Search

Ronald B. Abelson

Examiner (ID: 14522, Phone: (571)272-3165 , Office: P/2476 )

Most Active Art Unit
2476
Art Unit(s)
2666, 2476, 2419, 2619, 2616, 2663
Total Applications
2097
Issued Applications
1821
Pending Applications
143
Abandoned Applications
161

Applications

Application numberTitle of the applicationFiling DateStatus
Array ( [id] => 9253090 [patent_doc_number] => 08616496 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2013-12-31 [patent_title] => 'Systems and methods for a self-deploying vehicle drag device' [patent_app_type] => utility [patent_app_number] => 13/197333 [patent_app_country] => US [patent_app_date] => 2011-08-03 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 5 [patent_figures_cnt] => 8 [patent_no_of_words] => 5266 [patent_no_of_claims] => 20 [patent_no_of_ind_claims] => 3 [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] => 13197333 [rel_patent_id] =>[rel_patent_doc_number] =>)
13/197333
Systems and methods for a self-deploying vehicle drag device Aug 2, 2011 Issued
Array ( [id] => 9439173 [patent_doc_number] => 08708273 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2014-04-29 [patent_title] => 'Three-wing, six tilt-propulsion unit, VTOL aircraft' [patent_app_type] => utility [patent_app_number] => 13/168624 [patent_app_country] => US [patent_app_date] => 2011-06-24 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 6 [patent_figures_cnt] => 8 [patent_no_of_words] => 10937 [patent_no_of_claims] => 7 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 186 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13168624 [rel_patent_id] =>[rel_patent_doc_number] =>)
13/168624
Three-wing, six tilt-propulsion unit, VTOL aircraft Jun 23, 2011 Issued
Array ( [id] => 8925335 [patent_doc_number] => 20130181095 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2013-07-18 [patent_title] => 'DEVICE TO GENERATE LIFT FORCE (OPTIONS)' [patent_app_type] => utility [patent_app_number] => 13/823317 [patent_app_country] => US [patent_app_date] => 2011-06-06 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 12 [patent_figures_cnt] => 12 [patent_no_of_words] => 4886 [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] => 13823317 [rel_patent_id] =>[rel_patent_doc_number] =>)
13/823317
DEVICE TO GENERATE LIFT FORCE (OPTIONS) Jun 5, 2011
Array ( [id] => 8919552 [patent_doc_number] => 08485476 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2013-07-16 [patent_title] => 'Discrete co-flow jet (DCFJ) airfoil' [patent_app_type] => utility [patent_app_number] => 13/102844 [patent_app_country] => US [patent_app_date] => 2011-05-06 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 24 [patent_figures_cnt] => 27 [patent_no_of_words] => 12110 [patent_no_of_claims] => 19 [patent_no_of_ind_claims] => 3 [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] => 13102844 [rel_patent_id] =>[rel_patent_doc_number] =>)
13/102844
Discrete co-flow jet (DCFJ) airfoil May 5, 2011 Issued
Array ( [id] => 8396986 [patent_doc_number] => 08267355 [patent_country] => US [patent_kind] => B1 [patent_issue_date] => 2012-09-18 [patent_title] => 'Method of controlling aircraft, missiles, munitions and ground vehicles with plasma actuators' [patent_app_type] => utility [patent_app_number] => 13/094872 [patent_app_country] => US [patent_app_date] => 2011-04-27 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 8 [patent_figures_cnt] => 8 [patent_no_of_words] => 5397 [patent_no_of_claims] => 20 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 148 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13094872 [rel_patent_id] =>[rel_patent_doc_number] =>)
13/094872
Method of controlling aircraft, missiles, munitions and ground vehicles with plasma actuators Apr 26, 2011 Issued
Array ( [id] => 9058365 [patent_doc_number] => 08544798 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2013-10-01 [patent_title] => 'Window replacement for filling a window frame' [patent_app_type] => utility [patent_app_number] => 13/084110 [patent_app_country] => US [patent_app_date] => 2011-04-11 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 3 [patent_figures_cnt] => 4 [patent_no_of_words] => 3760 [patent_no_of_claims] => 5 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 176 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13084110 [rel_patent_id] =>[rel_patent_doc_number] =>)
13/084110
Window replacement for filling a window frame Apr 10, 2011 Issued
Array ( [id] => 9387727 [patent_doc_number] => 08684315 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2014-04-01 [patent_title] => 'Active winglet' [patent_app_type] => utility [patent_app_number] => 13/075934 [patent_app_country] => US [patent_app_date] => 2011-03-30 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 8 [patent_figures_cnt] => 8 [patent_no_of_words] => 4616 [patent_no_of_claims] => 18 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 95 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13075934 [rel_patent_id] =>[rel_patent_doc_number] =>)
13/075934
Active winglet Mar 29, 2011 Issued
Array ( [id] => 9125597 [patent_doc_number] => 08573536 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2013-11-05 [patent_title] => 'Method and apparatus for automated launch, retrieval, and servicing of a hovering aircraft' [patent_app_type] => utility [patent_app_number] => 13/037436 [patent_app_country] => US [patent_app_date] => 2011-03-01 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 21 [patent_figures_cnt] => 21 [patent_no_of_words] => 2846 [patent_no_of_claims] => 30 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 191 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13037436 [rel_patent_id] =>[rel_patent_doc_number] =>)
13/037436
Method and apparatus for automated launch, retrieval, and servicing of a hovering aircraft Feb 28, 2011 Issued
Array ( [id] => 11263016 [patent_doc_number] => 09487301 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2016-11-08 [patent_title] => 'High efficiency external airbag for crash attenuation' [patent_app_type] => utility [patent_app_number] => 13/696970 [patent_app_country] => US [patent_app_date] => 2011-02-23 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 7 [patent_figures_cnt] => 13 [patent_no_of_words] => 4140 [patent_no_of_claims] => 15 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 218 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13696970 [rel_patent_id] =>[rel_patent_doc_number] =>)
13/696970
High efficiency external airbag for crash attenuation Feb 22, 2011 Issued
Array ( [id] => 6207916 [patent_doc_number] => 20110133024 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2011-06-09 [patent_title] => 'METHOD AND APPARATUS FOR RETRIEVING A HOVERING AIRCRAFT' [patent_app_type] => utility [patent_app_number] => 13/024843 [patent_app_country] => US [patent_app_date] => 2011-02-10 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 21 [patent_figures_cnt] => 21 [patent_no_of_words] => 4104 [patent_no_of_claims] => 19 [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/A1/0133/20110133024.pdf [firstpage_image] =>[orig_patent_app_number] => 13024843 [rel_patent_id] =>[rel_patent_doc_number] =>)
13/024843
Method and apparatus for retrieving a hovering aircraft Feb 9, 2011 Issued
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
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