
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] => 7370667
[patent_doc_number] => 20040079834
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2004-04-29
[patent_title] => 'ACTIVE SYSTEM FOR WIDE AREA SUPPRESSION OF ENGINE VORTEX'
[patent_app_type] => new
[patent_app_number] => 10/280411
[patent_app_country] => US
[patent_app_date] => 2002-10-25
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 10
[patent_figures_cnt] => 10
[patent_no_of_words] => 3346
[patent_no_of_claims] => 23
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 80
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0079/20040079834.pdf
[firstpage_image] =>[orig_patent_app_number] => 10280411
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/280411 | Active system for wide area suppression of engine vortex | Oct 24, 2002 | Issued |
Array
(
[id] => 351699
[patent_doc_number] => 07490793
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2009-02-17
[patent_title] => 'Wireless landing gear monitoring system'
[patent_app_type] => utility
[patent_app_number] => 10/273659
[patent_app_country] => US
[patent_app_date] => 2002-10-18
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 8
[patent_no_of_words] => 3713
[patent_no_of_claims] => 16
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 158
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/07/490/07490793.pdf
[firstpage_image] =>[orig_patent_app_number] => 10273659
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/273659 | Wireless landing gear monitoring system | Oct 17, 2002 | Issued |
Array
(
[id] => 6718541
[patent_doc_number] => 20030052228
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2003-03-20
[patent_title] => 'Tri-body aircraft and methods for their manufacture'
[patent_app_type] => new
[patent_app_number] => 10/271631
[patent_app_country] => US
[patent_app_date] => 2002-10-15
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 6
[patent_figures_cnt] => 6
[patent_no_of_words] => 4697
[patent_no_of_claims] => 52
[patent_no_of_ind_claims] => 5
[patent_words_short_claim] => 77
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0052/20030052228.pdf
[firstpage_image] =>[orig_patent_app_number] => 10271631
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/271631 | Tri-body aircraft and methods for their manufacture | Oct 14, 2002 | Issued |
Array
(
[id] => 6686242
[patent_doc_number] => 20030029965
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2003-02-13
[patent_title] => 'Telescopic vertical take-off aircraft'
[patent_app_type] => new
[patent_app_number] => 10/265378
[patent_app_country] => US
[patent_app_date] => 2002-10-07
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 15
[patent_figures_cnt] => 15
[patent_no_of_words] => 3161
[patent_no_of_claims] => 23
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 307
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0029/20030029965.pdf
[firstpage_image] =>[orig_patent_app_number] => 10265378
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/265378 | Telescopic vertical take-off aircraft | Oct 6, 2002 | Issued |
Array
(
[id] => 1120310
[patent_doc_number] => 06793173
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2004-09-21
[patent_title] => 'Automatic control device for a helicopter and automatic control system comprising such a device'
[patent_app_type] => B2
[patent_app_number] => 10/264256
[patent_app_country] => US
[patent_app_date] => 2002-10-04
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 4
[patent_no_of_words] => 5868
[patent_no_of_claims] => 9
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 208
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/793/06793173.pdf
[firstpage_image] =>[orig_patent_app_number] => 10264256
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/264256 | Automatic control device for a helicopter and automatic control system comprising such a device | Oct 3, 2002 | Issued |
Array
(
[id] => 6858819
[patent_doc_number] => 20030089827
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2003-05-15
[patent_title] => 'Control device and method for emergency opening of an aircraft evacuation door'
[patent_app_type] => new
[patent_app_number] => 10/264610
[patent_app_country] => US
[patent_app_date] => 2002-10-03
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
[patent_figures_cnt] => 5
[patent_no_of_words] => 3864
[patent_no_of_claims] => 12
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 47
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0089/20030089827.pdf
[firstpage_image] =>[orig_patent_app_number] => 10264610
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/264610 | Control device and method for emergency opening of an aircraft evacuation door | Oct 2, 2002 | Issued |
Array
(
[id] => 1084598
[patent_doc_number] => 06830217
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2004-12-14
[patent_title] => 'Integrated cockpit door lock and access system'
[patent_app_type] => B2
[patent_app_number] => 10/255916
[patent_app_country] => US
[patent_app_date] => 2002-09-26
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 10
[patent_figures_cnt] => 15
[patent_no_of_words] => 5757
[patent_no_of_claims] => 27
[patent_no_of_ind_claims] => 5
[patent_words_short_claim] => 174
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/830/06830217.pdf
[firstpage_image] =>[orig_patent_app_number] => 10255916
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/255916 | Integrated cockpit door lock and access system | Sep 25, 2002 | Issued |
Array
(
[id] => 7278651
[patent_doc_number] => 20040061028
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2004-04-01
[patent_title] => 'METHOD OF OPERATING A SATELLITE FOR END-OF-LIFE MANEUVERS'
[patent_app_type] => new
[patent_app_number] => 10/255540
[patent_app_country] => US
[patent_app_date] => 2002-09-26
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 3
[patent_no_of_words] => 2260
[patent_no_of_claims] => 20
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 53
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0061/20040061028.pdf
[firstpage_image] =>[orig_patent_app_number] => 10255540
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/255540 | Method of operating a satellite for end-of-life maneuvers | Sep 25, 2002 | Issued |
Array
(
[id] => 6646029
[patent_doc_number] => 20030075642
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2003-04-24
[patent_title] => 'Internet linked environment data collection system and method'
[patent_app_type] => new
[patent_app_number] => 10/254510
[patent_app_country] => US
[patent_app_date] => 2002-09-26
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 24
[patent_figures_cnt] => 24
[patent_no_of_words] => 11666
[patent_no_of_claims] => 80
[patent_no_of_ind_claims] => 4
[patent_words_short_claim] => 40
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0075/20030075642.pdf
[firstpage_image] =>[orig_patent_app_number] => 10254510
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/254510 | Internet linked environment data collection system and method | Sep 25, 2002 | Abandoned |
Array
(
[id] => 6867552
[patent_doc_number] => 20030080241
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2003-05-01
[patent_title] => 'Air launch of payload carrying vehicle from a transport aircraft'
[patent_app_type] => new
[patent_app_number] => 10/256249
[patent_app_country] => US
[patent_app_date] => 2002-09-26
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 4
[patent_no_of_words] => 2435
[patent_no_of_claims] => 20
[patent_no_of_ind_claims] => 4
[patent_words_short_claim] => 66
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0080/20030080241.pdf
[firstpage_image] =>[orig_patent_app_number] => 10256249
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/256249 | Air launch of payload carrying vehicle from a transport aircraft | Sep 25, 2002 | Abandoned |
Array
(
[id] => 1302515
[patent_doc_number] => 06612521
[patent_country] => US
[patent_kind] => B1
[patent_issue_date] => 2003-09-02
[patent_title] => 'Safety pitot tube cover'
[patent_app_type] => B1
[patent_app_number] => 10/253301
[patent_app_country] => US
[patent_app_date] => 2002-09-24
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 6
[patent_no_of_words] => 2008
[patent_no_of_claims] => 9
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 101
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/612/06612521.pdf
[firstpage_image] =>[orig_patent_app_number] => 10253301
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/253301 | Safety pitot tube cover | Sep 23, 2002 | Issued |
Array
(
[id] => 7444311
[patent_doc_number] => 20040051002
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2004-03-18
[patent_title] => 'Environmental control system'
[patent_app_type] => new
[patent_app_number] => 10/246157
[patent_app_country] => US
[patent_app_date] => 2002-09-18
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 2
[patent_figures_cnt] => 2
[patent_no_of_words] => 2481
[patent_no_of_claims] => 14
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 173
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0051/20040051002.pdf
[firstpage_image] =>[orig_patent_app_number] => 10246157
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/246157 | Environmental control system | Sep 17, 2002 | Issued |
Array
(
[id] => 235645
[patent_doc_number] => 07594623
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2009-09-29
[patent_title] => 'Torsionally de-coupled engine mount system'
[patent_app_type] => utility
[patent_app_number] => 10/528213
[patent_app_country] => US
[patent_app_date] => 2002-09-17
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 9
[patent_figures_cnt] => 17
[patent_no_of_words] => 5884
[patent_no_of_claims] => 5
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 244
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/07/594/07594623.pdf
[firstpage_image] =>[orig_patent_app_number] => 10528213
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/528213 | Torsionally de-coupled engine mount system | Sep 16, 2002 | Issued |
Array
(
[id] => 7444297
[patent_doc_number] => 20040050999
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2004-03-18
[patent_title] => 'Active vibration control system'
[patent_app_type] => new
[patent_app_number] => 10/244583
[patent_app_country] => US
[patent_app_date] => 2002-09-16
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 16
[patent_figures_cnt] => 16
[patent_no_of_words] => 11725
[patent_no_of_claims] => 16
[patent_no_of_ind_claims] => 4
[patent_words_short_claim] => 76
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0050/20040050999.pdf
[firstpage_image] =>[orig_patent_app_number] => 10244583
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/244583 | Active vibration control system | Sep 15, 2002 | Issued |
Array
(
[id] => 1238577
[patent_doc_number] => 06682017
[patent_country] => US
[patent_kind] => B1
[patent_issue_date] => 2004-01-27
[patent_title] => 'Aircraft with a detachable passenger escape cabin and an aircraft with airbags'
[patent_app_type] => B1
[patent_app_number] => 10/220977
[patent_app_country] => US
[patent_app_date] => 2002-09-09
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 18
[patent_figures_cnt] => 44
[patent_no_of_words] => 7654
[patent_no_of_claims] => 8
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[patent_words_short_claim] => 419
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/682/06682017.pdf
[firstpage_image] =>[orig_patent_app_number] => 10220977
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/220977 | Aircraft with a detachable passenger escape cabin and an aircraft with airbags | Sep 8, 2002 | Issued |
Array
(
[id] => 7335334
[patent_doc_number] => 20040244334
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2004-12-09
[patent_title] => 'Composite material structure'
[patent_app_type] => new
[patent_app_number] => 10/487457
[patent_app_country] => US
[patent_app_date] => 2004-02-24
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 4
[patent_no_of_words] => 3661
[patent_no_of_claims] => 11
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 2
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0244/20040244334.pdf
[firstpage_image] =>[orig_patent_app_number] => 10487457
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/487457 | Composite material structure | Sep 5, 2002 | Issued |
Array
(
[id] => 1108409
[patent_doc_number] => 06805320
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2004-10-19
[patent_title] => 'Aircraft landing gear with highly offset strut pivot axis'
[patent_app_type] => B2
[patent_app_number] => 10/220526
[patent_app_country] => US
[patent_app_date] => 2002-08-28
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
[patent_figures_cnt] => 14
[patent_no_of_words] => 4466
[patent_no_of_claims] => 13
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[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/805/06805320.pdf
[firstpage_image] =>[orig_patent_app_number] => 10220526
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/220526 | Aircraft landing gear with highly offset strut pivot axis | Aug 27, 2002 | Issued |
Array
(
[id] => 1145838
[patent_doc_number] => 06766987
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2004-07-27
[patent_title] => 'Satellite system and method of deploying same'
[patent_app_type] => B2
[patent_app_number] => 10/230424
[patent_app_country] => US
[patent_app_date] => 2002-08-28
[patent_effective_date] => 0000-00-00
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[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/766/06766987.pdf
[firstpage_image] =>[orig_patent_app_number] => 10230424
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/230424 | Satellite system and method of deploying same | Aug 27, 2002 | Issued |
Array
(
[id] => 1251525
[patent_doc_number] => 06669137
[patent_country] => US
[patent_kind] => B1
[patent_issue_date] => 2003-12-30
[patent_title] => 'Air vehicle having rotor/scissors wing'
[patent_app_type] => B1
[patent_app_number] => 10/227955
[patent_app_country] => US
[patent_app_date] => 2002-08-26
[patent_effective_date] => 0000-00-00
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[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/669/06669137.pdf
[firstpage_image] =>[orig_patent_app_number] => 10227955
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/227955 | Air vehicle having rotor/scissors wing | Aug 25, 2002 | Issued |
Array
(
[id] => 7379281
[patent_doc_number] => 20040035979
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2004-02-26
[patent_title] => 'Integrally stiffened axial load carrying skin panels for primary aircraft structure and closed loop manufacturing methods for making the same'
[patent_app_type] => new
[patent_app_number] => 10/226922
[patent_app_country] => US
[patent_app_date] => 2002-08-23
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 11
[patent_figures_cnt] => 11
[patent_no_of_words] => 8026
[patent_no_of_claims] => 33
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[patent_words_short_claim] => 14
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0035/20040035979.pdf
[firstpage_image] =>[orig_patent_app_number] => 10226922
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/226922 | Integrally stiffened axial load carrying skin panels for primary aircraft structure and closed loop manufacturing methods for making the same | Aug 22, 2002 | Abandoned |