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] => 9988090 [patent_doc_number] => 09033283 [patent_country] => US [patent_kind] => B1 [patent_issue_date] => 2015-05-19 [patent_title] => 'Passive adaptive structures' [patent_app_type] => utility [patent_app_number] => 13/800678 [patent_app_country] => US [patent_app_date] => 2013-03-13 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 22 [patent_figures_cnt] => 34 [patent_no_of_words] => 23337 [patent_no_of_claims] => 17 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 144 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13800678 [rel_patent_id] =>[rel_patent_doc_number] =>)
13/800678
Passive adaptive structures Mar 12, 2013 Issued
Array ( [id] => 9942482 [patent_doc_number] => 08991771 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2015-03-31 [patent_title] => 'Piloting device for piloting an aircraft having a protected force sensor' [patent_app_type] => utility [patent_app_number] => 13/794847 [patent_app_country] => US [patent_app_date] => 2013-03-12 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 5 [patent_figures_cnt] => 9 [patent_no_of_words] => 4703 [patent_no_of_claims] => 13 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 262 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13794847 [rel_patent_id] =>[rel_patent_doc_number] =>)
13/794847
Piloting device for piloting an aircraft having a protected force sensor Mar 11, 2013 Issued
Array ( [id] => 11767641 [patent_doc_number] => 09376206 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2016-06-28 [patent_title] => 'Tiltrotor aircraft with inboard wing mounted fixed engine arrangement' [patent_app_type] => utility [patent_app_number] => 13/797350 [patent_app_country] => US [patent_app_date] => 2013-03-12 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 16 [patent_figures_cnt] => 16 [patent_no_of_words] => 6891 [patent_no_of_claims] => 25 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 97 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13797350 [rel_patent_id] =>[rel_patent_doc_number] =>)
13/797350
Tiltrotor aircraft with inboard wing mounted fixed engine arrangement Mar 11, 2013 Issued
Array ( [id] => 10001140 [patent_doc_number] => 09045218 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2015-06-02 [patent_title] => 'Autonomous aircraft with disconnectable tether' [patent_app_type] => utility [patent_app_number] => 13/791105 [patent_app_country] => US [patent_app_date] => 2013-03-08 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 8 [patent_figures_cnt] => 16 [patent_no_of_words] => 2867 [patent_no_of_claims] => 20 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 125 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13791105 [rel_patent_id] =>[rel_patent_doc_number] =>)
13/791105
Autonomous aircraft with disconnectable tether Mar 7, 2013 Issued
Array ( [id] => 9949351 [patent_doc_number] => 08998124 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2015-04-07 [patent_title] => 'Aircraft with electrically conductive nanocoating' [patent_app_type] => utility [patent_app_number] => 13/789269 [patent_app_country] => US [patent_app_date] => 2013-03-07 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 5 [patent_figures_cnt] => 6 [patent_no_of_words] => 2436 [patent_no_of_claims] => 17 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 135 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13789269 [rel_patent_id] =>[rel_patent_doc_number] =>)
13/789269
Aircraft with electrically conductive nanocoating Mar 6, 2013 Issued
Array ( [id] => 9111556 [patent_doc_number] => 08567718 [patent_country] => US [patent_kind] => B1 [patent_issue_date] => 2013-10-29 [patent_title] => 'Launch and recovery system for unmanned aerial vehicles' [patent_app_type] => utility [patent_app_number] => 13/783575 [patent_app_country] => US [patent_app_date] => 2013-03-04 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 20 [patent_figures_cnt] => 32 [patent_no_of_words] => 13712 [patent_no_of_claims] => 6 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 103 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13783575 [rel_patent_id] =>[rel_patent_doc_number] =>)
13/783575
Launch and recovery system for unmanned aerial vehicles Mar 3, 2013 Issued
Array ( [id] => 9682362 [patent_doc_number] => 20140239125 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2014-08-28 [patent_title] => 'MODULAR CORE STRUCTURE FOR DUAL-MANIFEST SPACECRAFT LAUNCH' [patent_app_type] => utility [patent_app_number] => 13/781373 [patent_app_country] => US [patent_app_date] => 2013-02-28 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 12 [patent_figures_cnt] => 12 [patent_no_of_words] => 6358 [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] => 13781373 [rel_patent_id] =>[rel_patent_doc_number] =>)
13/781373
Modular core structure for dual-manifest spacecraft launch Feb 27, 2013 Issued
Array ( [id] => 10083232 [patent_doc_number] => 09120570 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2015-09-01 [patent_title] => 'Precision aerial delivery system' [patent_app_type] => utility [patent_app_number] => 13/776733 [patent_app_country] => US [patent_app_date] => 2013-02-26 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 5 [patent_figures_cnt] => 5 [patent_no_of_words] => 10998 [patent_no_of_claims] => 24 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 183 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13776733 [rel_patent_id] =>[rel_patent_doc_number] =>)
13/776733
Precision aerial delivery system Feb 25, 2013 Issued
Array ( [id] => 10573832 [patent_doc_number] => 09296460 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2016-03-29 [patent_title] => 'Airship with internal propulsion system' [patent_app_type] => utility [patent_app_number] => 13/767844 [patent_app_country] => US [patent_app_date] => 2013-02-14 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 7 [patent_figures_cnt] => 13 [patent_no_of_words] => 3991 [patent_no_of_claims] => 11 [patent_no_of_ind_claims] => 3 [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] => 13767844 [rel_patent_id] =>[rel_patent_doc_number] =>)
13/767844
Airship with internal propulsion system Feb 13, 2013 Issued
Array ( [id] => 8900992 [patent_doc_number] => 20130168495 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2013-07-04 [patent_title] => 'NON-FOGGING VEHICLE WINDOW' [patent_app_type] => utility [patent_app_number] => 13/761584 [patent_app_country] => US [patent_app_date] => 2013-02-07 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 8 [patent_figures_cnt] => 8 [patent_no_of_words] => 3886 [patent_no_of_claims] => 13 [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] => 13761584 [rel_patent_id] =>[rel_patent_doc_number] =>)
13/761584
Non-fogging vehicle window Feb 6, 2013 Issued
Array ( [id] => 10198863 [patent_doc_number] => 20150083849 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2015-03-26 [patent_title] => 'AEROSTAT SYSTEM' [patent_app_type] => utility [patent_app_number] => 14/372844 [patent_app_country] => US [patent_app_date] => 2013-01-17 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 6 [patent_figures_cnt] => 6 [patent_no_of_words] => 4547 [patent_no_of_claims] => 14 [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] => 14372844 [rel_patent_id] =>[rel_patent_doc_number] =>)
14/372844
Aerostat system with extended flight envelope Jan 16, 2013 Issued
Array ( [id] => 9058360 [patent_doc_number] => 08544793 [patent_country] => US [patent_kind] => B1 [patent_issue_date] => 2013-10-01 [patent_title] => 'Adjustable angle inlet for turbojet engines' [patent_app_type] => utility [patent_app_number] => 13/736891 [patent_app_country] => US [patent_app_date] => 2013-01-08 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 4 [patent_figures_cnt] => 4 [patent_no_of_words] => 2252 [patent_no_of_claims] => 13 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 79 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13736891 [rel_patent_id] =>[rel_patent_doc_number] =>)
13/736891
Adjustable angle inlet for turbojet engines Jan 7, 2013 Issued
Array ( [id] => 11685780 [patent_doc_number] => 09683820 [patent_country] => US [patent_kind] => B1 [patent_issue_date] => 2017-06-20 [patent_title] => 'Aircraft, missile, projectile or underwater vehicle with reconfigurable control surfaces and method of reconfiguring' [patent_app_type] => utility [patent_app_number] => 13/734368 [patent_app_country] => US [patent_app_date] => 2013-01-04 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 7 [patent_figures_cnt] => 9 [patent_no_of_words] => 5324 [patent_no_of_claims] => 13 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 129 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13734368 [rel_patent_id] =>[rel_patent_doc_number] =>)
13/734368
Aircraft, missile, projectile or underwater vehicle with reconfigurable control surfaces and method of reconfiguring Jan 3, 2013 Issued
Array ( [id] => 8924710 [patent_doc_number] => 20130180470 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2013-07-18 [patent_title] => 'Hip Lift Harness Device and Method' [patent_app_type] => utility [patent_app_number] => 13/724837 [patent_app_country] => US [patent_app_date] => 2012-12-21 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 4 [patent_figures_cnt] => 4 [patent_no_of_words] => 5648 [patent_no_of_claims] => 19 [patent_no_of_ind_claims] => 5 [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] => 13724837 [rel_patent_id] =>[rel_patent_doc_number] =>)
13/724837
Hip Lift Harness Device and Method Dec 20, 2012 Abandoned
Array ( [id] => 15308375 [patent_doc_number] => 10518877 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2019-12-31 [patent_title] => Inter-vehicle communication for hazard handling for an unoccupied flying vehicle (UFV) [patent_app_type] => utility [patent_app_number] => 13/720694 [patent_app_country] => US [patent_app_date] => 2012-12-19 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 19 [patent_figures_cnt] => 19 [patent_no_of_words] => 22307 [patent_no_of_claims] => 35 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 296 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13720694 [rel_patent_id] =>[rel_patent_doc_number] =>)
13/720694
Inter-vehicle communication for hazard handling for an unoccupied flying vehicle (UFV) Dec 18, 2012 Issued
Array ( [id] => 8913757 [patent_doc_number] => 20130175382 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2013-07-11 [patent_title] => 'System, method and apparatus for widespread commercialization of hydrogen as a carbon-free alternative fuel source' [patent_app_type] => utility [patent_app_number] => 13/716281 [patent_app_country] => US [patent_app_date] => 2012-12-17 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 5 [patent_figures_cnt] => 5 [patent_no_of_words] => 6813 [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] => 13716281 [rel_patent_id] =>[rel_patent_doc_number] =>)
13/716281
Lighter-than-air craft docking system using unmanned flight vehicle Dec 16, 2012 Issued
Array ( [id] => 9334596 [patent_doc_number] => 20140061378 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2014-03-06 [patent_title] => 'METHOD AND APPARATUS FOR RETRIEVING A HOVERING AIRCRAFT' [patent_app_type] => utility [patent_app_number] => 13/717147 [patent_app_country] => US [patent_app_date] => 2012-12-17 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 21 [patent_figures_cnt] => 21 [patent_no_of_words] => 4255 [patent_no_of_claims] => 28 [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] => 13717147 [rel_patent_id] =>[rel_patent_doc_number] =>)
13/717147
Method and apparatus for retrieving a hovering aircraft Dec 16, 2012 Issued
Array ( [id] => 9508549 [patent_doc_number] => 20140145040 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2014-05-29 [patent_title] => 'SYSTEM AND METHOD FOR MINIMIZING WAVE DRAG THROUGH BILATERALLY ASYMMETRIC DESIGN' [patent_app_type] => utility [patent_app_number] => 13/687483 [patent_app_country] => US [patent_app_date] => 2012-11-28 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 11 [patent_figures_cnt] => 11 [patent_no_of_words] => 9197 [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] => 13687483 [rel_patent_id] =>[rel_patent_doc_number] =>)
13/687483
System and method for minimizing wave drag through bilaterally asymmetric design Nov 27, 2012 Issued
Array ( [id] => 8883396 [patent_doc_number] => 20130156580 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2013-06-20 [patent_title] => 'Constant-Velocity Drive System for Gimbaled Rotor Hubs' [patent_app_type] => utility [patent_app_number] => 13/677146 [patent_app_country] => US [patent_app_date] => 2012-11-14 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 10 [patent_figures_cnt] => 10 [patent_no_of_words] => 6469 [patent_no_of_claims] => 3 [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] => 13677146 [rel_patent_id] =>[rel_patent_doc_number] =>)
13/677146
Constant-velocity drive system for gimbaled rotor hubs Nov 13, 2012 Issued
Array ( [id] => 9766627 [patent_doc_number] => 20140290287 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2014-10-02 [patent_title] => 'METHOD AND ARCHITECTURE FOR RECOVERY OF ENERGY IN AN AIRCRAFT' [patent_app_type] => utility [patent_app_number] => 14/353570 [patent_app_country] => US [patent_app_date] => 2012-11-09 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 5 [patent_figures_cnt] => 5 [patent_no_of_words] => 2937 [patent_no_of_claims] => 11 [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] => 14353570 [rel_patent_id] =>[rel_patent_doc_number] =>)
14/353570
Method and architecture for recovery of energy in an aircraft Nov 8, 2012 Issued
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