
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] => 7549321
[patent_doc_number] => 08061650
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2011-11-22
[patent_title] => 'Automatic control systems for aircraft auxiliary power units, and associated methods'
[patent_app_type] => utility
[patent_app_number] => 13/021422
[patent_app_country] => US
[patent_app_date] => 2011-02-04
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 4
[patent_no_of_words] => 3486
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[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/08/061/08061650.pdf
[firstpage_image] =>[orig_patent_app_number] => 13021422
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/021422 | Automatic control systems for aircraft auxiliary power units, and associated methods | Feb 3, 2011 | Issued |
Array
(
[id] => 7790691
[patent_doc_number] => 20120052247
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2012-03-01
[patent_title] => 'COMPOSITE STRUCTURES HAVING INTEGRATED STIFFENERS WITH SMOOTH RUNOUTS AND METHOD OF MAKING THE SAME'
[patent_app_type] => utility
[patent_app_number] => 13/012162
[patent_app_country] => US
[patent_app_date] => 2011-01-24
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 15
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[patent_no_of_words] => 7015
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[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0052/20120052247.pdf
[firstpage_image] =>[orig_patent_app_number] => 13012162
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/012162 | Composite structures having integrated stiffeners with smooth runouts and method of making the same | Jan 23, 2011 | Issued |
Array
(
[id] => 8643004
[patent_doc_number] => 08367992
[patent_country] => US
[patent_kind] => B1
[patent_issue_date] => 2013-02-05
[patent_title] => 'Aircraft, missile, projectile, or underwater vehicle with reconfigurable control surfaces'
[patent_app_type] => utility
[patent_app_number] => 12/977519
[patent_app_country] => US
[patent_app_date] => 2010-12-23
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 6
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[patent_no_of_words] => 5079
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[rel_patent_id] =>[rel_patent_doc_number] =>) 12/977519 | Aircraft, missile, projectile, or underwater vehicle with reconfigurable control surfaces | Dec 22, 2010 | Issued |
Array
(
[id] => 8624283
[patent_doc_number] => 08356775
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2013-01-22
[patent_title] => 'Space object deployment system and method'
[patent_app_type] => utility
[patent_app_number] => 12/965628
[patent_app_country] => US
[patent_app_date] => 2010-12-10
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 6
[patent_figures_cnt] => 8
[patent_no_of_words] => 4923
[patent_no_of_claims] => 10
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[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 12965628
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/965628 | Space object deployment system and method | Dec 9, 2010 | Issued |
Array
(
[id] => 8388402
[patent_doc_number] => 08265807
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2012-09-11
[patent_title] => 'Automatic takeoff and landing apparatus for aircraft, and methods for performing an automatic takeoff and an automatic landing of an aircraft'
[patent_app_type] => utility
[patent_app_number] => 12/954244
[patent_app_country] => US
[patent_app_date] => 2010-11-24
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 8
[patent_figures_cnt] => 11
[patent_no_of_words] => 7312
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[patent_words_short_claim] => 196
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[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 12954244
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/954244 | Automatic takeoff and landing apparatus for aircraft, and methods for performing an automatic takeoff and an automatic landing of an aircraft | Nov 23, 2010 | Issued |
Array
(
[id] => 8801039
[patent_doc_number] => 08439308
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2013-05-14
[patent_title] => 'Spring loaded pressure relief door'
[patent_app_type] => utility
[patent_app_number] => 12/927659
[patent_app_country] => US
[patent_app_date] => 2010-11-19
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
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[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 12927659
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/927659 | Spring loaded pressure relief door | Nov 18, 2010 | Issued |
Array
(
[id] => 8420356
[patent_doc_number] => 08276840
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2012-10-02
[patent_title] => 'Fail-operational multiple lifting-rotor aircraft'
[patent_app_type] => utility
[patent_app_number] => 12/944611
[patent_app_country] => US
[patent_app_date] => 2010-11-11
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 3
[patent_no_of_words] => 3291
[patent_no_of_claims] => 10
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[patent_words_short_claim] => 109
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 12944611
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/944611 | Fail-operational multiple lifting-rotor aircraft | Nov 10, 2010 | Issued |
Array
(
[id] => 9245760
[patent_doc_number] => 08610042
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2013-12-17
[patent_title] => 'Pyrotechnic fin deployment and retention mechanism'
[patent_app_type] => utility
[patent_app_number] => 12/927275
[patent_app_country] => US
[patent_app_date] => 2010-11-10
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 8
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[patent_no_of_words] => 3985
[patent_no_of_claims] => 4
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[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 12927275
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/927275 | Pyrotechnic fin deployment and retention mechanism | Nov 9, 2010 | Issued |
Array
(
[id] => 8189912
[patent_doc_number] => 08183508
[patent_country] => US
[patent_kind] => B1
[patent_issue_date] => 2012-05-22
[patent_title] => 'Pyrotechnic fin deployment and retention mechanism'
[patent_app_type] => utility
[patent_app_number] => 12/927310
[patent_app_country] => US
[patent_app_date] => 2010-11-10
[patent_effective_date] => 0000-00-00
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[pdf_file] => patents/08/183/08183508.pdf
[firstpage_image] =>[orig_patent_app_number] => 12927310
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/927310 | Pyrotechnic fin deployment and retention mechanism | Nov 9, 2010 | Issued |
Array
(
[id] => 7558688
[patent_doc_number] => 20110272519
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2011-11-10
[patent_title] => 'Aircraft with Helicopter Rotor, Thrust Generator and Assymetric Wing Configuration'
[patent_app_type] => utility
[patent_app_number] => 12/940459
[patent_app_country] => US
[patent_app_date] => 2010-11-05
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 13
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[patent_no_of_words] => 10281
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[pdf_file] => publications/A1/0272/20110272519.pdf
[firstpage_image] =>[orig_patent_app_number] => 12940459
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/940459 | Aircraft with helicopter rotor, thrust generator and assymetric wing configuration | Nov 4, 2010 | Issued |
Array
(
[id] => 9098067
[patent_doc_number] => 08561937
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2013-10-22
[patent_title] => 'Unmanned aerial vehicle'
[patent_app_type] => utility
[patent_app_number] => 12/906096
[patent_app_country] => US
[patent_app_date] => 2010-10-17
[patent_effective_date] => 0000-00-00
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[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 12906096
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/906096 | Unmanned aerial vehicle | Oct 16, 2010 | Issued |
Array
(
[id] => 8801044
[patent_doc_number] => 08439313
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2013-05-14
[patent_title] => 'Forward swept winglet'
[patent_app_type] => utility
[patent_app_number] => 12/905382
[patent_app_country] => US
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[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 12905382
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/905382 | Forward swept winglet | Oct 14, 2010 | Issued |
Array
(
[id] => 7544124
[patent_doc_number] => 08052088
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[patent_kind] => B2
[patent_issue_date] => 2011-11-08
[patent_title] => 'Injection-molded window panel and related methods'
[patent_app_type] => utility
[patent_app_number] => 12/904547
[patent_app_country] => US
[patent_app_date] => 2010-10-14
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[pdf_file] => patents/08/052/08052088.pdf
[firstpage_image] =>[orig_patent_app_number] => 12904547
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/904547 | Injection-molded window panel and related methods | Oct 13, 2010 | Issued |
Array
(
[id] => 6192798
[patent_doc_number] => 20110024552
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2011-02-03
[patent_title] => 'Anhedral Tip Blades for Tiltrotor Aircraft'
[patent_app_type] => utility
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[pdf_file] => publications/A1/0024/20110024552.pdf
[firstpage_image] =>[orig_patent_app_number] => 12903928
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/903928 | Anhedral tip blades for tiltrotor aircraft | Oct 12, 2010 | Issued |
Array
(
[id] => 6183739
[patent_doc_number] => 20110168835
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2011-07-14
[patent_title] => 'Three Wing, Six Tilt-Propulsion Units, VTOL Aircraft'
[patent_app_type] => utility
[patent_app_number] => 12/900790
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[firstpage_image] =>[orig_patent_app_number] => 12900790
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/900790 | Three wing, six tilt-propulsion units, VTOL aircraft | Oct 7, 2010 | Issued |
Array
(
[id] => 6026527
[patent_doc_number] => 20110079679
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2011-04-07
[patent_title] => 'DEVICE FOR LOCKING AN ENGINE ON AN AIRCRAFT PYLON'
[patent_app_type] => utility
[patent_app_number] => 12/894726
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[pdf_file] => publications/A1/0079/20110079679.pdf
[firstpage_image] =>[orig_patent_app_number] => 12894726
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/894726 | Device for locking an engine on an aircraft pylon | Sep 29, 2010 | Issued |
Array
(
[id] => 8434271
[patent_doc_number] => 08282037
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2012-10-09
[patent_title] => 'Nacelle flow assembly'
[patent_app_type] => utility
[patent_app_number] => 12/894505
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[rel_patent_id] =>[rel_patent_doc_number] =>) 12/894505 | Nacelle flow assembly | Sep 29, 2010 | Issued |
Array
(
[id] => 6026525
[patent_doc_number] => 20110079677
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2011-04-07
[patent_title] => 'Ornithopter'
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[firstpage_image] =>[orig_patent_app_number] => 12924592
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/924592 | Ornithopter | Sep 29, 2010 | Abandoned |
Array
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[id] => 8919547
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[patent_issue_date] => 2013-07-16
[patent_title] => 'Passive ejection seat arm flail restraint apparatus and method'
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[rel_patent_id] =>[rel_patent_doc_number] =>) 12/893217 | Passive ejection seat arm flail restraint apparatus and method | Sep 28, 2010 | Issued |
Array
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[patent_title] => 'Dynamically controlled cross flow instability inhibiting assembly'
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[firstpage_image] =>[orig_patent_app_number] => 12893618
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/893618 | Dynamically controlled cross flow instability inhibiting assembly | Sep 28, 2010 | Issued |