
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] => 6316481
[patent_doc_number] => 20020195526
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2002-12-26
[patent_title] => 'Method and apparatus for boundary layer reattachment using piezoelectric synthetic jet actuators'
[patent_app_type] => new
[patent_app_number] => 10/104914
[patent_app_country] => US
[patent_app_date] => 2002-03-22
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
[patent_figures_cnt] => 5
[patent_no_of_words] => 5403
[patent_no_of_claims] => 20
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[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0195/20020195526.pdf
[firstpage_image] =>[orig_patent_app_number] => 10104914
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/104914 | Method and apparatus for boundary layer reattachment using piezoelectric synthetic jet actuators | Mar 21, 2002 | Issued |
Array
(
[id] => 1149758
[patent_doc_number] => 06761331
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2004-07-13
[patent_title] => 'Missile having deployment mechanism for stowable fins'
[patent_app_type] => B2
[patent_app_number] => 10/102032
[patent_app_country] => US
[patent_app_date] => 2002-03-19
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 8
[patent_figures_cnt] => 20
[patent_no_of_words] => 6771
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[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/761/06761331.pdf
[firstpage_image] =>[orig_patent_app_number] => 10102032
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/102032 | Missile having deployment mechanism for stowable fins | Mar 18, 2002 | Issued |
Array
(
[id] => 1311891
[patent_doc_number] => 06604705
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2003-08-12
[patent_title] => 'Control group for directional fins on missiles and/or shells'
[patent_app_type] => B2
[patent_app_number] => 10/101140
[patent_app_country] => US
[patent_app_date] => 2002-03-19
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
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[patent_no_of_words] => 2663
[patent_no_of_claims] => 9
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[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/604/06604705.pdf
[firstpage_image] =>[orig_patent_app_number] => 10101140
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/101140 | Control group for directional fins on missiles and/or shells | Mar 18, 2002 | Issued |
Array
(
[id] => 6794585
[patent_doc_number] => 20030173458
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2003-09-18
[patent_title] => 'Avionic door lock system'
[patent_app_type] => new
[patent_app_number] => 10/100227
[patent_app_country] => US
[patent_app_date] => 2002-03-18
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 3
[patent_no_of_words] => 3557
[patent_no_of_claims] => 23
[patent_no_of_ind_claims] => 4
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[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0173/20030173458.pdf
[firstpage_image] =>[orig_patent_app_number] => 10100227
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/100227 | Avionic door lock system | Mar 17, 2002 | Abandoned |
Array
(
[id] => 6794581
[patent_doc_number] => 20030173454
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2003-09-18
[patent_title] => 'All terrain aircraft (ATA)'
[patent_app_type] => new
[patent_app_number] => 10/097825
[patent_app_country] => US
[patent_app_date] => 2002-03-14
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 18
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[patent_no_of_words] => 3490
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[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0173/20030173454.pdf
[firstpage_image] =>[orig_patent_app_number] => 10097825
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/097825 | All terrain aircraft (ATA) | Mar 13, 2002 | Abandoned |
Array
(
[id] => 1351598
[patent_doc_number] => 06565044
[patent_country] => US
[patent_kind] => B1
[patent_issue_date] => 2003-05-20
[patent_title] => 'Combination solar sail and electrodynamic tether propulsion system'
[patent_app_type] => B1
[patent_app_number] => 10/097698
[patent_app_country] => US
[patent_app_date] => 2002-03-14
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
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[patent_no_of_words] => 3170
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[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/565/06565044.pdf
[firstpage_image] =>[orig_patent_app_number] => 10097698
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/097698 | Combination solar sail and electrodynamic tether propulsion system | Mar 13, 2002 | Issued |
Array
(
[id] => 1341666
[patent_doc_number] => 06571715
[patent_country] => US
[patent_kind] => B1
[patent_issue_date] => 2003-06-03
[patent_title] => 'Boot mechanism for complex projectile base survival'
[patent_app_type] => B1
[patent_app_number] => 10/095208
[patent_app_country] => US
[patent_app_date] => 2002-03-11
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
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[patent_no_of_words] => 3181
[patent_no_of_claims] => 16
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[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/571/06571715.pdf
[firstpage_image] =>[orig_patent_app_number] => 10095208
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/095208 | Boot mechanism for complex projectile base survival | Mar 10, 2002 | Issued |
Array
(
[id] => 6413848
[patent_doc_number] => 20020125373
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2002-09-12
[patent_title] => 'Rotation stabilizing device in a microgravitational rotating apparatus'
[patent_app_type] => new
[patent_app_number] => 10/092539
[patent_app_country] => US
[patent_app_date] => 2002-03-08
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 36
[patent_figures_cnt] => 36
[patent_no_of_words] => 23784
[patent_no_of_claims] => 25
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[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0125/20020125373.pdf
[firstpage_image] =>[orig_patent_app_number] => 10092539
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/092539 | Rotation stabilizing device in a microgravitational rotating apparatus | Mar 7, 2002 | Issued |
Array
(
[id] => 1154927
[patent_doc_number] => 06758443
[patent_country] => US
[patent_kind] => B1
[patent_issue_date] => 2004-07-06
[patent_title] => 'Method for observing and stabilizing electrodynamic tethers'
[patent_app_type] => B1
[patent_app_number] => 10/094312
[patent_app_country] => US
[patent_app_date] => 2002-03-07
[patent_effective_date] => 0000-00-00
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[pdf_file] => patents/06/758/06758443.pdf
[firstpage_image] =>[orig_patent_app_number] => 10094312
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/094312 | Method for observing and stabilizing electrodynamic tethers | Mar 6, 2002 | Issued |
Array
(
[id] => 5964318
[patent_doc_number] => 20020088899
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2002-07-11
[patent_title] => 'Flying object with a rotational effect'
[patent_app_type] => new
[patent_app_number] => 10/092671
[patent_app_country] => US
[patent_app_date] => 2002-03-07
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 2
[patent_figures_cnt] => 2
[patent_no_of_words] => 2437
[patent_no_of_claims] => 1
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[patent_words_short_claim] => 228
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[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0088/20020088899.pdf
[firstpage_image] =>[orig_patent_app_number] => 10092671
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/092671 | Flying object with a rotational effect | Mar 6, 2002 | Abandoned |
Array
(
[id] => 763772
[patent_doc_number] => 07008233
[patent_country] => US
[patent_kind] => B1
[patent_issue_date] => 2006-03-07
[patent_title] => 'Retractable panel interface cable device and method'
[patent_app_type] => utility
[patent_app_number] => 10/086590
[patent_app_country] => US
[patent_app_date] => 2002-02-28
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 8
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[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/07/008/07008233.pdf
[firstpage_image] =>[orig_patent_app_number] => 10086590
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/086590 | Retractable panel interface cable device and method | Feb 27, 2002 | Issued |
Array
(
[id] => 6364989
[patent_doc_number] => 20020117583
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2002-08-29
[patent_title] => 'Moving apparatus'
[patent_app_type] => new
[patent_app_number] => 10/085181
[patent_app_country] => US
[patent_app_date] => 2002-02-27
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[pdf_file] => publications/A1/0117/20020117583.pdf
[firstpage_image] =>[orig_patent_app_number] => 10085181
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/085181 | Fluttering wing-operated flying moving apparatus | Feb 26, 2002 | Issued |
Array
(
[id] => 6738097
[patent_doc_number] => 20030155465
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2003-08-21
[patent_title] => 'Flying machine using umbrella-type devices'
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[patent_app_number] => 10/078569
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[pdf_file] => publications/A1/0155/20030155465.pdf
[firstpage_image] =>[orig_patent_app_number] => 10078569
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/078569 | Flying machine using umbrella-type devices | Feb 18, 2002 | Abandoned |
Array
(
[id] => 502829
[patent_doc_number] => 07198223
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2007-04-03
[patent_title] => 'Ultralight coaxial rotor aircraft'
[patent_app_type] => utility
[patent_app_number] => 10/077169
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[pdf_file] => patents/07/198/07198223.pdf
[firstpage_image] =>[orig_patent_app_number] => 10077169
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/077169 | Ultralight coaxial rotor aircraft | Feb 13, 2002 | Issued |
Array
(
[id] => 6704220
[patent_doc_number] => 20030150954
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2003-08-14
[patent_title] => 'CONTROL SYSTEM FOR VERTICAL TAKE OFF AND LAND (VTOL) AIRCRAFT'
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[pdf_file] => publications/A1/0150/20030150954.pdf
[firstpage_image] =>[orig_patent_app_number] => 10074710
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/074710 | Control system for vertical take off and land (VTOL) aircraft | Feb 12, 2002 | Issued |
Array
(
[id] => 6704225
[patent_doc_number] => 20030150959
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2003-08-14
[patent_title] => 'SHOCK ISOLATION SYSTEM FOR SPACECRAFT FAIRING'
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[patent_app_number] => 10/073617
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[pdf_file] => publications/A1/0150/20030150959.pdf
[firstpage_image] =>[orig_patent_app_number] => 10073617
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/073617 | Shock isolation system for spacecraft fairing | Feb 10, 2002 | Issued |
Array
(
[id] => 1294425
[patent_doc_number] => 06619178
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[patent_kind] => B1
[patent_issue_date] => 2003-09-16
[patent_title] => 'Method for launching counter-measures, and arrangement for storing and launching counter-measures'
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[patent_app_number] => 09/937505
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[rel_patent_id] =>[rel_patent_doc_number] =>) 09/937505 | Method for launching counter-measures, and arrangement for storing and launching counter-measures | Feb 5, 2002 | Issued |
Array
(
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[patent_title] => 'Device for connecting movable parts with structural elements of airplanes or the like'
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Array
(
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[patent_title] => 'In-situ chemical composition monitor on wafer during plasma etching for defect control'
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[rel_patent_id] =>[rel_patent_doc_number] =>) 10/052173 | In-situ chemical composition monitor on wafer during plasma etching for defect control | Jan 16, 2002 | Issued |
Array
(
[id] => 6653315
[patent_doc_number] => 20030131916
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[patent_title] => 'Heat resistant pitot tube cover'
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[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0131/20030131916.pdf
[firstpage_image] =>[orig_patent_app_number] => 10047756
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/047756 | Heat resistant pitot tube cover | Jan 14, 2002 | Abandoned |