
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] => 189842
[patent_doc_number] => 07641150
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2010-01-05
[patent_title] => 'Solid propellant-based space propulsion device'
[patent_app_type] => utility
[patent_app_number] => 11/435521
[patent_app_country] => US
[patent_app_date] => 2006-05-16
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
[patent_figures_cnt] => 5
[patent_no_of_words] => 13774
[patent_no_of_claims] => 7
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 286
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/07/641/07641150.pdf
[firstpage_image] =>[orig_patent_app_number] => 11435521
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/435521 | Solid propellant-based space propulsion device | May 15, 2006 | Issued |
Array
(
[id] => 5392792
[patent_doc_number] => 20090210105
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2009-08-20
[patent_title] => 'AIR-GROUND DETECTION SYSTEM AND METHOD'
[patent_app_type] => utility
[patent_app_number] => 11/383263
[patent_app_country] => US
[patent_app_date] => 2006-05-15
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 10
[patent_figures_cnt] => 10
[patent_no_of_words] => 8758
[patent_no_of_claims] => 37
[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/A1/0210/20090210105.pdf
[firstpage_image] =>[orig_patent_app_number] => 11383263
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/383263 | AIR-GROUND DETECTION SYSTEM AND METHOD | May 14, 2006 | Abandoned |
Array
(
[id] => 5104232
[patent_doc_number] => 20070063107
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2007-03-22
[patent_title] => 'REUSABLE ORBITAL VEHICLE WITH INTERCHANGEABLE CARGO MODULES'
[patent_app_type] => utility
[patent_app_number] => 11/382557
[patent_app_country] => US
[patent_app_date] => 2006-05-10
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 19
[patent_figures_cnt] => 19
[patent_no_of_words] => 7192
[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/A1/0063/20070063107.pdf
[firstpage_image] =>[orig_patent_app_number] => 11382557
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/382557 | REUSABLE ORBITAL VEHICLE WITH INTERCHANGEABLE CARGO MODULES | May 9, 2006 | Abandoned |
Array
(
[id] => 4531899
[patent_doc_number] => 07874525
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2011-01-25
[patent_title] => 'Method and system for fully fixed vehicle control surfaces'
[patent_app_type] => utility
[patent_app_number] => 11/417417
[patent_app_country] => US
[patent_app_date] => 2006-05-04
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 13
[patent_figures_cnt] => 17
[patent_no_of_words] => 4740
[patent_no_of_claims] => 11
[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/07/874/07874525.pdf
[firstpage_image] =>[orig_patent_app_number] => 11417417
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/417417 | Method and system for fully fixed vehicle control surfaces | May 3, 2006 | Issued |
Array
(
[id] => 8211255
[patent_doc_number] => 08191833
[patent_country] => US
[patent_kind] => B1
[patent_issue_date] => 2012-06-05
[patent_title] => 'Aircraft and missile afterbody flow control device and method of controlling flow'
[patent_app_type] => utility
[patent_app_number] => 11/415534
[patent_app_country] => US
[patent_app_date] => 2006-05-02
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
[patent_figures_cnt] => 8
[patent_no_of_words] => 5787
[patent_no_of_claims] => 17
[patent_no_of_ind_claims] => 4
[patent_words_short_claim] => 47
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/08/191/08191833.pdf
[firstpage_image] =>[orig_patent_app_number] => 11415534
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/415534 | Aircraft and missile afterbody flow control device and method of controlling flow | May 1, 2006 | Issued |
Array
(
[id] => 4489950
[patent_doc_number] => 07946528
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2011-05-24
[patent_title] => 'Flight control system especially suited for VTOL vehicles'
[patent_app_type] => utility
[patent_app_number] => 11/405003
[patent_app_country] => US
[patent_app_date] => 2006-04-17
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 27
[patent_figures_cnt] => 57
[patent_no_of_words] => 13300
[patent_no_of_claims] => 18
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 256
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/07/946/07946528.pdf
[firstpage_image] =>[orig_patent_app_number] => 11405003
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/405003 | Flight control system especially suited for VTOL vehicles | Apr 16, 2006 | Issued |
Array
(
[id] => 4843057
[patent_doc_number] => 20080179465
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2008-07-31
[patent_title] => 'Aircraft With Low Noise, Such as During Take-Off and Landing'
[patent_app_type] => utility
[patent_app_number] => 11/911604
[patent_app_country] => US
[patent_app_date] => 2006-04-11
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 2
[patent_figures_cnt] => 2
[patent_no_of_words] => 1037
[patent_no_of_claims] => 1
[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/A1/0179/20080179465.pdf
[firstpage_image] =>[orig_patent_app_number] => 11911604
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/911604 | Aircraft With Low Noise, Such as During Take-Off and Landing | Apr 10, 2006 | Abandoned |
Array
(
[id] => 4516348
[patent_doc_number] => 07950607
[patent_country] => US
[patent_kind] => B1
[patent_issue_date] => 2011-05-31
[patent_title] => 'Small munitions adaptor rack for releasing small munitions from an aircraft'
[patent_app_type] => utility
[patent_app_number] => 11/401526
[patent_app_country] => US
[patent_app_date] => 2006-04-10
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 6
[patent_no_of_words] => 2110
[patent_no_of_claims] => 10
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 201
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/07/950/07950607.pdf
[firstpage_image] =>[orig_patent_app_number] => 11401526
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/401526 | Small munitions adaptor rack for releasing small munitions from an aircraft | Apr 9, 2006 | Issued |
Array
(
[id] => 5299930
[patent_doc_number] => 20090294582
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2009-12-03
[patent_title] => 'Propulsion Unit for Lighter-Than-Air Aircraft'
[patent_app_type] => utility
[patent_app_number] => 11/918333
[patent_app_country] => US
[patent_app_date] => 2006-04-07
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 4
[patent_no_of_words] => 1988
[patent_no_of_claims] => 6
[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/A1/0294/20090294582.pdf
[firstpage_image] =>[orig_patent_app_number] => 11918333
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/918333 | Propulsion Unit for Lighter-Than-Air Aircraft | Apr 6, 2006 | Abandoned |
Array
(
[id] => 5123319
[patent_doc_number] => 20070235589
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2007-10-11
[patent_title] => 'Atmospheric ionizer for space rockets'
[patent_app_type] => utility
[patent_app_number] => 11/398410
[patent_app_country] => US
[patent_app_date] => 2006-04-05
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 2
[patent_figures_cnt] => 2
[patent_no_of_words] => 263
[patent_no_of_claims] => 2
[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/A1/0235/20070235589.pdf
[firstpage_image] =>[orig_patent_app_number] => 11398410
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/398410 | Atmospheric ionizer for space rockets | Apr 4, 2006 | Abandoned |
Array
(
[id] => 5750689
[patent_doc_number] => 20060219838
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2006-10-05
[patent_title] => 'Attachment means for hang glider simulator'
[patent_app_type] => utility
[patent_app_number] => 11/389727
[patent_app_country] => US
[patent_app_date] => 2006-03-27
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 7
[patent_figures_cnt] => 7
[patent_no_of_words] => 1701
[patent_no_of_claims] => 7
[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/A1/0219/20060219838.pdf
[firstpage_image] =>[orig_patent_app_number] => 11389727
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/389727 | Attachment means for hang glider simulator | Mar 26, 2006 | Abandoned |
Array
(
[id] => 5469523
[patent_doc_number] => 20090242689
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2009-10-01
[patent_title] => 'CRAFT HAVING A ROTATABLE FLUID PROPULSION DEVICE'
[patent_app_type] => utility
[patent_app_number] => 11/909507
[patent_app_country] => US
[patent_app_date] => 2006-03-23
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 6
[patent_figures_cnt] => 6
[patent_no_of_words] => 2420
[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/A1/0242/20090242689.pdf
[firstpage_image] =>[orig_patent_app_number] => 11909507
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/909507 | Craft having a rotatable fluid propulsion device | Mar 22, 2006 | Issued |
Array
(
[id] => 4810470
[patent_doc_number] => 20080191101
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2008-08-14
[patent_title] => 'Aerofoil Surface for Controlling Spin'
[patent_app_type] => utility
[patent_app_number] => 11/909500
[patent_app_country] => US
[patent_app_date] => 2006-03-23
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 2
[patent_figures_cnt] => 2
[patent_no_of_words] => 1871
[patent_no_of_claims] => 10
[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/A1/0191/20080191101.pdf
[firstpage_image] =>[orig_patent_app_number] => 11909500
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/909500 | Aerofoil Surface for Controlling Spin | Mar 22, 2006 | Abandoned |
Array
(
[id] => 5593701
[patent_doc_number] => 20060157617
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2006-07-20
[patent_title] => 'Airship having a multiple-lobed hull'
[patent_app_type] => utility
[patent_app_number] => 11/384348
[patent_app_country] => US
[patent_app_date] => 2006-03-21
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 10
[patent_figures_cnt] => 10
[patent_no_of_words] => 5136
[patent_no_of_claims] => 3
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[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0157/20060157617.pdf
[firstpage_image] =>[orig_patent_app_number] => 11384348
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/384348 | Airship having a multiple-lobed hull | Mar 20, 2006 | Abandoned |
Array
(
[id] => 5048904
[patent_doc_number] => 20070029448
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2007-02-08
[patent_title] => 'Method of traveling to earth\'s orbit using lighter than air vehicles'
[patent_app_type] => utility
[patent_app_number] => 11/372525
[patent_app_country] => US
[patent_app_date] => 2006-03-10
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
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[patent_no_of_words] => 1947
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[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0029/20070029448.pdf
[firstpage_image] =>[orig_patent_app_number] => 11372525
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/372525 | Method of traveling to Earth's orbit using lighter than air vehicles | Mar 9, 2006 | Issued |
Array
(
[id] => 100132
[patent_doc_number] => 07721989
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2010-05-25
[patent_title] => 'Multi-path inlet for aircraft engine'
[patent_app_type] => utility
[patent_app_number] => 11/365900
[patent_app_country] => US
[patent_app_date] => 2006-03-01
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 7
[patent_figures_cnt] => 10
[patent_no_of_words] => 3573
[patent_no_of_claims] => 19
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 135
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/07/721/07721989.pdf
[firstpage_image] =>[orig_patent_app_number] => 11365900
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/365900 | Multi-path inlet for aircraft engine | Feb 28, 2006 | Issued |
Array
(
[id] => 502885
[patent_doc_number] => 07198229
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2007-04-03
[patent_title] => 'In-flight refueling system, damping device and method for damping oscillations in in-flight refueling system components'
[patent_app_type] => utility
[patent_app_number] => 11/353276
[patent_app_country] => US
[patent_app_date] => 2006-02-13
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 6
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[patent_no_of_words] => 7763
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[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/07/198/07198229.pdf
[firstpage_image] =>[orig_patent_app_number] => 11353276
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/353276 | In-flight refueling system, damping device and method for damping oscillations in in-flight refueling system components | Feb 12, 2006 | Issued |
Array
(
[id] => 110328
[patent_doc_number] => 07712701
[patent_country] => US
[patent_kind] => B1
[patent_issue_date] => 2010-05-11
[patent_title] => 'Unmanned aerial vehicle with electrically powered, counterrotating ducted rotors'
[patent_app_type] => utility
[patent_app_number] => 11/351775
[patent_app_country] => US
[patent_app_date] => 2006-02-10
[patent_effective_date] => 0000-00-00
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[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/07/712/07712701.pdf
[firstpage_image] =>[orig_patent_app_number] => 11351775
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/351775 | Unmanned aerial vehicle with electrically powered, counterrotating ducted rotors | Feb 9, 2006 | Issued |
Array
(
[id] => 4890521
[patent_doc_number] => 20080099617
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2008-05-01
[patent_title] => 'Ice Protection of Aerodynamic Surfaces'
[patent_app_type] => utility
[patent_app_number] => 11/883102
[patent_app_country] => US
[patent_app_date] => 2006-02-03
[patent_effective_date] => 0000-00-00
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[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0099/20080099617.pdf
[firstpage_image] =>[orig_patent_app_number] => 11883102
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/883102 | Ice protection of aerodynamic surfaces | Feb 2, 2006 | Issued |
Array
(
[id] => 5685692
[patent_doc_number] => 20060284007
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2006-12-21
[patent_title] => 'Propeller guard for aircraft'
[patent_app_type] => utility
[patent_app_number] => 11/338027
[patent_app_country] => US
[patent_app_date] => 2006-01-24
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 9
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[patent_no_of_words] => 2790
[patent_no_of_claims] => 20
[patent_no_of_ind_claims] => 3
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[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0284/20060284007.pdf
[firstpage_image] =>[orig_patent_app_number] => 11338027
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/338027 | Propeller guard for aircraft | Jan 23, 2006 | Abandoned |