
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] => 8165608
[patent_doc_number] => 20120104157
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2012-05-03
[patent_title] => 'ROTOR DRIVEN AUXILIARY POWER APPARATUS AND METHOD'
[patent_app_type] => utility
[patent_app_number] => 13/282938
[patent_app_country] => US
[patent_app_date] => 2011-10-27
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 25
[patent_figures_cnt] => 25
[patent_no_of_words] => 10700
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[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0104/20120104157.pdf
[firstpage_image] =>[orig_patent_app_number] => 13282938
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/282938 | Rotor driven auxiliary power apparatus and method | Oct 26, 2011 | Issued |
Array
(
[id] => 8165603
[patent_doc_number] => 20120104155
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2012-05-03
[patent_title] => 'TAIL JET APPARATUS AND METHOD FOR LOW SPEED YAW CONTROL OF A ROTORCRAFT'
[patent_app_type] => utility
[patent_app_number] => 13/282815
[patent_app_country] => US
[patent_app_date] => 2011-10-27
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 25
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[pdf_file] => publications/A1/0104/20120104155.pdf
[firstpage_image] =>[orig_patent_app_number] => 13282815
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/282815 | Tail jet apparatus and method for low speed yaw control of a rotorcraft | Oct 26, 2011 | Issued |
Array
(
[id] => 8165606
[patent_doc_number] => 20120104154
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2012-05-03
[patent_title] => 'TAIL FAN APPARATUS AND METHODS FOR LOW SPEED YAW CONTROL OF A ROTORCRAFT'
[patent_app_type] => utility
[patent_app_number] => 13/282749
[patent_app_country] => US
[patent_app_date] => 2011-10-27
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 25
[patent_figures_cnt] => 25
[patent_no_of_words] => 10891
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[pdf_file] => publications/A1/0104/20120104154.pdf
[firstpage_image] =>[orig_patent_app_number] => 13282749
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/282749 | Tail fan apparatus and method for low speed yaw control of a rotorcraft | Oct 26, 2011 | Issued |
Array
(
[id] => 8248752
[patent_doc_number] => 20120153073
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2012-06-21
[patent_title] => 'MISSION-ADAPTIVE ROTOR BLADE'
[patent_app_type] => utility
[patent_app_number] => 13/282877
[patent_app_country] => US
[patent_app_date] => 2011-10-27
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 10
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[patent_no_of_words] => 8710
[patent_no_of_claims] => 20
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[pdf_file] => publications/A1/0153/20120153073.pdf
[firstpage_image] =>[orig_patent_app_number] => 13282877
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/282877 | Mission-adaptive rotor blade | Oct 26, 2011 | Issued |
Array
(
[id] => 8165602
[patent_doc_number] => 20120104156
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2012-05-03
[patent_title] => 'USE OF AUXILIARY RUDDERS FOR YAW CONTROL AT LOW SPEED'
[patent_app_type] => utility
[patent_app_number] => 13/282985
[patent_app_country] => US
[patent_app_date] => 2011-10-27
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 25
[patent_figures_cnt] => 25
[patent_no_of_words] => 10891
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[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0104/20120104156.pdf
[firstpage_image] =>[orig_patent_app_number] => 13282985
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/282985 | Use of auxiliary rudders for yaw control at low speed | Oct 26, 2011 | Issued |
Array
(
[id] => 8165597
[patent_doc_number] => 20120104153
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2012-05-03
[patent_title] => 'GYROPLANE PREROTATION BY COMPRESSED AIR'
[patent_app_type] => utility
[patent_app_number] => 13/282780
[patent_app_country] => US
[patent_app_date] => 2011-10-27
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 11
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[patent_no_of_words] => 8729
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[firstpage_image] =>[orig_patent_app_number] => 13282780
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/282780 | GYROPLANE PREROTATION BY COMPRESSED AIR | Oct 26, 2011 | Abandoned |
| 13/317751 | Rotor hub compressed air system and method | Oct 26, 2011 | Abandoned |
Array
(
[id] => 8764754
[patent_doc_number] => 20130092791
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2013-04-18
[patent_title] => 'METHOD FOR A NOISE ABATEMENT PROCEDURE FOR AN AIRCRAFT'
[patent_app_type] => utility
[patent_app_number] => 13/276007
[patent_app_country] => US
[patent_app_date] => 2011-10-18
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 7
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[patent_no_of_words] => 3728
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[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13276007
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/276007 | METHOD FOR A NOISE ABATEMENT PROCEDURE FOR AN AIRCRAFT | Oct 17, 2011 | Abandoned |
Array
(
[id] => 9921083
[patent_doc_number] => 08979032
[patent_country] => US
[patent_kind] => B1
[patent_issue_date] => 2015-03-17
[patent_title] => 'Methods and systems for retrieving personnel'
[patent_app_type] => utility
[patent_app_number] => 13/275974
[patent_app_country] => US
[patent_app_date] => 2011-10-18
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 7
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[patent_no_of_words] => 5416
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[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13275974
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/275974 | Methods and systems for retrieving personnel | Oct 17, 2011 | Issued |
Array
(
[id] => 7749994
[patent_doc_number] => 20120025012
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2012-02-02
[patent_title] => 'ROTARY WING VEHICLE'
[patent_app_type] => utility
[patent_app_number] => 13/270872
[patent_app_country] => US
[patent_app_date] => 2011-10-11
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 30
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[pdf_file] => publications/A1/0025/20120025012.pdf
[firstpage_image] =>[orig_patent_app_number] => 13270872
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/270872 | Rotary wing vehicle | Oct 10, 2011 | Issued |
Array
(
[id] => 8742429
[patent_doc_number] => 20130082146
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2013-04-04
[patent_title] => 'SYSTEM AND METHOD FOR CREATING AN ARTIFICIAL ATMOSPHERE FOR THE REMOVAL OF SPACE DEBRIS'
[patent_app_type] => utility
[patent_app_number] => 13/250409
[patent_app_country] => US
[patent_app_date] => 2011-09-30
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 9
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[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13250409
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/250409 | SYSTEM AND METHOD FOR CREATING AN ARTIFICIAL ATMOSPHERE FOR THE REMOVAL OF SPACE DEBRIS | Sep 29, 2011 | Abandoned |
Array
(
[id] => 8049053
[patent_doc_number] => 20120074262
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2012-03-29
[patent_title] => 'DE-ICING SYSTEM FOR A FIXED OR ROTARY AIRCRAFT WING'
[patent_app_type] => utility
[patent_app_number] => 13/240838
[patent_app_country] => US
[patent_app_date] => 2011-09-22
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
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[pdf_file] => publications/A1/0074/20120074262.pdf
[firstpage_image] =>[orig_patent_app_number] => 13240838
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/240838 | De-icing system for a fixed or rotary aircraft wing | Sep 21, 2011 | Issued |
Array
(
[id] => 8049037
[patent_doc_number] => 20120074261
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2012-03-29
[patent_title] => 'FUSELAGE ARRANGEMENT, AIRCRAFT OR SPACECRAFT AND METHOD'
[patent_app_type] => utility
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[firstpage_image] =>[orig_patent_app_number] => 13240174
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/240174 | FUSELAGE ARRANGEMENT, AIRCRAFT OR SPACECRAFT AND METHOD | Sep 21, 2011 | Abandoned |
Array
(
[id] => 10874741
[patent_doc_number] => 08899522
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2014-12-02
[patent_title] => 'Aircraft fuselage with high strength frames'
[patent_app_type] => utility
[patent_app_number] => 13/229927
[patent_app_country] => US
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[rel_patent_id] =>[rel_patent_doc_number] =>) 13/229927 | Aircraft fuselage with high strength frames | Sep 11, 2011 | Issued |
Array
(
[id] => 7666540
[patent_doc_number] => 20110315809
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2011-12-29
[patent_title] => 'THREE WING, SIX-TILT PROPULSION UNIT, VTOL AIRCRAFT'
[patent_app_type] => utility
[patent_app_number] => 13/230173
[patent_app_country] => US
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[patent_effective_date] => 0000-00-00
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[rel_patent_id] =>[rel_patent_doc_number] =>) 13/230173 | Three wing, six-tilt propulsion unit, VTOL aircraft | Sep 11, 2011 | Issued |
Array
(
[id] => 9822246
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[patent_issue_date] => 2015-01-13
[patent_title] => 'Fail safe, multiple source, tip-jet supply apparatus and method'
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[rel_patent_id] =>[rel_patent_doc_number] =>) 13/199682 | Fail safe, multiple source, tip-jet supply apparatus and method | Sep 6, 2011 | Issued |
Array
(
[id] => 9848977
[patent_doc_number] => 08950699
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[patent_issue_date] => 2015-02-10
[patent_title] => 'Heliplane rotor thermal management for maintaining dimensional stability'
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Array
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Array
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Array
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