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] => 5707971 [patent_doc_number] => 20060049315 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2006-03-09 [patent_title] => 'Precision attitude control system for gimaled thruster' [patent_app_type] => utility [patent_app_number] => 10/522576 [patent_app_country] => US [patent_app_date] => 2004-10-14 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 9 [patent_figures_cnt] => 9 [patent_no_of_words] => 3108 [patent_no_of_claims] => 24 [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/A1/0049/20060049315.pdf [firstpage_image] =>[orig_patent_app_number] => 10522576 [rel_patent_id] =>[rel_patent_doc_number] =>)
10/522576
Precision attitude control system for gimbaled thruster Oct 13, 2004 Issued
Array ( [id] => 6936315 [patent_doc_number] => 20050109876 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2005-05-26 [patent_title] => 'Aircraft control surface drive system and associated methods' [patent_app_type] => utility [patent_app_number] => 10/959629 [patent_app_country] => US [patent_app_date] => 2004-10-05 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 5 [patent_figures_cnt] => 5 [patent_no_of_words] => 5398 [patent_no_of_claims] => 15 [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/A1/0109/20050109876.pdf [firstpage_image] =>[orig_patent_app_number] => 10959629 [rel_patent_id] =>[rel_patent_doc_number] =>)
10/959629
Aircraft control surface drive system and associated methods Oct 4, 2004 Issued
Array ( [id] => 5823515 [patent_doc_number] => 20060060697 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2006-03-23 [patent_title] => 'Device for assembly of a shroud placed between an aircraft engine air intake and a pylon' [patent_app_type] => utility [patent_app_number] => 10/954192 [patent_app_country] => US [patent_app_date] => 2004-10-01 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 6 [patent_figures_cnt] => 6 [patent_no_of_words] => 5161 [patent_no_of_claims] => 11 [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/A1/0060/20060060697.pdf [firstpage_image] =>[orig_patent_app_number] => 10954192 [rel_patent_id] =>[rel_patent_doc_number] =>)
10/954192
Device for assembly of a shroud placed between an aircraft engine air intake and a pylon Sep 30, 2004 Issued
Array ( [id] => 848240 [patent_doc_number] => 07380754 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2008-06-03 [patent_title] => 'Clamp block assemblies and methods' [patent_app_type] => utility [patent_app_number] => 10/956001 [patent_app_country] => US [patent_app_date] => 2004-09-30 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 2 [patent_figures_cnt] => 6 [patent_no_of_words] => 1404 [patent_no_of_claims] => 11 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 210 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/07/380/07380754.pdf [firstpage_image] =>[orig_patent_app_number] => 10956001 [rel_patent_id] =>[rel_patent_doc_number] =>)
10/956001
Clamp block assemblies and methods Sep 29, 2004 Issued
Array ( [id] => 5634805 [patent_doc_number] => 20060065778 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2006-03-30 [patent_title] => 'Actuator with helical cam guides' [patent_app_type] => utility [patent_app_number] => 10/953230 [patent_app_country] => US [patent_app_date] => 2004-09-29 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 7 [patent_figures_cnt] => 7 [patent_no_of_words] => 2429 [patent_no_of_claims] => 9 [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/A1/0065/20060065778.pdf [firstpage_image] =>[orig_patent_app_number] => 10953230 [rel_patent_id] =>[rel_patent_doc_number] =>)
10/953230
Actuator with helical cam guides Sep 28, 2004 Issued
Array ( [id] => 89754 [patent_doc_number] => 07731121 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2010-06-08 [patent_title] => 'Propulsive anti-torque system for rotorcraft' [patent_app_type] => utility [patent_app_number] => 11/662559 [patent_app_country] => US [patent_app_date] => 2004-09-28 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 5 [patent_figures_cnt] => 8 [patent_no_of_words] => 3496 [patent_no_of_claims] => 15 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 167 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/07/731/07731121.pdf [firstpage_image] =>[orig_patent_app_number] => 11662559 [rel_patent_id] =>[rel_patent_doc_number] =>)
11/662559
Propulsive anti-torque system for rotorcraft Sep 27, 2004 Issued
Array ( [id] => 5823521 [patent_doc_number] => 20060060703 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2006-03-23 [patent_title] => 'Three dimensional seating arrangement to increase seating capacity' [patent_app_type] => utility [patent_app_number] => 10/948419 [patent_app_country] => US [patent_app_date] => 2004-09-22 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 3 [patent_figures_cnt] => 3 [patent_no_of_words] => 1283 [patent_no_of_claims] => 17 [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/A1/0060/20060060703.pdf [firstpage_image] =>[orig_patent_app_number] => 10948419 [rel_patent_id] =>[rel_patent_doc_number] =>)
10/948419
Three dimensional seating arrangement to increase seating capacity Sep 21, 2004 Abandoned
Array ( [id] => 6955475 [patent_doc_number] => 20050211845 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2005-09-29 [patent_title] => 'Airship having a multiple-lobed hull' [patent_app_type] => utility [patent_app_number] => 10/944905 [patent_app_country] => US [patent_app_date] => 2004-09-21 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 10 [patent_figures_cnt] => 10 [patent_no_of_words] => 5139 [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/A1/0211/20050211845.pdf [firstpage_image] =>[orig_patent_app_number] => 10944905 [rel_patent_id] =>[rel_patent_doc_number] =>)
10/944905
Airship having a multiple-lobed hull Sep 20, 2004 Abandoned
Array ( [id] => 7008194 [patent_doc_number] => 20050061910 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2005-03-24 [patent_title] => 'Aircraft' [patent_app_type] => utility [patent_app_number] => 10/934634 [patent_app_country] => US [patent_app_date] => 2004-09-03 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 3 [patent_figures_cnt] => 3 [patent_no_of_words] => 2365 [patent_no_of_claims] => 37 [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/A1/0061/20050061910.pdf [firstpage_image] =>[orig_patent_app_number] => 10934634 [rel_patent_id] =>[rel_patent_doc_number] =>)
10/934634
Aircraft Sep 2, 2004 Issued
Array ( [id] => 5898005 [patent_doc_number] => 20060043238 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2006-03-02 [patent_title] => 'Modular design with built-in upgradeability for aerospace applications' [patent_app_type] => utility [patent_app_number] => 10/930626 [patent_app_country] => US [patent_app_date] => 2004-08-31 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 6 [patent_figures_cnt] => 6 [patent_no_of_words] => 2418 [patent_no_of_claims] => 33 [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/A1/0043/20060043238.pdf [firstpage_image] =>[orig_patent_app_number] => 10930626 [rel_patent_id] =>[rel_patent_doc_number] =>)
10/930626
Modular design with built-in upgradeability for aerospace applications Aug 30, 2004 Abandoned
Array ( [id] => 4520913 [patent_doc_number] => 07922117 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2011-04-12 [patent_title] => 'Primary panel and motor controller integration for aircraft power distribution system' [patent_app_type] => utility [patent_app_number] => 10/929318 [patent_app_country] => US [patent_app_date] => 2004-08-30 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 3 [patent_figures_cnt] => 3 [patent_no_of_words] => 2183 [patent_no_of_claims] => 19 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 32 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/07/922/07922117.pdf [firstpage_image] =>[orig_patent_app_number] => 10929318 [rel_patent_id] =>[rel_patent_doc_number] =>)
10/929318
Primary panel and motor controller integration for aircraft power distribution system Aug 29, 2004 Issued
Array ( [id] => 7187450 [patent_doc_number] => 20050039557 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2005-02-24 [patent_title] => 'Linear actuation device for spacecraft and solar generator unfolding systems' [patent_app_type] => utility [patent_app_number] => 10/928405 [patent_app_country] => US [patent_app_date] => 2004-08-30 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 5 [patent_figures_cnt] => 5 [patent_no_of_words] => 3484 [patent_no_of_claims] => 36 [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/A1/0039/20050039557.pdf [firstpage_image] =>[orig_patent_app_number] => 10928405 [rel_patent_id] =>[rel_patent_doc_number] =>)
10/928405
Linear actuation device for spacecraft and solar generator unfolding systems Aug 29, 2004 Issued
Array ( [id] => 5823527 [patent_doc_number] => 20060060709 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2006-03-23 [patent_title] => 'In-flight refueling system, sensor system and method for damping oscillations in in-flight refueling system components' [patent_app_type] => utility [patent_app_number] => 10/927217 [patent_app_country] => US [patent_app_date] => 2004-08-26 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 5 [patent_figures_cnt] => 5 [patent_no_of_words] => 6509 [patent_no_of_claims] => 26 [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/A1/0060/20060060709.pdf [firstpage_image] =>[orig_patent_app_number] => 10927217 [rel_patent_id] =>[rel_patent_doc_number] =>)
10/927217
In-flight refueling system, sensor system and method for damping oscillations in in-flight refueling system components Aug 25, 2004 Issued
Array ( [id] => 5823532 [patent_doc_number] => 20060060714 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2006-03-23 [patent_title] => 'Aircraft store ejector rack systems and methods' [patent_app_type] => utility [patent_app_number] => 10/926630 [patent_app_country] => US [patent_app_date] => 2004-08-26 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 9 [patent_figures_cnt] => 9 [patent_no_of_words] => 2753 [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/A1/0060/20060060714.pdf [firstpage_image] =>[orig_patent_app_number] => 10926630 [rel_patent_id] =>[rel_patent_doc_number] =>)
10/926630
Aircraft store ejector rack systems and methods Aug 25, 2004 Issued
Array ( [id] => 5588607 [patent_doc_number] => 20060038058 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2006-02-23 [patent_title] => 'Active control of airfoils' [patent_app_type] => utility [patent_app_number] => 10/925382 [patent_app_country] => US [patent_app_date] => 2004-08-23 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 3 [patent_figures_cnt] => 3 [patent_no_of_words] => 873 [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/A1/0038/20060038058.pdf [firstpage_image] =>[orig_patent_app_number] => 10925382 [rel_patent_id] =>[rel_patent_doc_number] =>)
10/925382
Active control of airfoils Aug 22, 2004 Abandoned
Array ( [id] => 7240929 [patent_doc_number] => 20050072878 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2005-04-07 [patent_title] => 'Luggage bins and aircraft passenger cabin ceilings' [patent_app_type] => utility [patent_app_number] => 10/922113 [patent_app_country] => US [patent_app_date] => 2004-08-19 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 8 [patent_figures_cnt] => 8 [patent_no_of_words] => 5179 [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/A1/0072/20050072878.pdf [firstpage_image] =>[orig_patent_app_number] => 10922113 [rel_patent_id] =>[rel_patent_doc_number] =>)
10/922113
Luggage bins and aircraft passenger cabin ceilings Aug 18, 2004 Issued
Array ( [id] => 615094 [patent_doc_number] => 07143978 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2006-12-05 [patent_title] => 'In-seat power supply floor module' [patent_app_type] => utility [patent_app_number] => 10/921124 [patent_app_country] => US [patent_app_date] => 2004-08-19 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 2 [patent_figures_cnt] => 2 [patent_no_of_words] => 976 [patent_no_of_claims] => 8 [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/07/143/07143978.pdf [firstpage_image] =>[orig_patent_app_number] => 10921124 [rel_patent_id] =>[rel_patent_doc_number] =>)
10/921124
In-seat power supply floor module Aug 18, 2004 Issued
Array ( [id] => 194996 [patent_doc_number] => 07637459 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2009-12-29 [patent_title] => 'Weight-on-gear sensor' [patent_app_type] => utility [patent_app_number] => 11/659748 [patent_app_country] => US [patent_app_date] => 2004-08-10 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 2 [patent_figures_cnt] => 9 [patent_no_of_words] => 3284 [patent_no_of_claims] => 6 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 115 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/07/637/07637459.pdf [firstpage_image] =>[orig_patent_app_number] => 11659748 [rel_patent_id] =>[rel_patent_doc_number] =>)
11/659748
Weight-on-gear sensor Aug 9, 2004 Issued
Array ( [id] => 7086416 [patent_doc_number] => 20050006528 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2005-01-13 [patent_title] => 'Integrated cockpit door lock and access system' [patent_app_type] => utility [patent_app_number] => 10/911842 [patent_app_country] => US [patent_app_date] => 2004-08-05 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 11 [patent_figures_cnt] => 11 [patent_no_of_words] => 5788 [patent_no_of_claims] => 21 [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/A1/0006/20050006528.pdf [firstpage_image] =>[orig_patent_app_number] => 10911842 [rel_patent_id] =>[rel_patent_doc_number] =>)
10/911842
Integrated cockpit door lock and access system Aug 4, 2004 Abandoned
Array ( [id] => 7008203 [patent_doc_number] => 20050061919 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2005-03-24 [patent_title] => 'Method for use of external secondary payloads' [patent_app_type] => utility [patent_app_number] => 10/913094 [patent_app_country] => US [patent_app_date] => 2004-08-05 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 8 [patent_figures_cnt] => 8 [patent_no_of_words] => 9630 [patent_no_of_claims] => 34 [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/A1/0061/20050061919.pdf [firstpage_image] =>[orig_patent_app_number] => 10913094 [rel_patent_id] =>[rel_patent_doc_number] =>)
10/913094
Method for use of external secondary payloads Aug 4, 2004 Abandoned
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