
Joseph W. Sanderson
Examiner (ID: 8781, Phone: (571)272-6337 , Office: P/3644 )
| Most Active Art Unit | 3644 |
| Art Unit(s) | 3619, 3644 |
| Total Applications | 1179 |
| Issued Applications | 870 |
| Pending Applications | 83 |
| Abandoned Applications | 244 |
Applications
| Application number | Title of the application | Filing Date | Status |
|---|---|---|---|
Array
(
[id] => 5048899
[patent_doc_number] => 20070029443
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2007-02-08
[patent_title] => 'Cover for an aircraft structure'
[patent_app_type] => utility
[patent_app_number] => 11/581543
[patent_app_country] => US
[patent_app_date] => 2006-10-16
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 7
[patent_figures_cnt] => 7
[patent_no_of_words] => 3405
[patent_no_of_claims] => 12
[patent_no_of_ind_claims] => 2
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[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0029/20070029443.pdf
[firstpage_image] =>[orig_patent_app_number] => 11581543
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/581543 | Cover for an aircraft structure | Oct 15, 2006 | Abandoned |
Array
(
[id] => 6113816
[patent_doc_number] => 20110073705
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2011-03-31
[patent_title] => 'DRIVE DEVICE FOR PROJECTILE FINS'
[patent_app_type] => utility
[patent_app_number] => 11/528377
[patent_app_country] => US
[patent_app_date] => 2006-09-28
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 6
[patent_figures_cnt] => 6
[patent_no_of_words] => 2560
[patent_no_of_claims] => 13
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[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0073/20110073705.pdf
[firstpage_image] =>[orig_patent_app_number] => 11528377
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/528377 | Drive device for projectile fins | Sep 27, 2006 | Issued |
Array
(
[id] => 4714872
[patent_doc_number] => 20080237394
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2008-10-02
[patent_title] => 'Engine Mounting Structure Interposed Between an Aircraft Wing System and Said Engine'
[patent_app_type] => utility
[patent_app_number] => 12/065837
[patent_app_country] => US
[patent_app_date] => 2006-09-26
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 4
[patent_no_of_words] => 3151
[patent_no_of_claims] => 10
[patent_no_of_ind_claims] => 1
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[patent_maintenance] => 1
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[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0237/20080237394.pdf
[firstpage_image] =>[orig_patent_app_number] => 12065837
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/065837 | Engine mounting structure interposed between an aircraft wing system and said engine | Sep 25, 2006 | Issued |
Array
(
[id] => 4493381
[patent_doc_number] => 07918417
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2011-04-05
[patent_title] => 'Undercarriage with anticrash and antiresonance skids for a rotary wing aircraft, and an aircraft'
[patent_app_type] => utility
[patent_app_number] => 11/526573
[patent_app_country] => US
[patent_app_date] => 2006-09-26
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 1
[patent_figures_cnt] => 6
[patent_no_of_words] => 6642
[patent_no_of_claims] => 20
[patent_no_of_ind_claims] => 3
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[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/07/918/07918417.pdf
[firstpage_image] =>[orig_patent_app_number] => 11526573
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/526573 | Undercarriage with anticrash and antiresonance skids for a rotary wing aircraft, and an aircraft | Sep 25, 2006 | Issued |
Array
(
[id] => 9708754
[patent_doc_number] => 08833310
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2014-09-16
[patent_title] => 'Tether device, system, and method'
[patent_app_type] => utility
[patent_app_number] => 11/534973
[patent_app_country] => US
[patent_app_date] => 2006-09-25
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 16
[patent_no_of_words] => 5529
[patent_no_of_claims] => 13
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[patent_maintenance] => 1
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[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 11534973
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/534973 | Tether device, system, and method | Sep 24, 2006 | Issued |
Array
(
[id] => 8531962
[patent_doc_number] => 08308112
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2012-11-13
[patent_title] => 'Plasma actuators for drag reduction on wings, nacelles and/or fuselage of vertical take-off and landing aircraft'
[patent_app_type] => utility
[patent_app_number] => 11/519770
[patent_app_country] => US
[patent_app_date] => 2006-09-13
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 41
[patent_figures_cnt] => 56
[patent_no_of_words] => 8205
[patent_no_of_claims] => 23
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[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 11519770
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/519770 | Plasma actuators for drag reduction on wings, nacelles and/or fuselage of vertical take-off and landing aircraft | Sep 12, 2006 | Issued |
Array
(
[id] => 5104226
[patent_doc_number] => 20070063101
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2007-03-22
[patent_title] => 'Support device for a galley'
[patent_app_type] => utility
[patent_app_number] => 11/519741
[patent_app_country] => US
[patent_app_date] => 2006-09-12
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
[patent_figures_cnt] => 5
[patent_no_of_words] => 2968
[patent_no_of_claims] => 11
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 0
[patent_maintenance] => 1
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[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0063/20070063101.pdf
[firstpage_image] =>[orig_patent_app_number] => 11519741
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/519741 | Support device for a galley | Sep 11, 2006 | Issued |
Array
(
[id] => 139603
[patent_doc_number] => 07690598
[patent_country] => US
[patent_kind] => B1
[patent_issue_date] => 2010-04-06
[patent_title] => 'Aircraft exhaust vent assembly'
[patent_app_type] => utility
[patent_app_number] => 11/518971
[patent_app_country] => US
[patent_app_date] => 2006-09-11
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 6
[patent_no_of_words] => 4738
[patent_no_of_claims] => 17
[patent_no_of_ind_claims] => 4
[patent_words_short_claim] => 211
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/07/690/07690598.pdf
[firstpage_image] =>[orig_patent_app_number] => 11518971
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/518971 | Aircraft exhaust vent assembly | Sep 10, 2006 | Issued |
Array
(
[id] => 4952455
[patent_doc_number] => 20080185479
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2008-08-07
[patent_title] => 'Window Arrangement for Installing Larger Aircraft Windows'
[patent_app_type] => utility
[patent_app_number] => 12/066919
[patent_app_country] => US
[patent_app_date] => 2006-09-05
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 9
[patent_figures_cnt] => 9
[patent_no_of_words] => 3370
[patent_no_of_claims] => 13
[patent_no_of_ind_claims] => 2
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[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0185/20080185479.pdf
[firstpage_image] =>[orig_patent_app_number] => 12066919
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/066919 | Window arrangement for installing larger aircraft windows | Sep 4, 2006 | Issued |
Array
(
[id] => 227907
[patent_doc_number] => 07600717
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2009-10-13
[patent_title] => 'Aircraft wings and fuel tanks'
[patent_app_type] => utility
[patent_app_number] => 11/469071
[patent_app_country] => US
[patent_app_date] => 2006-08-31
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
[patent_figures_cnt] => 8
[patent_no_of_words] => 8833
[patent_no_of_claims] => 28
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 311
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/07/600/07600717.pdf
[firstpage_image] =>[orig_patent_app_number] => 11469071
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/469071 | Aircraft wings and fuel tanks | Aug 30, 2006 | Issued |
Array
(
[id] => 858700
[patent_doc_number] => 07370835
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2008-05-13
[patent_title] => 'Platform and system for mass storage and transfer in space'
[patent_app_type] => utility
[patent_app_number] => 11/468568
[patent_app_country] => US
[patent_app_date] => 2006-08-30
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 6
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[patent_no_of_words] => 5955
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[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/07/370/07370835.pdf
[firstpage_image] =>[orig_patent_app_number] => 11468568
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/468568 | Platform and system for mass storage and transfer in space | Aug 29, 2006 | Issued |
Array
(
[id] => 4968343
[patent_doc_number] => 20070108345
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2007-05-17
[patent_title] => 'Launch and recovery system for unmanned aerial vehicles'
[patent_app_type] => utility
[patent_app_number] => 11/510920
[patent_app_country] => US
[patent_app_date] => 2006-08-28
[patent_effective_date] => 0000-00-00
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[pdf_file] => publications/A1/0108/20070108345.pdf
[firstpage_image] =>[orig_patent_app_number] => 11510920
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/510920 | Launch and recovery system for unmanned aerial vehicles | Aug 27, 2006 | Issued |
Array
(
[id] => 4941545
[patent_doc_number] => 20080078868
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2008-04-03
[patent_title] => 'System and method for a power-assisted compartment'
[patent_app_type] => utility
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[patent_app_country] => US
[patent_app_date] => 2006-08-25
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[pdf_file] => publications/A1/0078/20080078868.pdf
[firstpage_image] =>[orig_patent_app_number] => 11510779
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/510779 | System and method for a power-assisted compartment | Aug 24, 2006 | Issued |
Array
(
[id] => 5144681
[patent_doc_number] => 20070044735
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2007-03-01
[patent_title] => 'HIP LIFT HARNESS'
[patent_app_type] => utility
[patent_app_number] => 11/467460
[patent_app_country] => US
[patent_app_date] => 2006-08-25
[patent_effective_date] => 0000-00-00
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[pdf_file] => publications/A1/0044/20070044735.pdf
[firstpage_image] =>[orig_patent_app_number] => 11467460
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/467460 | Hip lift harness | Aug 24, 2006 | Issued |
Array
(
[id] => 5116640
[patent_doc_number] => 20070138353
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2007-06-21
[patent_title] => 'LINE HOLDER IN AN AIRCRAFT'
[patent_app_type] => utility
[patent_app_number] => 11/466234
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[patent_app_date] => 2006-08-22
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[pdf_file] => publications/A1/0138/20070138353.pdf
[firstpage_image] =>[orig_patent_app_number] => 11466234
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/466234 | Line holder in an aircraft | Aug 21, 2006 | Issued |
Array
(
[id] => 5145423
[patent_doc_number] => 20070045477
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2007-03-01
[patent_title] => 'Aircraft wing slat'
[patent_app_type] => utility
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[patent_app_country] => US
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[pdf_file] => publications/A1/0045/20070045477.pdf
[firstpage_image] =>[orig_patent_app_number] => 11507373
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/507373 | Aircraft wing slat | Aug 20, 2006 | Issued |
Array
(
[id] => 9237571
[patent_doc_number] => 08602356
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2013-12-10
[patent_title] => 'Framework wing box for a wing'
[patent_app_type] => utility
[patent_app_number] => 11/990578
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[rel_patent_id] =>[rel_patent_doc_number] =>) 11/990578 | Framework wing box for a wing | Aug 16, 2006 | Issued |
Array
(
[id] => 6415563
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[patent_issue_date] => 2010-11-04
[patent_title] => 'Fail-operational multiple lifting-rotor aircraft'
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[firstpage_image] =>[orig_patent_app_number] => 11506044
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/506044 | Fail-operational multiple lifting-rotor aircraft | Aug 15, 2006 | Abandoned |
Array
(
[id] => 577368
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[patent_title] => 'Compound aircraft control system and method'
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[firstpage_image] =>[orig_patent_app_number] => 11505235
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/505235 | Compound aircraft control system and method | Aug 15, 2006 | Issued |
Array
(
[id] => 6442061
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[patent_title] => 'Unmanned Aerial Surveillance Device'
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[pdf_file] => publications/A1/0282/20100282897.pdf
[firstpage_image] =>[orig_patent_app_number] => 11464973
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/464973 | Unmanned Aerial Surveillance Device | Aug 15, 2006 | Abandoned |