
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] => 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
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[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
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[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
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[patent_no_of_words] => 4514
[patent_no_of_claims] => 21
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[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
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[patent_no_of_words] => 3516
[patent_no_of_claims] => 27
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[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
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[patent_no_of_words] => 2419
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[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
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[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
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[patent_no_of_words] => 1724
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[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
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[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
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[patent_issue_date] => 2006-06-29
[patent_title] => 'Apparatus with helical tension cables for ejecting a spin-stabilized body from a spacecraft'
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[patent_app_number] => 11/305430
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[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
(
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[patent_doc_number] => 07445183
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[patent_title] => 'Apparatus with axis-parallel tension cables for ejecting a spin-stabilized body from a spacecraft'
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[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 |