Search

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 numberTitle of the applicationFiling DateStatus
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 [patent_no_of_claims] => 19 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 0 [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 [patent_figures_cnt] => 25 [patent_no_of_words] => 10753 [patent_no_of_claims] => 20 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 0 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [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 [patent_no_of_claims] => 20 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 0 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [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 [patent_figures_cnt] => 10 [patent_no_of_words] => 8710 [patent_no_of_claims] => 20 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 0 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [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 [patent_no_of_claims] => 20 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 0 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [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 [patent_figures_cnt] => 11 [patent_no_of_words] => 8729 [patent_no_of_claims] => 20 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 0 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] => publications/A1/0104/20120104153.pdf [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 [patent_figures_cnt] => 7 [patent_no_of_words] => 3728 [patent_no_of_claims] => 16 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 0 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [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 [patent_figures_cnt] => 7 [patent_no_of_words] => 5416 [patent_no_of_claims] => 14 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 100 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [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 [patent_figures_cnt] => 30 [patent_no_of_words] => 7832 [patent_no_of_claims] => 20 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 0 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [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 [patent_figures_cnt] => 9 [patent_no_of_words] => 7968 [patent_no_of_claims] => 22 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 0 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [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 [patent_figures_cnt] => 4 [patent_no_of_words] => 5083 [patent_no_of_claims] => 20 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 0 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [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 [patent_app_number] => 13/240174 [patent_app_country] => US [patent_app_date] => 2011-09-22 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 2 [patent_figures_cnt] => 2 [patent_no_of_words] => 1871 [patent_no_of_claims] => 10 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 0 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] => publications/A1/0074/20120074261.pdf [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 [patent_app_date] => 2011-09-12 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 4 [patent_figures_cnt] => 21 [patent_no_of_words] => 2375 [patent_no_of_claims] => 11 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 127 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13229927 [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 [patent_app_date] => 2011-09-12 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 13 [patent_figures_cnt] => 13 [patent_no_of_words] => 11437 [patent_no_of_claims] => 23 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 0 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13230173 [rel_patent_id] =>[rel_patent_doc_number] =>)
13/230173
Three wing, six-tilt propulsion unit, VTOL aircraft Sep 11, 2011 Issued
Array ( [id] => 9822246 [patent_doc_number] => 08931728 [patent_country] => US [patent_kind] => B1 [patent_issue_date] => 2015-01-13 [patent_title] => 'Fail safe, multiple source, tip-jet supply apparatus and method' [patent_app_type] => utility [patent_app_number] => 13/199682 [patent_app_country] => US [patent_app_date] => 2011-09-07 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 6 [patent_figures_cnt] => 11 [patent_no_of_words] => 5452 [patent_no_of_claims] => 19 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 122 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13199682 [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 [patent_country] => US [patent_kind] => B1 [patent_issue_date] => 2015-02-10 [patent_title] => 'Heliplane rotor thermal management for maintaining dimensional stability' [patent_app_type] => utility [patent_app_number] => 13/199681 [patent_app_country] => US [patent_app_date] => 2011-09-07 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 27 [patent_figures_cnt] => 33 [patent_no_of_words] => 15178 [patent_no_of_claims] => 20 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 173 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13199681 [rel_patent_id] =>[rel_patent_doc_number] =>)
13/199681
Heliplane rotor thermal management for maintaining dimensional stability Sep 6, 2011 Issued
Array ( [id] => 9760569 [patent_doc_number] => 08844880 [patent_country] => US [patent_kind] => B1 [patent_issue_date] => 2014-09-30 [patent_title] => 'Two-place, collective pitch and throttle control' [patent_app_type] => utility [patent_app_number] => 13/199671 [patent_app_country] => US [patent_app_date] => 2011-09-07 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 10 [patent_figures_cnt] => 12 [patent_no_of_words] => 7222 [patent_no_of_claims] => 20 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 345 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13199671 [rel_patent_id] =>[rel_patent_doc_number] =>)
13/199671
Two-place, collective pitch and throttle control Sep 6, 2011 Issued
Array ( [id] => 9976013 [patent_doc_number] => 09022314 [patent_country] => US [patent_kind] => B1 [patent_issue_date] => 2015-05-05 [patent_title] => 'Torsionally stiff rotorcraft control apparatus and method' [patent_app_type] => utility [patent_app_number] => 13/199684 [patent_app_country] => US [patent_app_date] => 2011-09-07 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 27 [patent_figures_cnt] => 33 [patent_no_of_words] => 15047 [patent_no_of_claims] => 19 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 174 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13199684 [rel_patent_id] =>[rel_patent_doc_number] =>)
13/199684
Torsionally stiff rotorcraft control apparatus and method Sep 6, 2011 Issued
Array ( [id] => 9887620 [patent_doc_number] => 08973863 [patent_country] => US [patent_kind] => B1 [patent_issue_date] => 2015-03-10 [patent_title] => 'Blade root attachment apparatus and method' [patent_app_type] => utility [patent_app_number] => 13/199705 [patent_app_country] => US [patent_app_date] => 2011-09-07 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 11 [patent_figures_cnt] => 15 [patent_no_of_words] => 7987 [patent_no_of_claims] => 17 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 165 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13199705 [rel_patent_id] =>[rel_patent_doc_number] =>)
13/199705
Blade root attachment apparatus and method Sep 6, 2011 Issued
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