
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] => 1148374
[patent_doc_number] => 06764043
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2004-07-20
[patent_title] => 'Rotatable scarf inlet for an aircraft engine and method of using the same'
[patent_app_type] => B2
[patent_app_number] => 10/316497
[patent_app_country] => US
[patent_app_date] => 2002-12-11
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 11
[patent_no_of_words] => 3498
[patent_no_of_claims] => 46
[patent_no_of_ind_claims] => 5
[patent_words_short_claim] => 63
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/764/06764043.pdf
[firstpage_image] =>[orig_patent_app_number] => 10316497
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/316497 | Rotatable scarf inlet for an aircraft engine and method of using the same | Dec 10, 2002 | Issued |
Array
(
[id] => 6785635
[patent_doc_number] => 20030136874
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2003-07-24
[patent_title] => 'Method for safer mid-air refueling'
[patent_app_type] => new
[patent_app_number] => 10/316623
[patent_app_country] => US
[patent_app_date] => 2002-12-10
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 8
[patent_figures_cnt] => 8
[patent_no_of_words] => 7250
[patent_no_of_claims] => 3
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 390
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0136/20030136874.pdf
[firstpage_image] =>[orig_patent_app_number] => 10316623
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/316623 | Method for safer mid-air refueling | Dec 9, 2002 | Abandoned |
Array
(
[id] => 1193965
[patent_doc_number] => 06726150
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2004-04-27
[patent_title] => 'Method and apparatus for stiffener reinforcement of a ram air parachute canopy'
[patent_app_type] => B2
[patent_app_number] => 10/315488
[patent_app_country] => US
[patent_app_date] => 2002-12-09
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 2
[patent_figures_cnt] => 5
[patent_no_of_words] => 1835
[patent_no_of_claims] => 13
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 40
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/726/06726150.pdf
[firstpage_image] =>[orig_patent_app_number] => 10315488
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/315488 | Method and apparatus for stiffener reinforcement of a ram air parachute canopy | Dec 8, 2002 | Issued |
Array
(
[id] => 1142963
[patent_doc_number] => 06769649
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2004-08-03
[patent_title] => 'Ram air parachute canopy with improved nose structure'
[patent_app_type] => B2
[patent_app_number] => 10/315459
[patent_app_country] => US
[patent_app_date] => 2002-12-09
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
[patent_figures_cnt] => 11
[patent_no_of_words] => 4117
[patent_no_of_claims] => 8
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 102
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/769/06769649.pdf
[firstpage_image] =>[orig_patent_app_number] => 10315459
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/315459 | Ram air parachute canopy with improved nose structure | Dec 8, 2002 | Issued |
Array
(
[id] => 1061417
[patent_doc_number] => 06848649
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2005-02-01
[patent_title] => 'V/STOL biplane aircraft'
[patent_app_type] => utility
[patent_app_number] => 10/313580
[patent_app_country] => US
[patent_app_date] => 2002-12-09
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 18
[patent_figures_cnt] => 41
[patent_no_of_words] => 18523
[patent_no_of_claims] => 20
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 420
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/848/06848649.pdf
[firstpage_image] =>[orig_patent_app_number] => 10313580
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/313580 | V/STOL biplane aircraft | Dec 8, 2002 | Issued |
Array
(
[id] => 6666594
[patent_doc_number] => 20030111577
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2003-06-19
[patent_title] => 'Membrane structure'
[patent_app_type] => new
[patent_app_number] => 10/310840
[patent_app_country] => US
[patent_app_date] => 2002-12-06
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 6
[patent_figures_cnt] => 6
[patent_no_of_words] => 5115
[patent_no_of_claims] => 6
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 156
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0111/20030111577.pdf
[firstpage_image] =>[orig_patent_app_number] => 10310840
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/310840 | Membrane structure | Dec 5, 2002 | Issued |
Array
(
[id] => 6694767
[patent_doc_number] => 20030106961
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2003-06-12
[patent_title] => 'Method and device for steepening a landing approach of an aircraft'
[patent_app_type] => new
[patent_app_number] => 10/313052
[patent_app_country] => US
[patent_app_date] => 2002-12-06
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 3
[patent_no_of_words] => 3234
[patent_no_of_claims] => 22
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 74
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0106/20030106961.pdf
[firstpage_image] =>[orig_patent_app_number] => 10313052
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/313052 | Method and device for steepening a landing approach of an aircraft | Dec 5, 2002 | Issued |
Array
(
[id] => 453905
[patent_doc_number] => 07243879
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2007-07-17
[patent_title] => 'Lattice fin for missiles or other fluid-born bodies and method for producing same'
[patent_app_type] => utility
[patent_app_number] => 10/313222
[patent_app_country] => US
[patent_app_date] => 2002-12-06
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 8
[patent_figures_cnt] => 17
[patent_no_of_words] => 5324
[patent_no_of_claims] => 21
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 117
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/07/243/07243879.pdf
[firstpage_image] =>[orig_patent_app_number] => 10313222
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/313222 | Lattice fin for missiles or other fluid-born bodies and method for producing same | Dec 5, 2002 | Issued |
Array
(
[id] => 502850
[patent_doc_number] => 07198225
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2007-04-03
[patent_title] => 'Aircraft control system'
[patent_app_type] => utility
[patent_app_number] => 10/310415
[patent_app_country] => US
[patent_app_date] => 2002-12-05
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 28
[patent_figures_cnt] => 38
[patent_no_of_words] => 14299
[patent_no_of_claims] => 8
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 142
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/07/198/07198225.pdf
[firstpage_image] =>[orig_patent_app_number] => 10310415
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/310415 | Aircraft control system | Dec 4, 2002 | Issued |
Array
(
[id] => 7080386
[patent_doc_number] => 20050045766
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2005-03-03
[patent_title] => 'FORM FACTORED COMPLIANT METALLIC TRANSITION ELEMENT FOR ATTACHING A CERAMIC ELEMENT TO A METALLIC ELEMENT'
[patent_app_type] => utility
[patent_app_number] => 10/313713
[patent_app_country] => US
[patent_app_date] => 2002-12-04
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 3
[patent_no_of_words] => 4913
[patent_no_of_claims] => 30
[patent_no_of_ind_claims] => 9
[patent_words_short_claim] => 0
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0045/20050045766.pdf
[firstpage_image] =>[orig_patent_app_number] => 10313713
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/313713 | Form factored compliant metallic transition element for attaching a ceramic element to a metallic element | Dec 3, 2002 | Issued |
Array
(
[id] => 8100903
[patent_doc_number] => 08152099
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2012-04-10
[patent_title] => 'Method of landing an aircraft and apparatus therefor'
[patent_app_type] => utility
[patent_app_number] => 10/497317
[patent_app_country] => US
[patent_app_date] => 2002-12-03
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 7
[patent_no_of_words] => 5867
[patent_no_of_claims] => 12
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 68
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/08/152/08152099.pdf
[firstpage_image] =>[orig_patent_app_number] => 10497317
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/497317 | Method of landing an aircraft and apparatus therefor | Dec 2, 2002 | Issued |
Array
(
[id] => 1253779
[patent_doc_number] => 06666407
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2003-12-23
[patent_title] => 'Helicopter undercarriage'
[patent_app_type] => B2
[patent_app_number] => 10/304910
[patent_app_country] => US
[patent_app_date] => 2002-11-26
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
[patent_figures_cnt] => 5
[patent_no_of_words] => 2517
[patent_no_of_claims] => 13
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 120
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/666/06666407.pdf
[firstpage_image] =>[orig_patent_app_number] => 10304910
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/304910 | Helicopter undercarriage | Nov 25, 2002 | Issued |
Array
(
[id] => 615099
[patent_doc_number] => 07143981
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2006-12-05
[patent_title] => 'Parachute rescue system for multistory buildings'
[patent_app_type] => utility
[patent_app_number] => 10/494519
[patent_app_country] => US
[patent_app_date] => 2002-11-13
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 2
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[patent_no_of_words] => 2876
[patent_no_of_claims] => 16
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[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/07/143/07143981.pdf
[firstpage_image] =>[orig_patent_app_number] => 10494519
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/494519 | Parachute rescue system for multistory buildings | Nov 12, 2002 | Issued |
Array
(
[id] => 1243660
[patent_doc_number] => 06676072
[patent_country] => US
[patent_kind] => B1
[patent_issue_date] => 2004-01-13
[patent_title] => 'Short duration, high-torque rocket nozzle'
[patent_app_type] => B1
[patent_app_number] => 10/292948
[patent_app_country] => US
[patent_app_date] => 2002-11-13
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 1
[patent_figures_cnt] => 2
[patent_no_of_words] => 4061
[patent_no_of_claims] => 18
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[patent_words_short_claim] => 131
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/676/06676072.pdf
[firstpage_image] =>[orig_patent_app_number] => 10292948
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/292948 | Short duration, high-torque rocket nozzle | Nov 12, 2002 | Issued |
Array
(
[id] => 7352915
[patent_doc_number] => 20040089763
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2004-05-13
[patent_title] => 'Personal flight vehicle and system'
[patent_app_type] => new
[patent_app_number] => 10/293826
[patent_app_country] => US
[patent_app_date] => 2002-11-12
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 37
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[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0089/20040089763.pdf
[firstpage_image] =>[orig_patent_app_number] => 10293826
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/293826 | Personal flight vehicle and system | Nov 11, 2002 | Issued |
Array
(
[id] => 7188824
[patent_doc_number] => 20040084566
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2004-05-06
[patent_title] => 'Multi-nozzle grid missile propulsion system'
[patent_app_type] => new
[patent_app_number] => 10/288943
[patent_app_country] => US
[patent_app_date] => 2002-11-06
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 6
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[patent_no_of_words] => 9158
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[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0084/20040084566.pdf
[firstpage_image] =>[orig_patent_app_number] => 10288943
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/288943 | Multi-nozzle grid missile propulsion system | Nov 5, 2002 | Abandoned |
Array
(
[id] => 7147227
[patent_doc_number] => 20050023410
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2005-02-03
[patent_title] => 'Multipurpose airfoil assembly'
[patent_app_type] => utility
[patent_app_number] => 10/286290
[patent_app_country] => US
[patent_app_date] => 2002-11-01
[patent_effective_date] => 0000-00-00
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[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0023/20050023410.pdf
[firstpage_image] =>[orig_patent_app_number] => 10286290
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/286290 | Multipurpose airfoil assembly | Oct 31, 2002 | Abandoned |
Array
(
[id] => 7188826
[patent_doc_number] => 20040084567
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2004-05-06
[patent_title] => 'Guided parafoil system for delivering lightweight payloads'
[patent_app_type] => new
[patent_app_number] => 10/284699
[patent_app_country] => US
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[pdf_file] => publications/A1/0084/20040084567.pdf
[firstpage_image] =>[orig_patent_app_number] => 10284699
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/284699 | Guided parafoil system for delivering lightweight payloads | Oct 29, 2002 | Issued |
Array
(
[id] => 1224635
[patent_doc_number] => 06695258
[patent_country] => US
[patent_kind] => B1
[patent_issue_date] => 2004-02-24
[patent_title] => 'Kite device'
[patent_app_type] => B1
[patent_app_number] => 10/286922
[patent_app_country] => US
[patent_app_date] => 2002-10-25
[patent_effective_date] => 0000-00-00
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[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/695/06695258.pdf
[firstpage_image] =>[orig_patent_app_number] => 10286922
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/286922 | Kite device | Oct 24, 2002 | Issued |
Array
(
[id] => 6854062
[patent_doc_number] => 20030127563
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2003-07-10
[patent_title] => 'Differential pressure sensing release system'
[patent_app_type] => new
[patent_app_number] => 10/280271
[patent_app_country] => US
[patent_app_date] => 2002-10-25
[patent_effective_date] => 0000-00-00
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[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0127/20030127563.pdf
[firstpage_image] =>[orig_patent_app_number] => 10280271
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/280271 | Differential pressure sensing release system | Oct 24, 2002 | Abandoned |