
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] => 8150760
[patent_doc_number] => 08167244
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2012-05-01
[patent_title] => 'Class divider for aircraft cabin'
[patent_app_type] => utility
[patent_app_number] => 12/166004
[patent_app_country] => US
[patent_app_date] => 2008-07-01
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 4
[patent_no_of_words] => 2165
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[patent_words_short_claim] => 168
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/08/167/08167244.pdf
[firstpage_image] =>[orig_patent_app_number] => 12166004
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/166004 | Class divider for aircraft cabin | Jun 30, 2008 | Issued |
Array
(
[id] => 4457116
[patent_doc_number] => 07878456
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2011-02-01
[patent_title] => 'Protective shield assembly for space optics and associated methods'
[patent_app_type] => utility
[patent_app_number] => 12/137981
[patent_app_country] => US
[patent_app_date] => 2008-06-12
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
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[patent_no_of_words] => 5072
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[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/07/878/07878456.pdf
[firstpage_image] =>[orig_patent_app_number] => 12137981
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/137981 | Protective shield assembly for space optics and associated methods | Jun 11, 2008 | Issued |
Array
(
[id] => 9748595
[patent_doc_number] => 08840060
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2014-09-23
[patent_title] => 'Actuating device for a locking system of an engine nacelle'
[patent_app_type] => utility
[patent_app_number] => 12/674184
[patent_app_country] => US
[patent_app_date] => 2008-06-12
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 6
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[patent_no_of_words] => 4015
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[patent_maintenance] => 1
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[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 12674184
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/674184 | Actuating device for a locking system of an engine nacelle | Jun 11, 2008 | Issued |
Array
(
[id] => 5327658
[patent_doc_number] => 20090108135
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2009-04-30
[patent_title] => 'Inflatable wing flight vehicle'
[patent_app_type] => utility
[patent_app_number] => 12/157600
[patent_app_country] => US
[patent_app_date] => 2008-06-11
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 7
[patent_figures_cnt] => 7
[patent_no_of_words] => 7414
[patent_no_of_claims] => 17
[patent_no_of_ind_claims] => 3
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[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0108/20090108135.pdf
[firstpage_image] =>[orig_patent_app_number] => 12157600
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/157600 | Inflatable wing flight vehicle | Jun 10, 2008 | Issued |
Array
(
[id] => 5488077
[patent_doc_number] => 20090289148
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2009-11-26
[patent_title] => 'Faired tether for wind power generation systems'
[patent_app_type] => utility
[patent_app_number] => 12/154685
[patent_app_country] => US
[patent_app_date] => 2008-05-23
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 20
[patent_figures_cnt] => 20
[patent_no_of_words] => 4990
[patent_no_of_claims] => 21
[patent_no_of_ind_claims] => 1
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[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0289/20090289148.pdf
[firstpage_image] =>[orig_patent_app_number] => 12154685
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/154685 | Faired tether for wind power generation systems | May 22, 2008 | Abandoned |
Array
(
[id] => 8281494
[patent_doc_number] => 08215589
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2012-07-10
[patent_title] => 'Reversible space plane'
[patent_app_type] => utility
[patent_app_number] => 12/154185
[patent_app_country] => US
[patent_app_date] => 2008-05-19
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 8
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[patent_no_of_words] => 7344
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[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 12154185
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/154185 | Reversible space plane | May 18, 2008 | Issued |
Array
(
[id] => 8384637
[patent_doc_number] => 08262031
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2012-09-11
[patent_title] => 'Co-flow jet aircraft'
[patent_app_type] => utility
[patent_app_number] => 12/119193
[patent_app_country] => US
[patent_app_date] => 2008-05-12
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 21
[patent_figures_cnt] => 24
[patent_no_of_words] => 10139
[patent_no_of_claims] => 20
[patent_no_of_ind_claims] => 2
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[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 12119193
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/119193 | Co-flow jet aircraft | May 11, 2008 | Issued |
Array
(
[id] => 4638203
[patent_doc_number] => 08016228
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2011-09-13
[patent_title] => 'Combined fuel cell aircraft auxiliary power unit and environmental control system'
[patent_app_type] => utility
[patent_app_number] => 12/106799
[patent_app_country] => US
[patent_app_date] => 2008-04-21
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 5
[patent_no_of_words] => 3227
[patent_no_of_claims] => 14
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[patent_words_short_claim] => 99
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/08/016/08016228.pdf
[firstpage_image] =>[orig_patent_app_number] => 12106799
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/106799 | Combined fuel cell aircraft auxiliary power unit and environmental control system | Apr 20, 2008 | Issued |
Array
(
[id] => 9007821
[patent_doc_number] => 08523110
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2013-09-03
[patent_title] => 'Door frame component of cast titanium and structural fuselage part'
[patent_app_type] => utility
[patent_app_number] => 12/058626
[patent_app_country] => US
[patent_app_date] => 2008-03-28
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
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[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 12058626
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/058626 | Door frame component of cast titanium and structural fuselage part | Mar 27, 2008 | Issued |
Array
(
[id] => 5518328
[patent_doc_number] => 20090026309
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2009-01-29
[patent_title] => 'Aircraft'
[patent_app_type] => utility
[patent_app_number] => 12/056463
[patent_app_country] => US
[patent_app_date] => 2008-03-27
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 3
[patent_no_of_words] => 1693
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[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0026/20090026309.pdf
[firstpage_image] =>[orig_patent_app_number] => 12056463
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/056463 | Aircraft | Mar 26, 2008 | Abandoned |
Array
(
[id] => 4462049
[patent_doc_number] => 07880125
[patent_country] => US
[patent_kind] => B1
[patent_issue_date] => 2011-02-01
[patent_title] => 'Aircraft, missile, projectile or underwater vehicle with reconfigurable control surfaces'
[patent_app_type] => utility
[patent_app_number] => 12/077447
[patent_app_country] => US
[patent_app_date] => 2008-03-19
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 6
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[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/07/880/07880125.pdf
[firstpage_image] =>[orig_patent_app_number] => 12077447
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/077447 | Aircraft, missile, projectile or underwater vehicle with reconfigurable control surfaces | Mar 18, 2008 | Issued |
Array
(
[id] => 8373910
[patent_doc_number] => 08256702
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2012-09-04
[patent_title] => 'Aircraft landing gear provided with at least one noise reducing means'
[patent_app_type] => utility
[patent_app_number] => 12/532387
[patent_app_country] => US
[patent_app_date] => 2008-03-18
[patent_effective_date] => 0000-00-00
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[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 12532387
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/532387 | Aircraft landing gear provided with at least one noise reducing means | Mar 17, 2008 | Issued |
Array
(
[id] => 5362242
[patent_doc_number] => 20090037036
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2009-02-05
[patent_title] => 'Automatic Control Systems for Aircraft Auxiliary Power Units, and Associated Methods'
[patent_app_type] => utility
[patent_app_number] => 12/047833
[patent_app_country] => US
[patent_app_date] => 2008-03-13
[patent_effective_date] => 0000-00-00
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[pdf_file] => publications/A1/0037/20090037036.pdf
[firstpage_image] =>[orig_patent_app_number] => 12047833
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/047833 | Automatic control systems for aircraft auxiliary power units, and associated methods | Mar 12, 2008 | Issued |
Array
(
[id] => 4816735
[patent_doc_number] => 20080223994
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2008-09-18
[patent_title] => 'MOVEABLE WINGS ON A FLYING/HOVERING VEHICLE'
[patent_app_type] => utility
[patent_app_number] => 12/045207
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[patent_app_date] => 2008-03-10
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[pdf_file] => publications/A1/0223/20080223994.pdf
[firstpage_image] =>[orig_patent_app_number] => 12045207
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/045207 | Moveable wings on a flying/hovering vehicle | Mar 9, 2008 | Issued |
Array
(
[id] => 4695286
[patent_doc_number] => 20080217470
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2008-09-11
[patent_title] => 'Modularized airplane structures and methods'
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[rel_patent_id] =>[rel_patent_doc_number] =>) 12/074737 | Modularized airplane structures and methods | Mar 5, 2008 | Issued |
Array
(
[id] => 8310214
[patent_doc_number] => 20120187235
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2012-07-26
[patent_title] => 'GUIDANCE CONTROL SYSTEM FOR PROJECTILES'
[patent_app_type] => utility
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[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 12042087
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/042087 | Guidance control system for projectiles | Mar 3, 2008 | Issued |
Array
(
[id] => 8541847
[patent_doc_number] => 08317133
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2012-11-27
[patent_title] => 'Aircraft floor and fuselage supplied with said floor'
[patent_app_type] => utility
[patent_app_number] => 12/041748
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[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 12041748
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/041748 | Aircraft floor and fuselage supplied with said floor | Mar 3, 2008 | Issued |
Array
(
[id] => 9243835
[patent_doc_number] => 08608112
[patent_country] => US
[patent_kind] => B1
[patent_issue_date] => 2013-12-17
[patent_title] => 'Modular programmable electronic initiation device for parachute disreefing or disconnect'
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[rel_patent_id] =>[rel_patent_doc_number] =>) 12/072812 | Modular programmable electronic initiation device for parachute disreefing or disconnect | Feb 27, 2008 | Issued |
Array
(
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Array
(
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[patent_title] => 'MULTI-RING SYSTEM FOR FUSELAGE BARREL FORMATION'
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[firstpage_image] =>[orig_patent_app_number] => 12033579
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/033579 | MULTI-RING SYSTEM FOR FUSELAGE BARREL FORMATION | Feb 18, 2008 | Abandoned |