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] => 5185857 [patent_doc_number] => 20070164163 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2007-07-19 [patent_title] => 'Integral accumulator valve and ram module with seal heater' [patent_app_type] => utility [patent_app_number] => 11/335324 [patent_app_country] => US [patent_app_date] => 2006-01-19 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 4 [patent_figures_cnt] => 4 [patent_no_of_words] => 2477 [patent_no_of_claims] => 10 [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/A1/0164/20070164163.pdf [firstpage_image] =>[orig_patent_app_number] => 11335324 [rel_patent_id] =>[rel_patent_doc_number] =>)
11/335324
Integral accumulator valve and ram module with seal heater Jan 18, 2006 Abandoned
Array ( [id] => 5217187 [patent_doc_number] => 20070158498 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2007-07-12 [patent_title] => 'UAV recovery system II' [patent_app_type] => utility [patent_app_number] => 11/327616 [patent_app_country] => US [patent_app_date] => 2006-01-06 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 7 [patent_figures_cnt] => 7 [patent_no_of_words] => 3912 [patent_no_of_claims] => 20 [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/A1/0158/20070158498.pdf [firstpage_image] =>[orig_patent_app_number] => 11327616 [rel_patent_id] =>[rel_patent_doc_number] =>)
11/327616
UAV recovery system II Jan 5, 2006 Issued
Array ( [id] => 567428 [patent_doc_number] => 07451951 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2008-11-18 [patent_title] => 'Miniature airplane apparatus and method' [patent_app_type] => utility [patent_app_number] => 11/326790 [patent_app_country] => US [patent_app_date] => 2006-01-05 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 17 [patent_figures_cnt] => 25 [patent_no_of_words] => 4669 [patent_no_of_claims] => 2 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 285 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/07/451/07451951.pdf [firstpage_image] =>[orig_patent_app_number] => 11326790 [rel_patent_id] =>[rel_patent_doc_number] =>)
11/326790
Miniature airplane apparatus and method Jan 4, 2006 Issued
11/324122 Access apparatus Dec 29, 2005 Abandoned
Array ( [id] => 5674491 [patent_doc_number] => 20060179846 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2006-08-17 [patent_title] => 'Auxiliary power unit intake duct with aero-acoustic guide vanes' [patent_app_type] => utility [patent_app_number] => 11/324020 [patent_app_country] => US [patent_app_date] => 2005-12-30 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 5 [patent_figures_cnt] => 5 [patent_no_of_words] => 3201 [patent_no_of_claims] => 20 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 0 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] => publications/A1/0179/20060179846.pdf [firstpage_image] =>[orig_patent_app_number] => 11324020 [rel_patent_id] =>[rel_patent_doc_number] =>)
11/324020
Auxiliary power unit intake duct with aero-acoustic guide vanes Dec 29, 2005 Issued
Array ( [id] => 208513 [patent_doc_number] => 07624949 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2009-12-01 [patent_title] => 'Satellite provided with means for countering solar pressure' [patent_app_type] => utility [patent_app_number] => 11/319527 [patent_app_country] => US [patent_app_date] => 2005-12-29 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 2 [patent_figures_cnt] => 2 [patent_no_of_words] => 1709 [patent_no_of_claims] => 6 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 123 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/07/624/07624949.pdf [firstpage_image] =>[orig_patent_app_number] => 11319527 [rel_patent_id] =>[rel_patent_doc_number] =>)
11/319527
Satellite provided with means for countering solar pressure Dec 28, 2005 Issued
Array ( [id] => 8373937 [patent_doc_number] => 08256720 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2012-09-04 [patent_title] => 'Smart vortex generator, and aircraft, vessel, and rotary machine being equipped with the same' [patent_app_type] => utility [patent_app_number] => 12/088771 [patent_app_country] => US [patent_app_date] => 2005-12-28 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 15 [patent_figures_cnt] => 19 [patent_no_of_words] => 32903 [patent_no_of_claims] => 21 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 169 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 12088771 [rel_patent_id] =>[rel_patent_doc_number] =>)
12/088771
Smart vortex generator, and aircraft, vessel, and rotary machine being equipped with the same Dec 27, 2005 Issued
Array ( [id] => 5730091 [patent_doc_number] => 20060255205 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2006-11-16 [patent_title] => 'Small remotely controllable aircraft' [patent_app_type] => utility [patent_app_number] => 11/314316 [patent_app_country] => US [patent_app_date] => 2005-12-22 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 3 [patent_figures_cnt] => 3 [patent_no_of_words] => 1660 [patent_no_of_claims] => 13 [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/A1/0255/20060255205.pdf [firstpage_image] =>[orig_patent_app_number] => 11314316 [rel_patent_id] =>[rel_patent_doc_number] =>)
11/314316
Small remotely controllable aircraft Dec 21, 2005 Abandoned
Array ( [id] => 369075 [patent_doc_number] => 07475847 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2009-01-13 [patent_title] => 'Retractable lifting blades for aircraft' [patent_app_type] => utility [patent_app_number] => 11/317855 [patent_app_country] => US [patent_app_date] => 2005-12-22 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 20 [patent_figures_cnt] => 31 [patent_no_of_words] => 7495 [patent_no_of_claims] => 12 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 127 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/07/475/07475847.pdf [firstpage_image] =>[orig_patent_app_number] => 11317855 [rel_patent_id] =>[rel_patent_doc_number] =>)
11/317855
Retractable lifting blades for aircraft Dec 21, 2005 Issued
Array ( [id] => 219688 [patent_doc_number] => 07607617 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2009-10-27 [patent_title] => 'Wing unit, in particular spar box, for forming aerodynamically active surfaces of an aircraft, in particular airfoils, horizontal tail units or rudder units of a plane' [patent_app_type] => utility [patent_app_number] => 11/316126 [patent_app_country] => US [patent_app_date] => 2005-12-22 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 3 [patent_figures_cnt] => 3 [patent_no_of_words] => 6631 [patent_no_of_claims] => 38 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 158 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/07/607/07607617.pdf [firstpage_image] =>[orig_patent_app_number] => 11316126 [rel_patent_id] =>[rel_patent_doc_number] =>)
11/316126
Wing unit, in particular spar box, for forming aerodynamically active surfaces of an aircraft, in particular airfoils, horizontal tail units or rudder units of a plane Dec 21, 2005 Issued
Array ( [id] => 5524564 [patent_doc_number] => 20090194640 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2009-08-06 [patent_title] => 'Apparatus system and method for drag reduction' [patent_app_type] => utility [patent_app_number] => 11/314525 [patent_app_country] => US [patent_app_date] => 2005-12-22 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 13 [patent_figures_cnt] => 13 [patent_no_of_words] => 3765 [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/A1/0194/20090194640.pdf [firstpage_image] =>[orig_patent_app_number] => 11314525 [rel_patent_id] =>[rel_patent_doc_number] =>)
11/314525
Apparatus system and method for drag reduction Dec 21, 2005 Issued
Array ( [id] => 5664494 [patent_doc_number] => 20060169844 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2006-08-03 [patent_title] => 'Coating for prevention of electrostatic discharge within an equipment in a spatial environment' [patent_app_type] => utility [patent_app_number] => 11/312564 [patent_app_country] => US [patent_app_date] => 2005-12-21 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 3 [patent_figures_cnt] => 3 [patent_no_of_words] => 2221 [patent_no_of_claims] => 8 [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/A1/0169/20060169844.pdf [firstpage_image] =>[orig_patent_app_number] => 11312564 [rel_patent_id] =>[rel_patent_doc_number] =>)
11/312564
Coating for prevention of electrostatic discharge within an equipment in a spatial environment Dec 20, 2005 Issued
Array ( [id] => 4782348 [patent_doc_number] => 20080135677 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2008-06-12 [patent_title] => 'Reaction-drive rotorcraft having an adjustable blade jet' [patent_app_type] => utility [patent_app_number] => 11/313044 [patent_app_country] => US [patent_app_date] => 2005-12-20 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 5 [patent_figures_cnt] => 5 [patent_no_of_words] => 4514 [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/A1/0135/20080135677.pdf [firstpage_image] =>[orig_patent_app_number] => 11313044 [rel_patent_id] =>[rel_patent_doc_number] =>)
11/313044
Reaction-drive rotorcraft having an adjustable blade jet Dec 19, 2005 Issued
Array ( [id] => 224018 [patent_doc_number] => 07604199 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2009-10-20 [patent_title] => 'Aerofoil containment structure' [patent_app_type] => utility [patent_app_number] => 11/305206 [patent_app_country] => US [patent_app_date] => 2005-12-19 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 4 [patent_figures_cnt] => 11 [patent_no_of_words] => 3516 [patent_no_of_claims] => 27 [patent_no_of_ind_claims] => 7 [patent_words_short_claim] => 72 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/07/604/07604199.pdf [firstpage_image] =>[orig_patent_app_number] => 11305206 [rel_patent_id] =>[rel_patent_doc_number] =>)
11/305206
Aerofoil containment structure Dec 18, 2005 Issued
Array ( [id] => 5664911 [patent_doc_number] => 20060170261 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2006-08-03 [patent_title] => 'Passenger seat unit, in particular for commercial aircraft' [patent_app_type] => utility [patent_app_number] => 11/311858 [patent_app_country] => US [patent_app_date] => 2005-12-19 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 4 [patent_figures_cnt] => 4 [patent_no_of_words] => 2419 [patent_no_of_claims] => 14 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 0 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] => publications/A1/0170/20060170261.pdf [firstpage_image] =>[orig_patent_app_number] => 11311858 [rel_patent_id] =>[rel_patent_doc_number] =>)
11/311858
Passenger seat unit, in particular for commercial aircraft Dec 18, 2005 Issued
Array ( [id] => 255528 [patent_doc_number] => 07575192 [patent_country] => US [patent_kind] => B1 [patent_issue_date] => 2009-08-18 [patent_title] => 'Transmission system for use in microturbine-powered applications' [patent_app_type] => utility [patent_app_number] => 11/305711 [patent_app_country] => US [patent_app_date] => 2005-12-16 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 9 [patent_figures_cnt] => 17 [patent_no_of_words] => 7079 [patent_no_of_claims] => 28 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 204 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/07/575/07575192.pdf [firstpage_image] =>[orig_patent_app_number] => 11305711 [rel_patent_id] =>[rel_patent_doc_number] =>)
11/305711
Transmission system for use in microturbine-powered applications Dec 15, 2005 Issued
Array ( [id] => 5854347 [patent_doc_number] => 20060226280 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2006-10-12 [patent_title] => 'Stowable design for unmanned aerial vehicle' [patent_app_type] => utility [patent_app_number] => 11/305524 [patent_app_country] => US [patent_app_date] => 2005-12-16 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 4 [patent_figures_cnt] => 4 [patent_no_of_words] => 1724 [patent_no_of_claims] => 17 [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/A1/0226/20060226280.pdf [firstpage_image] =>[orig_patent_app_number] => 11305524 [rel_patent_id] =>[rel_patent_doc_number] =>)
11/305524
Stowable design for unmanned aerial vehicle Dec 15, 2005 Abandoned
Array ( [id] => 231863 [patent_doc_number] => 07597286 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2009-10-06 [patent_title] => 'Simplified power system for a cabin services system for an aircraft' [patent_app_type] => utility [patent_app_number] => 11/303498 [patent_app_country] => US [patent_app_date] => 2005-12-16 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 12 [patent_figures_cnt] => 12 [patent_no_of_words] => 5836 [patent_no_of_claims] => 19 [patent_no_of_ind_claims] => 6 [patent_words_short_claim] => 90 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/07/597/07597286.pdf [firstpage_image] =>[orig_patent_app_number] => 11303498 [rel_patent_id] =>[rel_patent_doc_number] =>)
11/303498
Simplified power system for a cabin services system for an aircraft Dec 15, 2005 Issued
Array ( [id] => 5652548 [patent_doc_number] => 20060138283 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2006-06-29 [patent_title] => 'Apparatus with helical tension cables for ejecting a spin-stabilized body from a spacecraft' [patent_app_type] => utility [patent_app_number] => 11/305430 [patent_app_country] => US [patent_app_date] => 2005-12-15 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 4 [patent_figures_cnt] => 4 [patent_no_of_words] => 4361 [patent_no_of_claims] => 19 [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/A1/0138/20060138283.pdf [firstpage_image] =>[orig_patent_app_number] => 11305430 [rel_patent_id] =>[rel_patent_doc_number] =>)
11/305430
Apparatus with helical tension cables for ejecting a spin-stabilized body from a spacecraft Dec 14, 2005 Issued
Array ( [id] => 573517 [patent_doc_number] => 07445183 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2008-11-04 [patent_title] => 'Apparatus with axis-parallel tension cables for ejecting a spin-stabilized body from a spacecraft' [patent_app_type] => utility [patent_app_number] => 11/305429 [patent_app_country] => US [patent_app_date] => 2005-12-15 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 3 [patent_figures_cnt] => 6 [patent_no_of_words] => 4392 [patent_no_of_claims] => 20 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 202 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/07/445/07445183.pdf [firstpage_image] =>[orig_patent_app_number] => 11305429 [rel_patent_id] =>[rel_patent_doc_number] =>)
11/305429
Apparatus with axis-parallel tension cables for ejecting a spin-stabilized body from a spacecraft Dec 14, 2005 Issued
Menu