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] => 1148374 [patent_doc_number] => 06764043 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2004-07-20 [patent_title] => 'Rotatable scarf inlet for an aircraft engine and method of using the same' [patent_app_type] => B2 [patent_app_number] => 10/316497 [patent_app_country] => US [patent_app_date] => 2002-12-11 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 4 [patent_figures_cnt] => 11 [patent_no_of_words] => 3498 [patent_no_of_claims] => 46 [patent_no_of_ind_claims] => 5 [patent_words_short_claim] => 63 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/06/764/06764043.pdf [firstpage_image] =>[orig_patent_app_number] => 10316497 [rel_patent_id] =>[rel_patent_doc_number] =>)
10/316497
Rotatable scarf inlet for an aircraft engine and method of using the same Dec 10, 2002 Issued
Array ( [id] => 6785635 [patent_doc_number] => 20030136874 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2003-07-24 [patent_title] => 'Method for safer mid-air refueling' [patent_app_type] => new [patent_app_number] => 10/316623 [patent_app_country] => US [patent_app_date] => 2002-12-10 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 8 [patent_figures_cnt] => 8 [patent_no_of_words] => 7250 [patent_no_of_claims] => 3 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 390 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] => publications/A1/0136/20030136874.pdf [firstpage_image] =>[orig_patent_app_number] => 10316623 [rel_patent_id] =>[rel_patent_doc_number] =>)
10/316623
Method for safer mid-air refueling Dec 9, 2002 Abandoned
Array ( [id] => 1193965 [patent_doc_number] => 06726150 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2004-04-27 [patent_title] => 'Method and apparatus for stiffener reinforcement of a ram air parachute canopy' [patent_app_type] => B2 [patent_app_number] => 10/315488 [patent_app_country] => US [patent_app_date] => 2002-12-09 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 2 [patent_figures_cnt] => 5 [patent_no_of_words] => 1835 [patent_no_of_claims] => 13 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 40 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/06/726/06726150.pdf [firstpage_image] =>[orig_patent_app_number] => 10315488 [rel_patent_id] =>[rel_patent_doc_number] =>)
10/315488
Method and apparatus for stiffener reinforcement of a ram air parachute canopy Dec 8, 2002 Issued
Array ( [id] => 1142963 [patent_doc_number] => 06769649 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2004-08-03 [patent_title] => 'Ram air parachute canopy with improved nose structure' [patent_app_type] => B2 [patent_app_number] => 10/315459 [patent_app_country] => US [patent_app_date] => 2002-12-09 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 5 [patent_figures_cnt] => 11 [patent_no_of_words] => 4117 [patent_no_of_claims] => 8 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 102 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/06/769/06769649.pdf [firstpage_image] =>[orig_patent_app_number] => 10315459 [rel_patent_id] =>[rel_patent_doc_number] =>)
10/315459
Ram air parachute canopy with improved nose structure Dec 8, 2002 Issued
Array ( [id] => 1061417 [patent_doc_number] => 06848649 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2005-02-01 [patent_title] => 'V/STOL biplane aircraft' [patent_app_type] => utility [patent_app_number] => 10/313580 [patent_app_country] => US [patent_app_date] => 2002-12-09 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 18 [patent_figures_cnt] => 41 [patent_no_of_words] => 18523 [patent_no_of_claims] => 20 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 420 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/06/848/06848649.pdf [firstpage_image] =>[orig_patent_app_number] => 10313580 [rel_patent_id] =>[rel_patent_doc_number] =>)
10/313580
V/STOL biplane aircraft Dec 8, 2002 Issued
Array ( [id] => 6666594 [patent_doc_number] => 20030111577 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2003-06-19 [patent_title] => 'Membrane structure' [patent_app_type] => new [patent_app_number] => 10/310840 [patent_app_country] => US [patent_app_date] => 2002-12-06 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 6 [patent_figures_cnt] => 6 [patent_no_of_words] => 5115 [patent_no_of_claims] => 6 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 156 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] => publications/A1/0111/20030111577.pdf [firstpage_image] =>[orig_patent_app_number] => 10310840 [rel_patent_id] =>[rel_patent_doc_number] =>)
10/310840
Membrane structure Dec 5, 2002 Issued
Array ( [id] => 6694767 [patent_doc_number] => 20030106961 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2003-06-12 [patent_title] => 'Method and device for steepening a landing approach of an aircraft' [patent_app_type] => new [patent_app_number] => 10/313052 [patent_app_country] => US [patent_app_date] => 2002-12-06 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 3 [patent_figures_cnt] => 3 [patent_no_of_words] => 3234 [patent_no_of_claims] => 22 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 74 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] => publications/A1/0106/20030106961.pdf [firstpage_image] =>[orig_patent_app_number] => 10313052 [rel_patent_id] =>[rel_patent_doc_number] =>)
10/313052
Method and device for steepening a landing approach of an aircraft Dec 5, 2002 Issued
Array ( [id] => 453905 [patent_doc_number] => 07243879 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2007-07-17 [patent_title] => 'Lattice fin for missiles or other fluid-born bodies and method for producing same' [patent_app_type] => utility [patent_app_number] => 10/313222 [patent_app_country] => US [patent_app_date] => 2002-12-06 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 8 [patent_figures_cnt] => 17 [patent_no_of_words] => 5324 [patent_no_of_claims] => 21 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 117 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/07/243/07243879.pdf [firstpage_image] =>[orig_patent_app_number] => 10313222 [rel_patent_id] =>[rel_patent_doc_number] =>)
10/313222
Lattice fin for missiles or other fluid-born bodies and method for producing same Dec 5, 2002 Issued
Array ( [id] => 502850 [patent_doc_number] => 07198225 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2007-04-03 [patent_title] => 'Aircraft control system' [patent_app_type] => utility [patent_app_number] => 10/310415 [patent_app_country] => US [patent_app_date] => 2002-12-05 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 28 [patent_figures_cnt] => 38 [patent_no_of_words] => 14299 [patent_no_of_claims] => 8 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 142 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/07/198/07198225.pdf [firstpage_image] =>[orig_patent_app_number] => 10310415 [rel_patent_id] =>[rel_patent_doc_number] =>)
10/310415
Aircraft control system Dec 4, 2002 Issued
Array ( [id] => 7080386 [patent_doc_number] => 20050045766 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2005-03-03 [patent_title] => 'FORM FACTORED COMPLIANT METALLIC TRANSITION ELEMENT FOR ATTACHING A CERAMIC ELEMENT TO A METALLIC ELEMENT' [patent_app_type] => utility [patent_app_number] => 10/313713 [patent_app_country] => US [patent_app_date] => 2002-12-04 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 3 [patent_figures_cnt] => 3 [patent_no_of_words] => 4913 [patent_no_of_claims] => 30 [patent_no_of_ind_claims] => 9 [patent_words_short_claim] => 0 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] => publications/A1/0045/20050045766.pdf [firstpage_image] =>[orig_patent_app_number] => 10313713 [rel_patent_id] =>[rel_patent_doc_number] =>)
10/313713
Form factored compliant metallic transition element for attaching a ceramic element to a metallic element Dec 3, 2002 Issued
Array ( [id] => 8100903 [patent_doc_number] => 08152099 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2012-04-10 [patent_title] => 'Method of landing an aircraft and apparatus therefor' [patent_app_type] => utility [patent_app_number] => 10/497317 [patent_app_country] => US [patent_app_date] => 2002-12-03 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 3 [patent_figures_cnt] => 7 [patent_no_of_words] => 5867 [patent_no_of_claims] => 12 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 68 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/08/152/08152099.pdf [firstpage_image] =>[orig_patent_app_number] => 10497317 [rel_patent_id] =>[rel_patent_doc_number] =>)
10/497317
Method of landing an aircraft and apparatus therefor Dec 2, 2002 Issued
Array ( [id] => 1253779 [patent_doc_number] => 06666407 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2003-12-23 [patent_title] => 'Helicopter undercarriage' [patent_app_type] => B2 [patent_app_number] => 10/304910 [patent_app_country] => US [patent_app_date] => 2002-11-26 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 5 [patent_figures_cnt] => 5 [patent_no_of_words] => 2517 [patent_no_of_claims] => 13 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 120 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/06/666/06666407.pdf [firstpage_image] =>[orig_patent_app_number] => 10304910 [rel_patent_id] =>[rel_patent_doc_number] =>)
10/304910
Helicopter undercarriage Nov 25, 2002 Issued
Array ( [id] => 615099 [patent_doc_number] => 07143981 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2006-12-05 [patent_title] => 'Parachute rescue system for multistory buildings' [patent_app_type] => utility [patent_app_number] => 10/494519 [patent_app_country] => US [patent_app_date] => 2002-11-13 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 2 [patent_figures_cnt] => 4 [patent_no_of_words] => 2876 [patent_no_of_claims] => 16 [patent_no_of_ind_claims] => 5 [patent_words_short_claim] => 53 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/07/143/07143981.pdf [firstpage_image] =>[orig_patent_app_number] => 10494519 [rel_patent_id] =>[rel_patent_doc_number] =>)
10/494519
Parachute rescue system for multistory buildings Nov 12, 2002 Issued
Array ( [id] => 1243660 [patent_doc_number] => 06676072 [patent_country] => US [patent_kind] => B1 [patent_issue_date] => 2004-01-13 [patent_title] => 'Short duration, high-torque rocket nozzle' [patent_app_type] => B1 [patent_app_number] => 10/292948 [patent_app_country] => US [patent_app_date] => 2002-11-13 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 1 [patent_figures_cnt] => 2 [patent_no_of_words] => 4061 [patent_no_of_claims] => 18 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 131 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/06/676/06676072.pdf [firstpage_image] =>[orig_patent_app_number] => 10292948 [rel_patent_id] =>[rel_patent_doc_number] =>)
10/292948
Short duration, high-torque rocket nozzle Nov 12, 2002 Issued
Array ( [id] => 7352915 [patent_doc_number] => 20040089763 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2004-05-13 [patent_title] => 'Personal flight vehicle and system' [patent_app_type] => new [patent_app_number] => 10/293826 [patent_app_country] => US [patent_app_date] => 2002-11-12 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 37 [patent_figures_cnt] => 37 [patent_no_of_words] => 13285 [patent_no_of_claims] => 27 [patent_no_of_ind_claims] => 5 [patent_words_short_claim] => 26 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] => publications/A1/0089/20040089763.pdf [firstpage_image] =>[orig_patent_app_number] => 10293826 [rel_patent_id] =>[rel_patent_doc_number] =>)
10/293826
Personal flight vehicle and system Nov 11, 2002 Issued
Array ( [id] => 7188824 [patent_doc_number] => 20040084566 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2004-05-06 [patent_title] => 'Multi-nozzle grid missile propulsion system' [patent_app_type] => new [patent_app_number] => 10/288943 [patent_app_country] => US [patent_app_date] => 2002-11-06 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 6 [patent_figures_cnt] => 6 [patent_no_of_words] => 9158 [patent_no_of_claims] => 19 [patent_no_of_ind_claims] => 4 [patent_words_short_claim] => 39 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] => publications/A1/0084/20040084566.pdf [firstpage_image] =>[orig_patent_app_number] => 10288943 [rel_patent_id] =>[rel_patent_doc_number] =>)
10/288943
Multi-nozzle grid missile propulsion system Nov 5, 2002 Abandoned
Array ( [id] => 7147227 [patent_doc_number] => 20050023410 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2005-02-03 [patent_title] => 'Multipurpose airfoil assembly' [patent_app_type] => utility [patent_app_number] => 10/286290 [patent_app_country] => US [patent_app_date] => 2002-11-01 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 8 [patent_figures_cnt] => 8 [patent_no_of_words] => 4176 [patent_no_of_claims] => 21 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 0 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] => publications/A1/0023/20050023410.pdf [firstpage_image] =>[orig_patent_app_number] => 10286290 [rel_patent_id] =>[rel_patent_doc_number] =>)
10/286290
Multipurpose airfoil assembly Oct 31, 2002 Abandoned
Array ( [id] => 7188826 [patent_doc_number] => 20040084567 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2004-05-06 [patent_title] => 'Guided parafoil system for delivering lightweight payloads' [patent_app_type] => new [patent_app_number] => 10/284699 [patent_app_country] => US [patent_app_date] => 2002-10-30 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 7 [patent_figures_cnt] => 7 [patent_no_of_words] => 2953 [patent_no_of_claims] => 21 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 105 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] => publications/A1/0084/20040084567.pdf [firstpage_image] =>[orig_patent_app_number] => 10284699 [rel_patent_id] =>[rel_patent_doc_number] =>)
10/284699
Guided parafoil system for delivering lightweight payloads Oct 29, 2002 Issued
Array ( [id] => 1224635 [patent_doc_number] => 06695258 [patent_country] => US [patent_kind] => B1 [patent_issue_date] => 2004-02-24 [patent_title] => 'Kite device' [patent_app_type] => B1 [patent_app_number] => 10/286922 [patent_app_country] => US [patent_app_date] => 2002-10-25 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 9 [patent_figures_cnt] => 11 [patent_no_of_words] => 883 [patent_no_of_claims] => 3 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 156 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/06/695/06695258.pdf [firstpage_image] =>[orig_patent_app_number] => 10286922 [rel_patent_id] =>[rel_patent_doc_number] =>)
10/286922
Kite device Oct 24, 2002 Issued
Array ( [id] => 6854062 [patent_doc_number] => 20030127563 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2003-07-10 [patent_title] => 'Differential pressure sensing release system' [patent_app_type] => new [patent_app_number] => 10/280271 [patent_app_country] => US [patent_app_date] => 2002-10-25 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 10 [patent_figures_cnt] => 10 [patent_no_of_words] => 1727 [patent_no_of_claims] => 13 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 145 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] => publications/A1/0127/20030127563.pdf [firstpage_image] =>[orig_patent_app_number] => 10280271 [rel_patent_id] =>[rel_patent_doc_number] =>)
10/280271
Differential pressure sensing release system Oct 24, 2002 Abandoned
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