
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] => 1008544
[patent_doc_number] => 06899300
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2005-05-31
[patent_title] => 'Process for the loading of fuel into an aircraft on the ground'
[patent_app_type] => utility
[patent_app_number] => 10/720151
[patent_app_country] => US
[patent_app_date] => 2003-11-25
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
[patent_figures_cnt] => 8
[patent_no_of_words] => 3247
[patent_no_of_claims] => 8
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 145
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/899/06899300.pdf
[firstpage_image] =>[orig_patent_app_number] => 10720151
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/720151 | Process for the loading of fuel into an aircraft on the ground | Nov 24, 2003 | Issued |
Array
(
[id] => 6936318
[patent_doc_number] => 20050109879
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2005-05-26
[patent_title] => 'Method and apparatus for quantum vortex implosion propulsion and species'
[patent_app_type] => utility
[patent_app_number] => 10/719717
[patent_app_country] => US
[patent_app_date] => 2003-11-21
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 25
[patent_figures_cnt] => 25
[patent_no_of_words] => 26010
[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/A1/0109/20050109879.pdf
[firstpage_image] =>[orig_patent_app_number] => 10719717
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/719717 | Method and apparatus for quantum vortex implosion propulsion and species | Nov 20, 2003 | Abandoned |
Array
(
[id] => 7139768
[patent_doc_number] => 20050116092
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2005-06-02
[patent_title] => 'Blended leading and trailing edge wing planform'
[patent_app_type] => utility
[patent_app_number] => 10/717366
[patent_app_country] => US
[patent_app_date] => 2003-11-19
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 2
[patent_figures_cnt] => 2
[patent_no_of_words] => 1348
[patent_no_of_claims] => 14
[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/A1/0116/20050116092.pdf
[firstpage_image] =>[orig_patent_app_number] => 10717366
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/717366 | Blended leading and trailing edge wing planform | Nov 18, 2003 | Abandoned |
Array
(
[id] => 7139793
[patent_doc_number] => 20050116112
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2005-06-02
[patent_title] => 'High energy electric feed drive system'
[patent_app_type] => utility
[patent_app_number] => 10/717848
[patent_app_country] => US
[patent_app_date] => 2003-11-19
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
[patent_figures_cnt] => 5
[patent_no_of_words] => 2862
[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/A1/0116/20050116112.pdf
[firstpage_image] =>[orig_patent_app_number] => 10717848
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/717848 | High energy electric feed drive system | Nov 18, 2003 | Abandoned |
Array
(
[id] => 382240
[patent_doc_number] => 07306188
[patent_country] => US
[patent_kind] => B1
[patent_issue_date] => 2007-12-11
[patent_title] => 'Non-pyrotechnic remote-controlled parachute jettison device'
[patent_app_type] => utility
[patent_app_number] => 10/715243
[patent_app_country] => US
[patent_app_date] => 2003-11-18
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 4
[patent_no_of_words] => 1208
[patent_no_of_claims] => 6
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 106
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/07/306/07306188.pdf
[firstpage_image] =>[orig_patent_app_number] => 10715243
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/715243 | Non-pyrotechnic remote-controlled parachute jettison device | Nov 17, 2003 | Issued |
Array
(
[id] => 1051835
[patent_doc_number] => 06857597
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2005-02-22
[patent_title] => 'Control system for vertical take off and land (VTOL) aircraft'
[patent_app_type] => utility
[patent_app_number] => 10/717213
[patent_app_country] => US
[patent_app_date] => 2003-11-18
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 13
[patent_figures_cnt] => 14
[patent_no_of_words] => 2497
[patent_no_of_claims] => 19
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 158
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/857/06857597.pdf
[firstpage_image] =>[orig_patent_app_number] => 10717213
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/717213 | Control system for vertical take off and land (VTOL) aircraft | Nov 17, 2003 | Issued |
Array
(
[id] => 7218774
[patent_doc_number] => 20040155146
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2004-08-12
[patent_title] => 'Method of controlling a landing guide path of an aircraft'
[patent_app_type] => new
[patent_app_number] => 10/713160
[patent_app_country] => US
[patent_app_date] => 2003-11-17
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 3
[patent_no_of_words] => 3258
[patent_no_of_claims] => 16
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 27
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0155/20040155146.pdf
[firstpage_image] =>[orig_patent_app_number] => 10713160
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/713160 | Method of controlling a landing guide path of an aircraft | Nov 16, 2003 | Abandoned |
Array
(
[id] => 703088
[patent_doc_number] => 07059034
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2006-06-13
[patent_title] => 'One-piece closed-shape structure and method of forming same'
[patent_app_type] => utility
[patent_app_number] => 10/712041
[patent_app_country] => US
[patent_app_date] => 2003-11-14
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 65
[patent_figures_cnt] => 79
[patent_no_of_words] => 17576
[patent_no_of_claims] => 4
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 66
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/07/059/07059034.pdf
[firstpage_image] =>[orig_patent_app_number] => 10712041
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/712041 | One-piece closed-shape structure and method of forming same | Nov 13, 2003 | Issued |
Array
(
[id] => 8878272
[patent_doc_number] => 08473254
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2013-06-25
[patent_title] => 'Methods for configuring aircraft to meet performance goals and shock wave disturbance constraints'
[patent_app_type] => utility
[patent_app_number] => 10/714276
[patent_app_country] => US
[patent_app_date] => 2003-11-14
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 10
[patent_figures_cnt] => 21
[patent_no_of_words] => 8042
[patent_no_of_claims] => 22
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 69
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 10714276
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/714276 | Methods for configuring aircraft to meet performance goals and shock wave disturbance constraints | Nov 13, 2003 | Issued |
Array
(
[id] => 601482
[patent_doc_number] => 07431239
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2008-10-07
[patent_title] => 'One-piece closed-shape structure and method of forming same'
[patent_app_type] => utility
[patent_app_number] => 10/712042
[patent_app_country] => US
[patent_app_date] => 2003-11-14
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 66
[patent_figures_cnt] => 79
[patent_no_of_words] => 17571
[patent_no_of_claims] => 22
[patent_no_of_ind_claims] => 7
[patent_words_short_claim] => 172
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/07/431/07431239.pdf
[firstpage_image] =>[orig_patent_app_number] => 10712042
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/712042 | One-piece closed-shape structure and method of forming same | Nov 13, 2003 | Issued |
Array
(
[id] => 7139764
[patent_doc_number] => 20050116088
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2005-06-02
[patent_title] => 'Shock and vibration isolation system'
[patent_app_type] => utility
[patent_app_number] => 10/713760
[patent_app_country] => US
[patent_app_date] => 2003-11-13
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 10
[patent_figures_cnt] => 10
[patent_no_of_words] => 3312
[patent_no_of_claims] => 29
[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/A1/0116/20050116088.pdf
[firstpage_image] =>[orig_patent_app_number] => 10713760
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/713760 | Shock and vibration isolation system | Nov 12, 2003 | Issued |
Array
(
[id] => 7139761
[patent_doc_number] => 20050116086
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2005-06-02
[patent_title] => 'Wing assemblies for aircraft'
[patent_app_type] => utility
[patent_app_number] => 10/705529
[patent_app_country] => US
[patent_app_date] => 2003-11-12
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 4
[patent_no_of_words] => 1843
[patent_no_of_claims] => 20
[patent_no_of_ind_claims] => 6
[patent_words_short_claim] => 0
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0116/20050116086.pdf
[firstpage_image] =>[orig_patent_app_number] => 10705529
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/705529 | Wing assemblies for aircraft | Nov 11, 2003 | Abandoned |
Array
(
[id] => 7139797
[patent_doc_number] => 20050116116
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2005-06-02
[patent_title] => 'Wing employing leading edge flaps and winglets to achieve improved aerodynamic performance'
[patent_app_type] => utility
[patent_app_number] => 10/706671
[patent_app_country] => US
[patent_app_date] => 2003-11-11
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 24
[patent_figures_cnt] => 24
[patent_no_of_words] => 10016
[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/A1/0116/20050116116.pdf
[firstpage_image] =>[orig_patent_app_number] => 10706671
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/706671 | Wing employing leading edge flaps and winglets to achieve improved aerodynamic performance | Nov 10, 2003 | Abandoned |
Array
(
[id] => 1019507
[patent_doc_number] => 06886774
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2005-05-03
[patent_title] => 'Method for piloting a spinning projectile'
[patent_app_type] => utility
[patent_app_number] => 10/703428
[patent_app_country] => US
[patent_app_date] => 2003-11-10
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 7
[patent_figures_cnt] => 7
[patent_no_of_words] => 7090
[patent_no_of_claims] => 5
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 345
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/886/06886774.pdf
[firstpage_image] =>[orig_patent_app_number] => 10703428
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/703428 | Method for piloting a spinning projectile | Nov 9, 2003 | Issued |
Array
(
[id] => 7101208
[patent_doc_number] => 20050103934
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2005-05-19
[patent_title] => 'Cargo oriented personal aircraft'
[patent_app_type] => utility
[patent_app_number] => 10/701146
[patent_app_country] => US
[patent_app_date] => 2003-11-04
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
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[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0103/20050103934.pdf
[firstpage_image] =>[orig_patent_app_number] => 10701146
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/701146 | Cargo oriented personal aircraft | Nov 3, 2003 | Issued |
Array
(
[id] => 7295622
[patent_doc_number] => 20040124312
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2004-07-01
[patent_title] => 'System and method for use of external secondary payloads'
[patent_app_type] => new
[patent_app_number] => 10/698261
[patent_app_country] => US
[patent_app_date] => 2003-10-31
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 8
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[patent_no_of_words] => 9764
[patent_no_of_claims] => 70
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[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0124/20040124312.pdf
[firstpage_image] =>[orig_patent_app_number] => 10698261
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/698261 | System for use of external secondary payloads | Oct 30, 2003 | Issued |
Array
(
[id] => 7439883
[patent_doc_number] => 20040195451
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2004-10-07
[patent_title] => 'Seat-mounting systems and methods'
[patent_app_type] => new
[patent_app_number] => 10/694241
[patent_app_country] => US
[patent_app_date] => 2003-10-27
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 9
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[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0195/20040195451.pdf
[firstpage_image] =>[orig_patent_app_number] => 10694241
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/694241 | Seat-mounting systems and methods | Oct 26, 2003 | Abandoned |
Array
(
[id] => 4595973
[patent_doc_number] => 07975465
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2011-07-12
[patent_title] => 'Hybrid engine accessory power system'
[patent_app_type] => utility
[patent_app_number] => 10/694645
[patent_app_country] => US
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[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/07/975/07975465.pdf
[firstpage_image] =>[orig_patent_app_number] => 10694645
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/694645 | Hybrid engine accessory power system | Oct 26, 2003 | Issued |
Array
(
[id] => 1063959
[patent_doc_number] => 06845939
[patent_country] => US
[patent_kind] => B1
[patent_issue_date] => 2005-01-25
[patent_title] => 'Tailboom-stabilized VTOL aircraft'
[patent_app_type] => utility
[patent_app_number] => 10/693800
[patent_app_country] => US
[patent_app_date] => 2003-10-24
[patent_effective_date] => 0000-00-00
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[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/845/06845939.pdf
[firstpage_image] =>[orig_patent_app_number] => 10693800
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/693800 | Tailboom-stabilized VTOL aircraft | Oct 23, 2003 | Issued |
Array
(
[id] => 7153955
[patent_doc_number] => 20050082425
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2005-04-21
[patent_title] => 'EMPENNAGE ASSEMBLY AND ATTACHMENT MECHANISM FOR A MODEL AIRPLANE'
[patent_app_type] => utility
[patent_app_number] => 10/690065
[patent_app_country] => US
[patent_app_date] => 2003-10-21
[patent_effective_date] => 0000-00-00
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[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0082/20050082425.pdf
[firstpage_image] =>[orig_patent_app_number] => 10690065
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/690065 | Empennage assembly and attachment mechanism for a model airplane | Oct 20, 2003 | Issued |