B2 [patent_app_number] => 10/012566 [patent_app_country] => US [patent_app_date] => 2001-12-12 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 3 [patent_figures_cnt] => 4 [patent_no_of_words] => 1505 [patent_no_of_claims] => 7 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 66 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/06/557/06557802.pdf [firstpage_image] =>[orig_patent_app_number] => 10012566 [rel_patent_id] =>[rel_patent_doc_number] =>)
10/012566
Device for separation of a plurality of axially arranged satellites Dec 11, 2001 Issued
Array ( [id] => 1354981 [patent_doc_number] => 06561456 [patent_country] => US [patent_kind] => B1 [patent_issue_date] => 2003-05-13 [patent_title] => 'Vertical/short take-off and landing aircraft' [patent_app_type] => B1 [patent_app_number] => 10/010649 [patent_app_country] => US [patent_app_date] => 2001-12-06 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 4 [patent_figures_cnt] => 16 [patent_no_of_words] => 5672 [patent_no_of_claims] => 25 [patent_no_of_ind_claims] => 4 [patent_words_short_claim] => 117 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/06/561/06561456.pdf [firstpage_image] =>[orig_patent_app_number] => 10010649 [rel_patent_id] =>[rel_patent_doc_number] =>)
10/010649
Vertical/short take-off and landing aircraft Dec 5, 2001 Issued
Array ( [id] => 1193974 [patent_doc_number] => 06726154 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2004-04-27 [patent_title] => 'Reusable space access launch vehicle system' [patent_app_type] => B2 [patent_app_number] => 10/000430 [patent_app_country] => US [patent_app_date] => 2001-11-30 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 2 [patent_figures_cnt] => 2 [patent_no_of_words] => 1327 [patent_no_of_claims] => 12 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 45 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/06/726/06726154.pdf [firstpage_image] =>[orig_patent_app_number] => 10000430 [rel_patent_id] =>[rel_patent_doc_number] =>)
10/000430
Reusable space access launch vehicle system Nov 29, 2001 Issued
Array ( [id] => 1286625 [patent_doc_number] => 06629673 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2003-10-07 [patent_title] => 'Adaptable solid-hybrid rocket for crew escape and orbital injection propulsion' [patent_app_type] => B2 [patent_app_number] => 09/996532 [patent_app_country] => US [patent_app_date] => 2001-11-28 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 2 [patent_figures_cnt] => 2 [patent_no_of_words] => 1921 [patent_no_of_claims] => 21 [patent_no_of_ind_claims] => 6 [patent_words_short_claim] => 89 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/06/629/06629673.pdf [firstpage_image] =>[orig_patent_app_number] => 09996532 [rel_patent_id] =>[rel_patent_doc_number] =>)
09/996532
Adaptable solid-hybrid rocket for crew escape and orbital injection propulsion Nov 27, 2001 Issued
Array ( [id] => 6568982 [patent_doc_number] => 20020084382 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2002-07-04 [patent_title] => 'Aircraft deicer' [patent_app_type] => new [patent_app_number] => 09/995242 [patent_app_country] => US [patent_app_date] => 2001-11-27 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 2 [patent_figures_cnt] => 2 [patent_no_of_words] => 2069 [patent_no_of_claims] => 33 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 37 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] => publications/A1/0084/20020084382.pdf [firstpage_image] =>[orig_patent_app_number] => 09995242 [rel_patent_id] =>[rel_patent_doc_number] =>)
09/995242
Aircraft deicer Nov 26, 2001 Abandoned
Array ( [id] => 1228019 [patent_doc_number] => 06691955 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2004-02-17 [patent_title] => 'Spacecraft having a momentum wheel configuration that prevents zero wheel speeds' [patent_app_type] => B2 [patent_app_number] => 09/995017 [patent_app_country] => US [patent_app_date] => 2001-11-27 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 2 [patent_figures_cnt] => 4 [patent_no_of_words] => 2114 [patent_no_of_claims] => 12 [patent_no_of_ind_claims] => 4 [patent_words_short_claim] => 30 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/06/691/06691955.pdf [firstpage_image] =>[orig_patent_app_number] => 09995017 [rel_patent_id] =>[rel_patent_doc_number] =>)
09/995017
Spacecraft having a momentum wheel configuration that prevents zero wheel speeds Nov 26, 2001 Issued
Array ( [id] => 6569010 [patent_doc_number] => 20020084384 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2002-07-04 [patent_title] => 'Kite control systems' [patent_app_type] => new [patent_app_number] => 09/990758 [patent_app_country] => US [patent_app_date] => 2001-11-16 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 12 [patent_figures_cnt] => 12 [patent_no_of_words] => 15606 [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/A1/0084/20020084384.pdf [firstpage_image] =>[orig_patent_app_number] => 09990758 [rel_patent_id] =>[rel_patent_doc_number] =>)
09/990758
Kite control systems Nov 15, 2001 Issued
Array ( [id] => 6348337 [patent_doc_number] => 20020056788 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2002-05-16 [patent_title] => 'One-piece closed-shape structure and method of forming same' [patent_app_type] => new [patent_app_number] => 09/987612 [patent_app_country] => US [patent_app_date] => 2001-11-15 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 66 [patent_figures_cnt] => 66 [patent_no_of_words] => 17856 [patent_no_of_claims] => 67 [patent_no_of_ind_claims] => 11 [patent_words_short_claim] => 44 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] => publications/A1/0056/20020056788.pdf [firstpage_image] =>[orig_patent_app_number] => 09987612 [rel_patent_id] =>[rel_patent_doc_number] =>)
09/987612
One-piece closed-shape structure and method of forming same Nov 14, 2001 Issued
Array ( [id] => 6955480 [patent_doc_number] => 20050211850 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2005-09-29 [patent_title] => 'TWO-SIDED DEPLOYABLE THERMAL RADIATOR SYSTEM AND METHOD' [patent_app_type] => utility [patent_app_number] => 10/007256 [patent_app_country] => US [patent_app_date] => 2001-11-11 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 4 [patent_figures_cnt] => 4 [patent_no_of_words] => 1303 [patent_no_of_claims] => 3 [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/A1/0211/20050211850.pdf [firstpage_image] =>[orig_patent_app_number] => 10007256 [rel_patent_id] =>[rel_patent_doc_number] =>)
10/007256
Two-sided deployable thermal radiator system and method Nov 10, 2001 Issued
Array ( [id] => 1595035 [patent_doc_number] => 06474601 [patent_country] => US [patent_kind] => B1 [patent_issue_date] => 2002-11-05 [patent_title] => 'Warren portal identification and tunnel resident disgorger system' [patent_app_type] => B1 [patent_app_number] => 10/004241 [patent_app_country] => US [patent_app_date] => 2001-11-02 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 2 [patent_figures_cnt] => 2 [patent_no_of_words] => 3429 [patent_no_of_claims] => 22 [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/06/474/06474601.pdf [firstpage_image] =>[orig_patent_app_number] => 10004241 [rel_patent_id] =>[rel_patent_doc_number] =>)
10/004241
Warren portal identification and tunnel resident disgorger system Nov 1, 2001 Issued
Array ( [id] => 6854060 [patent_doc_number] => 20030127561 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2003-07-10 [patent_title] => 'Wing airfoil' [patent_app_type] => new [patent_app_number] => 09/982972 [patent_app_country] => US [patent_app_date] => 2001-10-22 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 10 [patent_figures_cnt] => 10 [patent_no_of_words] => 3720 [patent_no_of_claims] => 22 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 60 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] => publications/A1/0127/20030127561.pdf [firstpage_image] =>[orig_patent_app_number] => 09982972 [rel_patent_id] =>[rel_patent_doc_number] =>)
09/982972
Wing airfoil Oct 21, 2001 Issued
Array ( [id] => 1299710 [patent_doc_number] => 06616097 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2003-09-09 [patent_title] => 'Reconfigurable reconnaissance pod system' [patent_app_type] => B2 [patent_app_number] => 09/977461 [patent_app_country] => US [patent_app_date] => 2001-10-15 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 8 [patent_figures_cnt] => 9 [patent_no_of_words] => 2013 [patent_no_of_claims] => 16 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 145 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/06/616/06616097.pdf [firstpage_image] =>[orig_patent_app_number] => 09977461 [rel_patent_id] =>[rel_patent_doc_number] =>)
09/977461
Reconfigurable reconnaissance pod system Oct 14, 2001 Issued
Array ( [id] => 251853 [patent_doc_number] => 07578483 [patent_country] => US [patent_kind] => B1 [patent_issue_date] => 2009-08-25 [patent_title] => 'Conformable skin element system for active vortex control' [patent_app_type] => utility [patent_app_number] => 09/975507 [patent_app_country] => US [patent_app_date] => 2001-10-12 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 5 [patent_figures_cnt] => 5 [patent_no_of_words] => 1771 [patent_no_of_claims] => 22 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 61 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/07/578/07578483.pdf [firstpage_image] =>[orig_patent_app_number] => 09975507 [rel_patent_id] =>[rel_patent_doc_number] =>)
09/975507
Conformable skin element system for active vortex control Oct 11, 2001 Issued
Array ( [id] => 1446612 [patent_doc_number] => 06454220 [patent_country] => US [patent_kind] => B1 [patent_issue_date] => 2002-09-24 [patent_title] => 'Evacuation slide with toe end center support member' [patent_app_type] => B1 [patent_app_number] => 09/976479 [patent_app_country] => US [patent_app_date] => 2001-10-11 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 2 [patent_figures_cnt] => 5 [patent_no_of_words] => 2153 [patent_no_of_claims] => 5 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 49 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/06/454/06454220.pdf [firstpage_image] =>[orig_patent_app_number] => 09976479 [rel_patent_id] =>[rel_patent_doc_number] =>)
09/976479
Evacuation slide with toe end center support member Oct 10, 2001 Issued
Array ( [id] => 1334948 [patent_doc_number] => 06581881 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2003-06-24 [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] => B2 [patent_app_number] => 09/972006 [patent_app_country] => US [patent_app_date] => 2001-10-09 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 9 [patent_figures_cnt] => 11 [patent_no_of_words] => 8188 [patent_no_of_claims] => 4 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 352 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/06/581/06581881.pdf [firstpage_image] =>[orig_patent_app_number] => 09972006 [rel_patent_id] =>[rel_patent_doc_number] =>)
09/972006
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 Oct 8, 2001 Issued
Array ( [id] => 1574275 [patent_doc_number] => 06446904 [patent_country] => US [patent_kind] => B1 [patent_issue_date] => 2002-09-10 [patent_title] => 'Aircraft weapons bay high frequency acoustic suppression apparatus' [patent_app_type] => B1 [patent_app_number] => 09/973175 [patent_app_country] => US [patent_app_date] => 2001-10-05 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 7 [patent_figures_cnt] => 7 [patent_no_of_words] => 3719 [patent_no_of_claims] => 7 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 86 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/06/446/06446904.pdf [firstpage_image] =>[orig_patent_app_number] => 09973175 [rel_patent_id] =>[rel_patent_doc_number] =>)
09/973175
Aircraft weapons bay high frequency acoustic suppression apparatus Oct 4, 2001 Issued
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