
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] => 4685472
[patent_doc_number] => 20080029653
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2008-02-07
[patent_title] => 'CONTROL SYSTEM FOR CONTROLLING PROPELLER AIRCRAFT ENGINE DURING TAKEOFF'
[patent_app_type] => utility
[patent_app_number] => 11/459756
[patent_app_country] => US
[patent_app_date] => 2006-07-25
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 4
[patent_no_of_words] => 3359
[patent_no_of_claims] => 19
[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/A1/0029/20080029653.pdf
[firstpage_image] =>[orig_patent_app_number] => 11459756
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/459756 | Control system for controlling propeller aircraft engine during takeoff | Jul 24, 2006 | Issued |
Array
(
[id] => 5299927
[patent_doc_number] => 20090294579
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2009-12-03
[patent_title] => 'PRIMARY ENGINE STRUT STRUCTURE OF AN AIRCRAFT'
[patent_app_type] => utility
[patent_app_number] => 11/997834
[patent_app_country] => US
[patent_app_date] => 2006-07-13
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 3
[patent_no_of_words] => 1393
[patent_no_of_claims] => 10
[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/A1/0294/20090294579.pdf
[firstpage_image] =>[orig_patent_app_number] => 11997834
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/997834 | PRIMARY ENGINE STRUT STRUCTURE OF AN AIRCRAFT | Jul 12, 2006 | Abandoned |
Array
(
[id] => 4930257
[patent_doc_number] => 20080001032
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2008-01-03
[patent_title] => 'Counter hijacking system for an airliner'
[patent_app_type] => utility
[patent_app_number] => 11/480019
[patent_app_country] => US
[patent_app_date] => 2006-07-03
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 6
[patent_figures_cnt] => 6
[patent_no_of_words] => 3021
[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/A1/0001/20080001032.pdf
[firstpage_image] =>[orig_patent_app_number] => 11480019
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/480019 | Counter hijacking system for an airliner | Jul 2, 2006 | Abandoned |
Array
(
[id] => 5377176
[patent_doc_number] => 20090189015
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2009-07-30
[patent_title] => 'Unmanned Aircraft for Telecommunicative or Scientific Purposes'
[patent_app_type] => utility
[patent_app_number] => 12/160119
[patent_app_country] => US
[patent_app_date] => 2006-07-01
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
[patent_figures_cnt] => 5
[patent_no_of_words] => 2830
[patent_no_of_claims] => 20
[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/A1/0189/20090189015.pdf
[firstpage_image] =>[orig_patent_app_number] => 12160119
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/160119 | Unmanned aircraft for telecommunicative or scientific purposes | Jun 30, 2006 | Issued |
Array
(
[id] => 5092716
[patent_doc_number] => 20070114325
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2007-05-24
[patent_title] => 'Tailboom-stabilized VTOL aircraft'
[patent_app_type] => utility
[patent_app_number] => 11/479833
[patent_app_country] => US
[patent_app_date] => 2006-06-30
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 10
[patent_figures_cnt] => 10
[patent_no_of_words] => 9538
[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/A1/0114/20070114325.pdf
[firstpage_image] =>[orig_patent_app_number] => 11479833
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/479833 | Tailboom-stabilized VTOL aircraft | Jun 29, 2006 | Abandoned |
Array
(
[id] => 9501830
[patent_doc_number] => 08740136
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2014-06-03
[patent_title] => 'Engine mount for an aircraft, to be placed between an engine and an engine mounting structure'
[patent_app_type] => utility
[patent_app_number] => 11/913950
[patent_app_country] => US
[patent_app_date] => 2006-06-27
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
[patent_figures_cnt] => 5
[patent_no_of_words] => 4107
[patent_no_of_claims] => 15
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 132
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 11913950
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/913950 | Engine mount for an aircraft, to be placed between an engine and an engine mounting structure | Jun 26, 2006 | Issued |
Array
(
[id] => 5327659
[patent_doc_number] => 20090108136
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2009-04-30
[patent_title] => 'Navigation Body, Navigation Device, and Space Navigation Device'
[patent_app_type] => utility
[patent_app_number] => 12/227024
[patent_app_country] => US
[patent_app_date] => 2006-06-26
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 15
[patent_figures_cnt] => 15
[patent_no_of_words] => 6796
[patent_no_of_claims] => 6
[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/A1/0108/20090108136.pdf
[firstpage_image] =>[orig_patent_app_number] => 12227024
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/227024 | Navigation Body, Navigation Device, and Space Navigation Device | Jun 25, 2006 | Abandoned |
Array
(
[id] => 74996
[patent_doc_number] => 07750275
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2010-07-06
[patent_title] => 'Folding control surface assembly and vehicle incorporating same'
[patent_app_type] => utility
[patent_app_number] => 11/474029
[patent_app_country] => US
[patent_app_date] => 2006-06-23
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 7
[patent_no_of_words] => 2581
[patent_no_of_claims] => 32
[patent_no_of_ind_claims] => 5
[patent_words_short_claim] => 75
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/07/750/07750275.pdf
[firstpage_image] =>[orig_patent_app_number] => 11474029
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/474029 | Folding control surface assembly and vehicle incorporating same | Jun 22, 2006 | Issued |
Array
(
[id] => 4465091
[patent_doc_number] => 07942366
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2011-05-17
[patent_title] => 'Aircraft landing gear with integrated extension, retraction, and leveling feature'
[patent_app_type] => utility
[patent_app_number] => 11/473977
[patent_app_country] => US
[patent_app_date] => 2006-06-23
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 6
[patent_no_of_words] => 2183
[patent_no_of_claims] => 15
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 141
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/07/942/07942366.pdf
[firstpage_image] =>[orig_patent_app_number] => 11473977
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/473977 | Aircraft landing gear with integrated extension, retraction, and leveling feature | Jun 22, 2006 | Issued |
Array
(
[id] => 5213501
[patent_doc_number] => 20070102581
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2007-05-10
[patent_title] => 'System and method for converting a passenger aircraft to a cargo aircraft'
[patent_app_type] => utility
[patent_app_number] => 11/473599
[patent_app_country] => US
[patent_app_date] => 2006-06-22
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 0
[patent_figures_cnt] => 0
[patent_no_of_words] => 271
[patent_no_of_claims] => 5
[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/A1/0102/20070102581.pdf
[firstpage_image] =>[orig_patent_app_number] => 11473599
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/473599 | System and method for converting a passenger aircraft to a cargo aircraft | Jun 21, 2006 | Abandoned |
Array
(
[id] => 5092715
[patent_doc_number] => 20070114324
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2007-05-24
[patent_title] => 'Vertical take-off aircraft - F'
[patent_app_type] => utility
[patent_app_number] => 11/454309
[patent_app_country] => US
[patent_app_date] => 2006-06-16
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 16
[patent_figures_cnt] => 16
[patent_no_of_words] => 3279
[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/A1/0114/20070114324.pdf
[firstpage_image] =>[orig_patent_app_number] => 11454309
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/454309 | Vertical take-off aircraft - F | Jun 15, 2006 | Abandoned |
Array
(
[id] => 5180504
[patent_doc_number] => 20070051846
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2007-03-08
[patent_title] => 'Small-size high-speed transmission system for use in microturbine-powered aircraft'
[patent_app_type] => utility
[patent_app_number] => 11/398375
[patent_app_country] => US
[patent_app_date] => 2006-06-14
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 11
[patent_figures_cnt] => 11
[patent_no_of_words] => 8022
[patent_no_of_claims] => 27
[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/A1/0051/20070051846.pdf
[firstpage_image] =>[orig_patent_app_number] => 11398375
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/398375 | Small-size high-speed transmission system for use in microturbine-powered aircraft | Jun 13, 2006 | Issued |
Array
(
[id] => 5268304
[patent_doc_number] => 20090072079
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2009-03-19
[patent_title] => 'Aircraft having a pivotable powerplant'
[patent_app_type] => utility
[patent_app_number] => 11/451216
[patent_app_country] => US
[patent_app_date] => 2006-06-12
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 4
[patent_no_of_words] => 6477
[patent_no_of_claims] => 23
[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/A1/0072/20090072079.pdf
[firstpage_image] =>[orig_patent_app_number] => 11451216
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/451216 | Aircraft having a pivotable powerplant | Jun 11, 2006 | Issued |
Array
(
[id] => 5388881
[patent_doc_number] => 20090206193
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2009-08-20
[patent_title] => 'Ballistically deployed telescoping aircraft wing'
[patent_app_type] => utility
[patent_app_number] => 11/450720
[patent_app_country] => US
[patent_app_date] => 2006-06-09
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 7
[patent_figures_cnt] => 7
[patent_no_of_words] => 5581
[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/A1/0206/20090206193.pdf
[firstpage_image] =>[orig_patent_app_number] => 11450720
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/450720 | Ballistically deployed telescoping aircraft wing | Jun 8, 2006 | Abandoned |
Array
(
[id] => 5848238
[patent_doc_number] => 20060231676
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2006-10-19
[patent_title] => 'Vertical take-off aircraft - E'
[patent_app_type] => utility
[patent_app_number] => 11/446231
[patent_app_country] => US
[patent_app_date] => 2006-06-05
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 16
[patent_figures_cnt] => 16
[patent_no_of_words] => 3013
[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/A1/0231/20060231676.pdf
[firstpage_image] =>[orig_patent_app_number] => 11446231
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/446231 | Vertical take-off aircraft - E | Jun 4, 2006 | Abandoned |
Array
(
[id] => 5213489
[patent_doc_number] => 20070102569
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2007-05-10
[patent_title] => 'Vertical take-off aircraft - P'
[patent_app_type] => utility
[patent_app_number] => 11/442404
[patent_app_country] => US
[patent_app_date] => 2006-05-30
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 10
[patent_figures_cnt] => 10
[patent_no_of_words] => 3029
[patent_no_of_claims] => 4
[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/A1/0102/20070102569.pdf
[firstpage_image] =>[orig_patent_app_number] => 11442404
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/442404 | Vertical take-off aircraft - P | May 29, 2006 | Abandoned |
Array
(
[id] => 202726
[patent_doc_number] => 07628354
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2009-12-08
[patent_title] => 'Apparatus for deploying wing of guided missile'
[patent_app_type] => utility
[patent_app_number] => 11/441732
[patent_app_country] => US
[patent_app_date] => 2006-05-26
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 9
[patent_figures_cnt] => 15
[patent_no_of_words] => 5110
[patent_no_of_claims] => 12
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 118
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/07/628/07628354.pdf
[firstpage_image] =>[orig_patent_app_number] => 11441732
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/441732 | Apparatus for deploying wing of guided missile | May 25, 2006 | Issued |
| 11/493944 | Aerial delivery device | May 24, 2006 | Abandoned |
Array
(
[id] => 194993
[patent_doc_number] => 07637458
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2009-12-29
[patent_title] => 'Systems and methods for providing back-up hydraulic power for aircraft, including tanker aircraft'
[patent_app_type] => utility
[patent_app_number] => 11/440816
[patent_app_country] => US
[patent_app_date] => 2006-05-24
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 4
[patent_no_of_words] => 4519
[patent_no_of_claims] => 21
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 249
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/07/637/07637458.pdf
[firstpage_image] =>[orig_patent_app_number] => 11440816
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/440816 | Systems and methods for providing back-up hydraulic power for aircraft, including tanker aircraft | May 23, 2006 | Issued |
Array
(
[id] => 9550516
[patent_doc_number] => 08757555
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2014-06-24
[patent_title] => 'Concept of a variable winglet for lateral load reduction for combined lateral and vertical load reduction, and for improving the performance of means of locomotion'
[patent_app_type] => utility
[patent_app_number] => 11/914411
[patent_app_country] => US
[patent_app_date] => 2006-05-19
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 6
[patent_figures_cnt] => 10
[patent_no_of_words] => 4536
[patent_no_of_claims] => 22
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 97
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 11914411
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/914411 | Concept of a variable winglet for lateral load reduction for combined lateral and vertical load reduction, and for improving the performance of means of locomotion | May 18, 2006 | Issued |