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] => 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 [patent_no_of_claims] => 20 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 238 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [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 [patent_figures_cnt] => 15 [patent_no_of_words] => 7015 [patent_no_of_claims] => 25 [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] => 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 [patent_figures_cnt] => 8 [patent_no_of_words] => 5079 [patent_no_of_claims] => 19 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 49 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 12977519 [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 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 89 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [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 [patent_no_of_claims] => 6 [patent_no_of_ind_claims] => 6 [patent_words_short_claim] => 196 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [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 [patent_figures_cnt] => 4 [patent_no_of_words] => 3919 [patent_no_of_claims] => 19 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 167 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [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 [patent_no_of_ind_claims] => 1 [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 [patent_figures_cnt] => 10 [patent_no_of_words] => 3985 [patent_no_of_claims] => 4 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 78 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [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 [patent_drawing_sheets_cnt] => 8 [patent_figures_cnt] => 10 [patent_no_of_words] => 3979 [patent_no_of_claims] => 5 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 138 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [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 [patent_figures_cnt] => 13 [patent_no_of_words] => 10281 [patent_no_of_claims] => 12 [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/A1/0272/20110272519.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 [patent_drawing_sheets_cnt] => 13 [patent_figures_cnt] => 13 [patent_no_of_words] => 6367 [patent_no_of_claims] => 19 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 229 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [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 [patent_app_date] => 2010-10-15 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 12 [patent_figures_cnt] => 17 [patent_no_of_words] => 6646 [patent_no_of_claims] => 20 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 87 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [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 [patent_country] => US [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 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 6 [patent_figures_cnt] => 8 [patent_no_of_words] => 3080 [patent_no_of_claims] => 14 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 250 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [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 [patent_app_number] => 12/903928 [patent_app_country] => US [patent_app_date] => 2010-10-13 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 5 [patent_figures_cnt] => 5 [patent_no_of_words] => 7860 [patent_no_of_claims] => 12 [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/A1/0024/20110024552.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 [patent_app_country] => US [patent_app_date] => 2010-10-08 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 6 [patent_figures_cnt] => 6 [patent_no_of_words] => 9987 [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/A1/0168/20110168835.pdf [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 [patent_app_country] => US [patent_app_date] => 2010-09-30 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 4 [patent_figures_cnt] => 4 [patent_no_of_words] => 2478 [patent_no_of_claims] => 8 [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/A1/0079/20110079679.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 [patent_app_country] => US [patent_app_date] => 2010-09-30 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 2 [patent_figures_cnt] => 4 [patent_no_of_words] => 1835 [patent_no_of_claims] => 8 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 121 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 12894505 [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' [patent_app_type] => utility [patent_app_number] => 12/924592 [patent_app_country] => US [patent_app_date] => 2010-09-30 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 5 [patent_figures_cnt] => 5 [patent_no_of_words] => 2092 [patent_no_of_claims] => 9 [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/A1/0079/20110079677.pdf [firstpage_image] =>[orig_patent_app_number] => 12924592 [rel_patent_id] =>[rel_patent_doc_number] =>)
12/924592
Ornithopter Sep 29, 2010 Abandoned
Array ( [id] => 8919547 [patent_doc_number] => 08485471 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2013-07-16 [patent_title] => 'Passive ejection seat arm flail restraint apparatus and method' [patent_app_type] => utility [patent_app_number] => 12/893217 [patent_app_country] => US [patent_app_date] => 2010-09-29 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 3 [patent_figures_cnt] => 4 [patent_no_of_words] => 2199 [patent_no_of_claims] => 16 [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] => 12893217 [rel_patent_id] =>[rel_patent_doc_number] =>)
12/893217
Passive ejection seat arm flail restraint apparatus and method Sep 28, 2010 Issued
Array ( [id] => 8049063 [patent_doc_number] => 20120074263 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2012-03-29 [patent_title] => 'Dynamically controlled cross flow instability inhibiting assembly' [patent_app_type] => utility [patent_app_number] => 12/893618 [patent_app_country] => US [patent_app_date] => 2010-09-29 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 4 [patent_figures_cnt] => 4 [patent_no_of_words] => 4342 [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] => publications/A1/0074/20120074263.pdf [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
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