
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 number | Title of the application | Filing Date | Status |
|---|---|---|---|
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
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[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
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[patent_no_of_words] => 873
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[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
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[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
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[patent_no_of_words] => 976
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[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
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[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
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[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
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[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 |