
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] => 306467
[patent_doc_number] => 07530530
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2009-05-12
[patent_title] => 'Assembly for securing a stringer to a substrate'
[patent_app_type] => utility
[patent_app_number] => 11/850882
[patent_app_country] => US
[patent_app_date] => 2007-09-06
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
[patent_figures_cnt] => 5
[patent_no_of_words] => 3797
[patent_no_of_claims] => 20
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 77
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/07/530/07530530.pdf
[firstpage_image] =>[orig_patent_app_number] => 11850882
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/850882 | Assembly for securing a stringer to a substrate | Sep 5, 2007 | Issued |
Array
(
[id] => 4540353
[patent_doc_number] => 07819359
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2010-10-26
[patent_title] => 'Aircraft firewall'
[patent_app_type] => utility
[patent_app_number] => 11/896812
[patent_app_country] => US
[patent_app_date] => 2007-09-06
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 1
[patent_figures_cnt] => 1
[patent_no_of_words] => 2059
[patent_no_of_claims] => 14
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 120
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/07/819/07819359.pdf
[firstpage_image] =>[orig_patent_app_number] => 11896812
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/896812 | Aircraft firewall | Sep 5, 2007 | Issued |
Array
(
[id] => 4643208
[patent_doc_number] => 08020808
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2011-09-20
[patent_title] => 'Aircraft subassembly and aircraft comprising such a subassembly'
[patent_app_type] => utility
[patent_app_number] => 11/848367
[patent_app_country] => US
[patent_app_date] => 2007-08-31
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 7
[patent_no_of_words] => 5366
[patent_no_of_claims] => 20
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 168
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/08/020/08020808.pdf
[firstpage_image] =>[orig_patent_app_number] => 11848367
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/848367 | Aircraft subassembly and aircraft comprising such a subassembly | Aug 30, 2007 | Issued |
Array
(
[id] => 4638210
[patent_doc_number] => 08016235
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2011-09-13
[patent_title] => 'Cover for an aircraft access opening'
[patent_app_type] => utility
[patent_app_number] => 11/897007
[patent_app_country] => US
[patent_app_date] => 2007-08-28
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 11
[patent_no_of_words] => 1774
[patent_no_of_claims] => 6
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 105
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/08/016/08016235.pdf
[firstpage_image] =>[orig_patent_app_number] => 11897007
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/897007 | Cover for an aircraft access opening | Aug 27, 2007 | Issued |
Array
(
[id] => 202727
[patent_doc_number] => 07628355
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2009-12-08
[patent_title] => 'Variable speed transmission for a rotary wing aircraft'
[patent_app_type] => utility
[patent_app_number] => 11/845181
[patent_app_country] => US
[patent_app_date] => 2007-08-27
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
[patent_figures_cnt] => 6
[patent_no_of_words] => 3339
[patent_no_of_claims] => 24
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 129
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/07/628/07628355.pdf
[firstpage_image] =>[orig_patent_app_number] => 11845181
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/845181 | Variable speed transmission for a rotary wing aircraft | Aug 26, 2007 | Issued |
Array
(
[id] => 4756454
[patent_doc_number] => 20080308679
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2008-12-18
[patent_title] => 'Device to reduce the lateral force generated by aerial refueling boom cross-section'
[patent_app_type] => utility
[patent_app_number] => 11/893107
[patent_app_country] => US
[patent_app_date] => 2007-08-14
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 7
[patent_figures_cnt] => 7
[patent_no_of_words] => 2241
[patent_no_of_claims] => 15
[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/A1/0308/20080308679.pdf
[firstpage_image] =>[orig_patent_app_number] => 11893107
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/893107 | Device to reduce the lateral force generated by aerial refueling boom cross-section | Aug 13, 2007 | Issued |
Array
(
[id] => 5413317
[patent_doc_number] => 20090039204
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2009-02-12
[patent_title] => 'Wingtip Feathers, Including Forward Swept Feathers, and Associated Aircraft Systems and Methods'
[patent_app_type] => utility
[patent_app_number] => 11/836414
[patent_app_country] => US
[patent_app_date] => 2007-08-09
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 4
[patent_no_of_words] => 3830
[patent_no_of_claims] => 25
[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/A1/0039/20090039204.pdf
[firstpage_image] =>[orig_patent_app_number] => 11836414
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/836414 | Wingtip feathers, including forward swept feathers, and associated aircraft systems and methods | Aug 8, 2007 | Issued |
Array
(
[id] => 8111991
[patent_doc_number] => 08157207
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2012-04-17
[patent_title] => 'Jet engine nozzle exit configurations, including projections oriented relative to pylons, and associated systems and methods'
[patent_app_type] => utility
[patent_app_number] => 11/836517
[patent_app_country] => US
[patent_app_date] => 2007-08-09
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 10
[patent_figures_cnt] => 26
[patent_no_of_words] => 8590
[patent_no_of_claims] => 22
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 195
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/08/157/08157207.pdf
[firstpage_image] =>[orig_patent_app_number] => 11836517
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/836517 | Jet engine nozzle exit configurations, including projections oriented relative to pylons, and associated systems and methods | Aug 8, 2007 | Issued |
Array
(
[id] => 100145
[patent_doc_number] => 07721997
[patent_country] => US
[patent_kind] => B1
[patent_issue_date] => 2010-05-25
[patent_title] => 'Method and system for providing cruciform steered, bent biconic and plasma suppression for maximum accuracy'
[patent_app_type] => utility
[patent_app_number] => 11/832613
[patent_app_country] => US
[patent_app_date] => 2007-08-01
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 18
[patent_figures_cnt] => 20
[patent_no_of_words] => 8853
[patent_no_of_claims] => 9
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 73
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/07/721/07721997.pdf
[firstpage_image] =>[orig_patent_app_number] => 11832613
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/832613 | Method and system for providing cruciform steered, bent biconic and plasma suppression for maximum accuracy | Jul 31, 2007 | Issued |
Array
(
[id] => 8373915
[patent_doc_number] => 08256707
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2012-09-04
[patent_title] => 'Engine mounting configuration for a turbofan gas turbine engine'
[patent_app_type] => utility
[patent_app_number] => 11/832107
[patent_app_country] => US
[patent_app_date] => 2007-08-01
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 16
[patent_figures_cnt] => 19
[patent_no_of_words] => 3059
[patent_no_of_claims] => 21
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 77
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 11832107
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/832107 | Engine mounting configuration for a turbofan gas turbine engine | Jul 31, 2007 | Issued |
Array
(
[id] => 4648531
[patent_doc_number] => 20080035786
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2008-02-14
[patent_title] => 'EXPENDABLE SONOBUOY FLIGHT KIT WITH AERODYNAMICALLY ASSISTED SONOBUOY SEPARATION'
[patent_app_type] => utility
[patent_app_number] => 11/782487
[patent_app_country] => US
[patent_app_date] => 2007-07-24
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 20
[patent_figures_cnt] => 20
[patent_no_of_words] => 11392
[patent_no_of_claims] => 66
[patent_no_of_ind_claims] => 14
[patent_words_short_claim] => 0
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0035/20080035786.pdf
[firstpage_image] =>[orig_patent_app_number] => 11782487
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/782487 | EXPENDABLE SONOBUOY FLIGHT KIT WITH AERODYNAMICALLY ASSISTED SONOBUOY SEPARATION | Jul 23, 2007 | Abandoned |
Array
(
[id] => 4429256
[patent_doc_number] => 07967255
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2011-06-28
[patent_title] => 'Autonomous space flight system and planetary lander for executing a discrete landing sequence to remove unknown navigation error, perform hazard avoidance and relocate the lander and method'
[patent_app_type] => utility
[patent_app_number] => 11/782407
[patent_app_country] => US
[patent_app_date] => 2007-07-24
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 16
[patent_figures_cnt] => 19
[patent_no_of_words] => 11584
[patent_no_of_claims] => 27
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[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/07/967/07967255.pdf
[firstpage_image] =>[orig_patent_app_number] => 11782407
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/782407 | Autonomous space flight system and planetary lander for executing a discrete landing sequence to remove unknown navigation error, perform hazard avoidance and relocate the lander and method | Jul 23, 2007 | Issued |
Array
(
[id] => 210577
[patent_doc_number] => 07621484
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2009-11-24
[patent_title] => 'Rotor kite'
[patent_app_type] => utility
[patent_app_number] => 11/779921
[patent_app_country] => US
[patent_app_date] => 2007-07-19
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 12
[patent_no_of_words] => 2223
[patent_no_of_claims] => 10
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[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/07/621/07621484.pdf
[firstpage_image] =>[orig_patent_app_number] => 11779921
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/779921 | Rotor kite | Jul 18, 2007 | Issued |
Array
(
[id] => 4493394
[patent_doc_number] => 07918420
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2011-04-05
[patent_title] => 'System and methods for simultaneous momentum dumping and orbit control'
[patent_app_type] => utility
[patent_app_number] => 11/778909
[patent_app_country] => US
[patent_app_date] => 2007-07-17
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 1
[patent_figures_cnt] => 1
[patent_no_of_words] => 7078
[patent_no_of_claims] => 20
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[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/07/918/07918420.pdf
[firstpage_image] =>[orig_patent_app_number] => 11778909
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/778909 | System and methods for simultaneous momentum dumping and orbit control | Jul 16, 2007 | Issued |
Array
(
[id] => 5340463
[patent_doc_number] => 20090179113
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2009-07-16
[patent_title] => 'Method and apparatus for elevating and manipulating objects using electromagnetic fields only'
[patent_app_type] => utility
[patent_app_number] => 11/827433
[patent_app_country] => US
[patent_app_date] => 2007-07-11
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 15
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[patent_no_of_words] => 18491
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[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0179/20090179113.pdf
[firstpage_image] =>[orig_patent_app_number] => 11827433
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/827433 | Method and apparatus for elevating and manipulating objects using electromagnetic fields only | Jul 10, 2007 | Abandoned |
Array
(
[id] => 4952451
[patent_doc_number] => 20080185475
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2008-08-07
[patent_title] => 'SOLAR-POWERED AIRCRAFT'
[patent_app_type] => utility
[patent_app_number] => 11/774732
[patent_app_country] => US
[patent_app_date] => 2007-07-09
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
[patent_figures_cnt] => 5
[patent_no_of_words] => 3930
[patent_no_of_claims] => 11
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[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0185/20080185475.pdf
[firstpage_image] =>[orig_patent_app_number] => 11774732
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/774732 | SOLAR-POWERED AIRCRAFT | Jul 8, 2007 | Abandoned |
Array
(
[id] => 11189
[patent_doc_number] => 07806367
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2010-10-05
[patent_title] => 'Integrated multispar torsion box of composite material'
[patent_app_type] => utility
[patent_app_number] => 11/825123
[patent_app_country] => US
[patent_app_date] => 2007-07-02
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 6
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[patent_no_of_words] => 2215
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[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/07/806/07806367.pdf
[firstpage_image] =>[orig_patent_app_number] => 11825123
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/825123 | Integrated multispar torsion box of composite material | Jul 1, 2007 | Issued |
Array
(
[id] => 5345860
[patent_doc_number] => 20090001221
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2009-01-01
[patent_title] => 'SPACECRAFT GRAPPLE ASSEMBLY AND DOCKING SYSTEM EMPLOYING THE SAME'
[patent_app_type] => utility
[patent_app_number] => 11/771597
[patent_app_country] => US
[patent_app_date] => 2007-06-29
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
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[pdf_file] => publications/A1/0001/20090001221.pdf
[firstpage_image] =>[orig_patent_app_number] => 11771597
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/771597 | SPACECRAFT GRAPPLE ASSEMBLY AND DOCKING SYSTEM EMPLOYING THE SAME | Jun 28, 2007 | Abandoned |
Array
(
[id] => 4849290
[patent_doc_number] => 20080315032
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2008-12-25
[patent_title] => 'Techniques for providing surface control to a guidable projectile'
[patent_app_type] => utility
[patent_app_number] => 11/820815
[patent_app_country] => US
[patent_app_date] => 2007-06-21
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 11
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[patent_no_of_words] => 7543
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[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0315/20080315032.pdf
[firstpage_image] =>[orig_patent_app_number] => 11820815
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/820815 | Techniques for providing surface control to a guidable projectile | Jun 20, 2007 | Issued |
Array
(
[id] => 9646922
[patent_doc_number] => 08800926
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2014-08-12
[patent_title] => 'Radio frequency shielding apparatus system and method'
[patent_app_type] => utility
[patent_app_number] => 11/812300
[patent_app_country] => US
[patent_app_date] => 2007-06-18
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 8
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[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 11812300
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/812300 | Radio frequency shielding apparatus system and method | Jun 17, 2007 | Issued |