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] => 14699493 [patent_doc_number] => 10377477 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2019-08-13 [patent_title] => Adjustable pitch link [patent_app_type] => utility [patent_app_number] => 13/669212 [patent_app_country] => US [patent_app_date] => 2012-11-05 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 2 [patent_figures_cnt] => 5 [patent_no_of_words] => 2570 [patent_no_of_claims] => 12 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 226 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13669212 [rel_patent_id] =>[rel_patent_doc_number] =>)
13/669212
Adjustable pitch link Nov 4, 2012 Issued
Array ( [id] => 9641674 [patent_doc_number] => 20140219784 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2014-08-07 [patent_title] => 'PROPULSION DEVICE' [patent_app_type] => utility [patent_app_number] => 13/661137 [patent_app_country] => US [patent_app_date] => 2012-10-26 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 9 [patent_figures_cnt] => 9 [patent_no_of_words] => 11587 [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] =>[firstpage_image] =>[orig_patent_app_number] => 13661137 [rel_patent_id] =>[rel_patent_doc_number] =>)
13/661137
PROPULSION DEVICE Oct 25, 2012 Abandoned
Array ( [id] => 10548171 [patent_doc_number] => 09272779 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2016-03-01 [patent_title] => 'Aircraft with pivoting rotor mast' [patent_app_type] => utility [patent_app_number] => 14/350326 [patent_app_country] => US [patent_app_date] => 2012-10-03 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 4 [patent_figures_cnt] => 6 [patent_no_of_words] => 2966 [patent_no_of_claims] => 22 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 60 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14350326 [rel_patent_id] =>[rel_patent_doc_number] =>)
14/350326
Aircraft with pivoting rotor mast Oct 2, 2012 Issued
Array ( [id] => 10874745 [patent_doc_number] => 08899526 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2014-12-02 [patent_title] => 'Parachute harness container with bio-contoured load distributing vest' [patent_app_type] => utility [patent_app_number] => 13/632304 [patent_app_country] => US [patent_app_date] => 2012-10-01 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 5 [patent_figures_cnt] => 12 [patent_no_of_words] => 3416 [patent_no_of_claims] => 17 [patent_no_of_ind_claims] => 4 [patent_words_short_claim] => 234 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13632304 [rel_patent_id] =>[rel_patent_doc_number] =>)
13/632304
Parachute harness container with bio-contoured load distributing vest Sep 30, 2012 Issued
Array ( [id] => 10175724 [patent_doc_number] => 09205913 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2015-12-08 [patent_title] => 'Rotorcraft, dynamic, CG management apparatus and method' [patent_app_type] => utility [patent_app_number] => 13/623778 [patent_app_country] => US [patent_app_date] => 2012-09-20 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 12 [patent_figures_cnt] => 14 [patent_no_of_words] => 7580 [patent_no_of_claims] => 17 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 132 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13623778 [rel_patent_id] =>[rel_patent_doc_number] =>)
13/623778
Rotorcraft, dynamic, CG management apparatus and method Sep 19, 2012 Issued
Array ( [id] => 9842464 [patent_doc_number] => 08944366 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2015-02-03 [patent_title] => 'Rotorcraft empennage mounting system' [patent_app_type] => utility [patent_app_number] => 13/605951 [patent_app_country] => US [patent_app_date] => 2012-09-06 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 7 [patent_figures_cnt] => 8 [patent_no_of_words] => 5859 [patent_no_of_claims] => 19 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 172 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13605951 [rel_patent_id] =>[rel_patent_doc_number] =>)
13/605951
Rotorcraft empennage mounting system Sep 5, 2012 Issued
Array ( [id] => 9231273 [patent_doc_number] => 08596573 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2013-12-03 [patent_title] => 'Nacelle flow assembly' [patent_app_type] => utility [patent_app_number] => 13/603706 [patent_app_country] => US [patent_app_date] => 2012-09-05 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 2 [patent_figures_cnt] => 4 [patent_no_of_words] => 1851 [patent_no_of_claims] => 15 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 161 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13603706 [rel_patent_id] =>[rel_patent_doc_number] =>)
13/603706
Nacelle flow assembly Sep 4, 2012 Issued
Array ( [id] => 9334598 [patent_doc_number] => 20140061380 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2014-03-06 [patent_title] => 'MODULARIZED AIRPLANE STRUCTURES AND METHODS' [patent_app_type] => utility [patent_app_number] => 13/602601 [patent_app_country] => US [patent_app_date] => 2012-09-04 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 18 [patent_figures_cnt] => 18 [patent_no_of_words] => 8322 [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] =>[firstpage_image] =>[orig_patent_app_number] => 13602601 [rel_patent_id] =>[rel_patent_doc_number] =>)
13/602601
MODULARIZED AIRPLANE STRUCTURES AND METHODS Sep 3, 2012 Abandoned
Array ( [id] => 12944824 [patent_doc_number] => 09834301 [patent_country] => US [patent_kind] => B1 [patent_issue_date] => 2017-12-05 [patent_title] => Method of increasing the performance of aircraft, missiles, munitions and ground vehicles with plasma actuators [patent_app_type] => utility [patent_app_number] => 13/570684 [patent_app_country] => US [patent_app_date] => 2012-08-09 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 8 [patent_figures_cnt] => 8 [patent_no_of_words] => 5280 [patent_no_of_claims] => 13 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 101 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13570684 [rel_patent_id] =>[rel_patent_doc_number] =>)
13/570684
Method of increasing the performance of aircraft, missiles, munitions and ground vehicles with plasma actuators Aug 8, 2012 Issued
Array ( [id] => 11263002 [patent_doc_number] => 09487287 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2016-11-08 [patent_title] => 'Wing leading edge venting' [patent_app_type] => utility [patent_app_number] => 13/558761 [patent_app_country] => US [patent_app_date] => 2012-07-26 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 5 [patent_figures_cnt] => 6 [patent_no_of_words] => 3749 [patent_no_of_claims] => 15 [patent_no_of_ind_claims] => 4 [patent_words_short_claim] => 136 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13558761 [rel_patent_id] =>[rel_patent_doc_number] =>)
13/558761
Wing leading edge venting Jul 25, 2012 Issued
Array ( [id] => 10089858 [patent_doc_number] => 09126671 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2015-09-08 [patent_title] => 'Stiff panel for aircraft, comprising stiffeners with notched cores' [patent_app_type] => utility [patent_app_number] => 13/557390 [patent_app_country] => US [patent_app_date] => 2012-07-25 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 2 [patent_figures_cnt] => 4 [patent_no_of_words] => 1732 [patent_no_of_claims] => 8 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 142 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13557390 [rel_patent_id] =>[rel_patent_doc_number] =>)
13/557390
Stiff panel for aircraft, comprising stiffeners with notched cores Jul 24, 2012 Issued
Array ( [id] => 8937205 [patent_doc_number] => 20130187002 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2013-07-25 [patent_title] => 'PROTECTIVE SHIELD AGAINST ICE IMPACTS ON AIRCRAFT' [patent_app_type] => utility [patent_app_number] => 13/550886 [patent_app_country] => US [patent_app_date] => 2012-07-17 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 4 [patent_figures_cnt] => 4 [patent_no_of_words] => 2878 [patent_no_of_claims] => 15 [patent_no_of_ind_claims] => 4 [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] => 13550886 [rel_patent_id] =>[rel_patent_doc_number] =>)
13/550886
PROTECTIVE SHIELD AGAINST ICE IMPACTS ON AIRCRAFT Jul 16, 2012 Abandoned
Array ( [id] => 10083227 [patent_doc_number] => 09120565 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2015-09-01 [patent_title] => 'Method for enhancing pilot efficiency and aircraft safety during ground travel' [patent_app_type] => utility [patent_app_number] => 13/550576 [patent_app_country] => US [patent_app_date] => 2012-07-16 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 2 [patent_figures_cnt] => 2 [patent_no_of_words] => 4880 [patent_no_of_claims] => 5 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 334 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13550576 [rel_patent_id] =>[rel_patent_doc_number] =>)
13/550576
Method for enhancing pilot efficiency and aircraft safety during ground travel Jul 15, 2012 Issued
Array ( [id] => 9528925 [patent_doc_number] => 08752786 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2014-06-17 [patent_title] => 'Low speed autogyro yaw control apparatus and method' [patent_app_type] => utility [patent_app_number] => 13/545904 [patent_app_country] => US [patent_app_date] => 2012-07-10 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 30 [patent_figures_cnt] => 44 [patent_no_of_words] => 13138 [patent_no_of_claims] => 9 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 68 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13545904 [rel_patent_id] =>[rel_patent_doc_number] =>)
13/545904
Low speed autogyro yaw control apparatus and method Jul 9, 2012 Issued
Array ( [id] => 9956209 [patent_doc_number] => 09004394 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2015-04-14 [patent_title] => 'Mission-adaptive rotor blade with circulation control' [patent_app_type] => utility [patent_app_number] => 13/544874 [patent_app_country] => US [patent_app_date] => 2012-07-09 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 8 [patent_figures_cnt] => 13 [patent_no_of_words] => 7506 [patent_no_of_claims] => 20 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 178 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13544874 [rel_patent_id] =>[rel_patent_doc_number] =>)
13/544874
Mission-adaptive rotor blade with circulation control Jul 8, 2012 Issued
Array ( [id] => 8480679 [patent_doc_number] => 20120280086 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2012-11-08 [patent_title] => 'Reversible Space Plane' [patent_app_type] => utility [patent_app_number] => 13/542523 [patent_app_country] => US [patent_app_date] => 2012-07-05 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 9 [patent_figures_cnt] => 9 [patent_no_of_words] => 7364 [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] => 13542523 [rel_patent_id] =>[rel_patent_doc_number] =>)
13/542523
Reversible space plane Jul 4, 2012 Issued
Array ( [id] => 8474205 [patent_doc_number] => 20120273612 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2012-11-01 [patent_title] => 'METHOD AND APPARATUS FOR RETRIEVING A HOVERING AIRCRAFT' [patent_app_type] => utility [patent_app_number] => 13/540032 [patent_app_country] => US [patent_app_date] => 2012-07-02 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 21 [patent_figures_cnt] => 21 [patent_no_of_words] => 4218 [patent_no_of_claims] => 9 [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] => 13540032 [rel_patent_id] =>[rel_patent_doc_number] =>)
13/540032
Method and apparatus for retrieving a hovering aircraft Jul 1, 2012 Issued
Array ( [id] => 8919553 [patent_doc_number] => 08485477 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2013-07-16 [patent_title] => 'Rotational aircraft throttle interface' [patent_app_type] => utility [patent_app_number] => 13/528666 [patent_app_country] => US [patent_app_date] => 2012-06-20 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 6 [patent_figures_cnt] => 7 [patent_no_of_words] => 7281 [patent_no_of_claims] => 17 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 101 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13528666 [rel_patent_id] =>[rel_patent_doc_number] =>)
13/528666
Rotational aircraft throttle interface Jun 19, 2012 Issued
Array ( [id] => 8888263 [patent_doc_number] => 20130161447 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2013-06-27 [patent_title] => 'METHOD AND APPARATUS FOR AUTOMATED LAUNCH, RETRIEVAL, AND SERVICING OF A HOVERING AIRCRAFT' [patent_app_type] => utility [patent_app_number] => 13/527177 [patent_app_country] => US [patent_app_date] => 2012-06-19 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 15 [patent_figures_cnt] => 15 [patent_no_of_words] => 2584 [patent_no_of_claims] => 17 [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] => 13527177 [rel_patent_id] =>[rel_patent_doc_number] =>)
13/527177
Method and apparatus for automated launch, retrieval, and servicing of a hovering aircraft Jun 18, 2012 Issued
Array ( [id] => 8506300 [patent_doc_number] => 20120305708 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2012-12-06 [patent_title] => 'INTEGRALLY STIFFENED PANEL' [patent_app_type] => utility [patent_app_number] => 13/486499 [patent_app_country] => US [patent_app_date] => 2012-06-01 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 27 [patent_figures_cnt] => 27 [patent_no_of_words] => 4082 [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] =>[firstpage_image] =>[orig_patent_app_number] => 13486499 [rel_patent_id] =>[rel_patent_doc_number] =>)
13/486499
Integrally stiffened panel May 31, 2012 Issued
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