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] => 10670507 [patent_doc_number] => 20160016652 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2016-01-21 [patent_title] => 'AERIAL VEHICLES AND METHODS OF USE' [patent_app_type] => utility [patent_app_number] => 14/734864 [patent_app_country] => US [patent_app_date] => 2015-06-09 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 15 [patent_figures_cnt] => 15 [patent_no_of_words] => 10156 [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] => 14734864 [rel_patent_id] =>[rel_patent_doc_number] =>)
14/734864
Aerial vehicles and methods of use Jun 8, 2015 Issued
Array ( [id] => 13813959 [patent_doc_number] => 10183740 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2019-01-22 [patent_title] => Leading edge nose structure on the vertical stabilizer of an aircraft [patent_app_type] => utility [patent_app_number] => 14/729632 [patent_app_country] => US [patent_app_date] => 2015-06-03 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 4 [patent_figures_cnt] => 8 [patent_no_of_words] => 2105 [patent_no_of_claims] => 8 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 134 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14729632 [rel_patent_id] =>[rel_patent_doc_number] =>)
14/729632
Leading edge nose structure on the vertical stabilizer of an aircraft Jun 2, 2015 Issued
Array ( [id] => 11325568 [patent_doc_number] => 20160356180 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2016-12-08 [patent_title] => 'NACELLE INLET HAVING AN ANGLE OR CURVED AFT BULKHEAD' [patent_app_type] => utility [patent_app_number] => 14/729420 [patent_app_country] => US [patent_app_date] => 2015-06-03 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 5 [patent_figures_cnt] => 5 [patent_no_of_words] => 3715 [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] => 14729420 [rel_patent_id] =>[rel_patent_doc_number] =>)
14/729420
NACELLE INLET HAVING AN ANGLE OR CURVED AFT BULKHEAD Jun 2, 2015 Abandoned
Array ( [id] => 11463566 [patent_doc_number] => 09580184 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2017-02-28 [patent_title] => 'Twin-engined rotorcraft having a fuel supply installation for a power plant auxiliary power unit (APU)' [patent_app_type] => utility [patent_app_number] => 14/722365 [patent_app_country] => US [patent_app_date] => 2015-05-27 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 2 [patent_figures_cnt] => 2 [patent_no_of_words] => 5171 [patent_no_of_claims] => 8 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 421 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14722365 [rel_patent_id] =>[rel_patent_doc_number] =>)
14/722365
Twin-engined rotorcraft having a fuel supply installation for a power plant auxiliary power unit (APU) May 26, 2015 Issued
Array ( [id] => 11408588 [patent_doc_number] => 09555879 [patent_country] => US [patent_kind] => B1 [patent_issue_date] => 2017-01-31 [patent_title] => 'Aircraft having circular body and blades' [patent_app_type] => utility [patent_app_number] => 14/712062 [patent_app_country] => US [patent_app_date] => 2015-05-14 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 4 [patent_figures_cnt] => 8 [patent_no_of_words] => 4977 [patent_no_of_claims] => 15 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 204 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14712062 [rel_patent_id] =>[rel_patent_doc_number] =>)
14/712062
Aircraft having circular body and blades May 13, 2015 Issued
Array ( [id] => 10347191 [patent_doc_number] => 20150232196 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2015-08-20 [patent_title] => 'SYSTEM AND METHOD FOR AIRCRAFT INCIDENT MITIGATION' [patent_app_type] => utility [patent_app_number] => 14/702693 [patent_app_country] => US [patent_app_date] => 2015-05-02 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 13 [patent_figures_cnt] => 13 [patent_no_of_words] => 5746 [patent_no_of_claims] => 18 [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] => 14702693 [rel_patent_id] =>[rel_patent_doc_number] =>)
14/702693
System and method for aircraft incident mitigation May 1, 2015 Issued
Array ( [id] => 11121524 [patent_doc_number] => 20160318498 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2016-11-03 [patent_title] => 'MULTI ROTOR AIRTRAIN' [patent_app_type] => utility [patent_app_number] => 14/698261 [patent_app_country] => US [patent_app_date] => 2015-04-28 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 8 [patent_figures_cnt] => 8 [patent_no_of_words] => 2061 [patent_no_of_claims] => 1 [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] => 14698261 [rel_patent_id] =>[rel_patent_doc_number] =>)
14/698261
MULTI ROTOR AIRTRAIN Apr 27, 2015 Abandoned
Array ( [id] => 11714595 [patent_doc_number] => 20170183094 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2017-06-29 [patent_title] => 'Convertible Payload Transport Aircraft' [patent_app_type] => utility [patent_app_number] => 15/309539 [patent_app_country] => US [patent_app_date] => 2015-04-24 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 44 [patent_figures_cnt] => 44 [patent_no_of_words] => 8155 [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] => 15309539 [rel_patent_id] =>[rel_patent_doc_number] =>)
15/309539
Convertible Payload Transport Aircraft Apr 23, 2015 Abandoned
Array ( [id] => 11685614 [patent_doc_number] => 09683652 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2017-06-20 [patent_title] => 'Method for the delivery of lubricant to a rotorcraft gearbox' [patent_app_type] => utility [patent_app_number] => 14/693334 [patent_app_country] => US [patent_app_date] => 2015-04-22 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 4 [patent_figures_cnt] => 6 [patent_no_of_words] => 3869 [patent_no_of_claims] => 20 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 168 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14693334 [rel_patent_id] =>[rel_patent_doc_number] =>)
14/693334
Method for the delivery of lubricant to a rotorcraft gearbox Apr 21, 2015 Issued
Array ( [id] => 11100572 [patent_doc_number] => 20160297542 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2016-10-13 [patent_title] => 'LIGHTNING DAMAGE RESISTANT AIRCRAFT SKIN FASTENERS' [patent_app_type] => utility [patent_app_number] => 14/684181 [patent_app_country] => US [patent_app_date] => 2015-04-10 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 5 [patent_figures_cnt] => 5 [patent_no_of_words] => 5557 [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] => 14684181 [rel_patent_id] =>[rel_patent_doc_number] =>)
14/684181
Lightning damage resistant aircraft skin fasteners Apr 9, 2015 Issued
Array ( [id] => 11589369 [patent_doc_number] => 20170113780 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2017-04-27 [patent_title] => 'A PASSENGER AIRCRAFT WITH A DOWNWARDLY FOLDABLE WING TIP DEVICE' [patent_app_type] => utility [patent_app_number] => 15/301858 [patent_app_country] => US [patent_app_date] => 2015-04-02 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 5 [patent_figures_cnt] => 5 [patent_no_of_words] => 4647 [patent_no_of_claims] => 22 [patent_no_of_ind_claims] => 6 [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] => 15301858 [rel_patent_id] =>[rel_patent_doc_number] =>)
15/301858
Passenger aircraft with a downwardly foldable wing tip device Apr 1, 2015 Issued
Array ( [id] => 11705836 [patent_doc_number] => 20170174335 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2017-06-22 [patent_title] => 'ROTOR-LIFT AIRCRAFT' [patent_app_type] => utility [patent_app_number] => 15/129732 [patent_app_country] => US [patent_app_date] => 2015-03-27 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 17 [patent_figures_cnt] => 17 [patent_no_of_words] => 3533 [patent_no_of_claims] => 17 [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] => 15129732 [rel_patent_id] =>[rel_patent_doc_number] =>)
15/129732
ROTOR-LIFT AIRCRAFT Mar 26, 2015 Abandoned
Array ( [id] => 10655737 [patent_doc_number] => 20160001881 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2016-01-07 [patent_title] => 'MISSION-ADAPTIVE ROTOR BLADE WITH CIRCULATION CONTROL' [patent_app_type] => utility [patent_app_number] => 14/665047 [patent_app_country] => US [patent_app_date] => 2015-03-23 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 9 [patent_figures_cnt] => 9 [patent_no_of_words] => 6227 [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] => 14665047 [rel_patent_id] =>[rel_patent_doc_number] =>)
14/665047
Mission-adaptive rotor blade with circulation control Mar 22, 2015 Issued
Array ( [id] => 18234057 [patent_doc_number] => 11598609 [patent_country] => US [patent_kind] => B1 [patent_issue_date] => 2023-03-07 [patent_title] => Wide-angle seeker [patent_app_type] => utility [patent_app_number] => 14/656293 [patent_app_country] => US [patent_app_date] => 2015-03-12 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 8 [patent_figures_cnt] => 13 [patent_no_of_words] => 6422 [patent_no_of_claims] => 30 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 107 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14656293 [rel_patent_id] =>[rel_patent_doc_number] =>)
14/656293
Wide-angle seeker Mar 11, 2015 Issued
Array ( [id] => 11698496 [patent_doc_number] => 09688398 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2017-06-27 [patent_title] => 'Long endurance vertical takeoff and landing aircraft' [patent_app_type] => utility [patent_app_number] => 14/643857 [patent_app_country] => US [patent_app_date] => 2015-03-10 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 12 [patent_figures_cnt] => 13 [patent_no_of_words] => 9357 [patent_no_of_claims] => 20 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 188 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14643857 [rel_patent_id] =>[rel_patent_doc_number] =>)
14/643857
Long endurance vertical takeoff and landing aircraft Mar 9, 2015 Issued
Array ( [id] => 12205565 [patent_doc_number] => 20180050791 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2018-02-22 [patent_title] => 'AIRCRAFT LANDING GEAR AND METHOD' [patent_app_type] => utility [patent_app_number] => 15/556590 [patent_app_country] => US [patent_app_date] => 2015-03-10 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 17 [patent_figures_cnt] => 17 [patent_no_of_words] => 10560 [patent_no_of_claims] => 21 [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] => 15556590 [rel_patent_id] =>[rel_patent_doc_number] =>)
15/556590
Amphibious aircraft, landing gear, and method Mar 9, 2015 Issued
Array ( [id] => 11698499 [patent_doc_number] => 09688401 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2017-06-27 [patent_title] => 'Methods and systems for retrieving personnel' [patent_app_type] => utility [patent_app_number] => 14/633215 [patent_app_country] => US [patent_app_date] => 2015-02-27 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 7 [patent_figures_cnt] => 7 [patent_no_of_words] => 5449 [patent_no_of_claims] => 16 [patent_no_of_ind_claims] => 1 [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] => 14633215 [rel_patent_id] =>[rel_patent_doc_number] =>)
14/633215
Methods and systems for retrieving personnel Feb 26, 2015 Issued
Array ( [id] => 11561397 [patent_doc_number] => 09623966 [patent_country] => US [patent_kind] => B1 [patent_issue_date] => 2017-04-18 [patent_title] => 'Blade root attachment apparatus and method' [patent_app_type] => utility [patent_app_number] => 14/544854 [patent_app_country] => US [patent_app_date] => 2015-02-25 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 11 [patent_figures_cnt] => 15 [patent_no_of_words] => 7218 [patent_no_of_claims] => 4 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 256 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14544854 [rel_patent_id] =>[rel_patent_doc_number] =>)
14/544854
Blade root attachment apparatus and method Feb 24, 2015 Issued
Array ( [id] => 10422170 [patent_doc_number] => 20150307180 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2015-10-29 [patent_title] => 'HEAT TRANSFER SYSTEM FOR AIRCRAFT STRUCTURES' [patent_app_type] => utility [patent_app_number] => 14/630819 [patent_app_country] => US [patent_app_date] => 2015-02-25 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 13 [patent_figures_cnt] => 13 [patent_no_of_words] => 3261 [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] => 14630819 [rel_patent_id] =>[rel_patent_doc_number] =>)
14/630819
Heat transfer system for aircraft structures Feb 24, 2015 Issued
Array ( [id] => 10399066 [patent_doc_number] => 20150284073 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2015-10-08 [patent_title] => 'BILATERALLY ASYMMETRIC DESIGN FOR MINIMIZING WAVE DRAG' [patent_app_type] => utility [patent_app_number] => 14/628218 [patent_app_country] => US [patent_app_date] => 2015-02-21 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 12 [patent_figures_cnt] => 12 [patent_no_of_words] => 10972 [patent_no_of_claims] => 20 [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] => 14628218 [rel_patent_id] =>[rel_patent_doc_number] =>)
14/628218
Bilaterally asymmetric design for minimizing wave drag Feb 20, 2015 Issued
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