Ronald B. Abelson

Array ( [id] => 9949354 [patent_doc_number] => 08998127 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2015-04-07 [patent_title] => 'Pre-landing, rotor-spin-up apparatus and method' [patent_app_type] => utility [patent_app_number] => 13/334261 [patent_app_country] => US [patent_app_date] => 2011-12-22 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 9 [patent_figures_cnt] => 15 [patent_no_of_words] => 10925 [patent_no_of_claims] => 19 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 126 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13334261 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 10936336 [patent_doc_number] => 20140339357 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2014-11-20 [patent_title] => 'SYSTEM AND METHOD FOR COOLING AN AIRCRAFT WING' [patent_app_type] => utility [patent_app_number] => 14/360925 [patent_app_country] => US [patent_app_date] => 2011-11-29 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 4 [patent_figures_cnt] => 4 [patent_no_of_words] => 3657 [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] => 14360925 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 9942457 [patent_doc_number] => 08991744 [patent_country] => US [patent_kind] => B1 [patent_issue_date] => 2015-03-31 [patent_title] => 'Rotor-mast-tilting apparatus and method for optimized crossing of natural frequencies' [patent_app_type] => utility [patent_app_number] => 13/373412 [patent_app_country] => US [patent_app_date] => 2011-11-14 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 11 [patent_figures_cnt] => 15 [patent_no_of_words] => 9496 [patent_no_of_claims] => 20 [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] => 13373412 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 9994357 [patent_doc_number] => 09038940 [patent_country] => US [patent_kind] => B1 [patent_issue_date] => 2015-05-26 [patent_title] => 'Rotor configuration for reaction drive rotor system' [patent_app_type] => utility [patent_app_number] => 13/373433 [patent_app_country] => US [patent_app_date] => 2011-11-14 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 32 [patent_figures_cnt] => 45 [patent_no_of_words] => 17438 [patent_no_of_claims] => 12 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 193 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13373433 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 10135697 [patent_doc_number] => 09169009 [patent_country] => US [patent_kind] => B1 [patent_issue_date] => 2015-10-27 [patent_title] => 'Hub-mounted auxilliary systems for tipjets in a reaction drive rotor system' [patent_app_type] => utility [patent_app_number] => 13/373421 [patent_app_country] => US [patent_app_date] => 2011-11-14 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 38 [patent_figures_cnt] => 54 [patent_no_of_words] => 19113 [patent_no_of_claims] => 5 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 165 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13373421 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 9942456 [patent_doc_number] => 08991745 [patent_country] => US [patent_kind] => B1 [patent_issue_date] => 2015-03-31 [patent_title] => 'Rotor-mast-tilting apparatus and method for lower flapping loads' [patent_app_type] => utility [patent_app_number] => 13/373414 [patent_app_country] => US [patent_app_date] => 2011-11-14 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 11 [patent_figures_cnt] => 15 [patent_no_of_words] => 9628 [patent_no_of_claims] => 20 [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] => 13373414 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 9942460 [patent_doc_number] => 08991748 [patent_country] => US [patent_kind] => B1 [patent_issue_date] => 2015-03-31 [patent_title] => 'Solid lubricated blade pitch control system for use within a compressed airstream of a reaction driven rotorcraft' [patent_app_type] => utility [patent_app_number] => 13/373406 [patent_app_country] => US [patent_app_date] => 2011-11-14 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 32 [patent_figures_cnt] => 45 [patent_no_of_words] => 17521 [patent_no_of_claims] => 18 [patent_no_of_ind_claims] => 3 [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] => 13373406 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 8165602 [patent_doc_number] => 20120104156 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2012-05-03 [patent_title] => 'USE OF AUXILIARY RUDDERS FOR YAW CONTROL AT LOW SPEED' [patent_app_type] => utility [patent_app_number] => 13/282985 [patent_app_country] => US [patent_app_date] => 2011-10-27 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 25 [patent_figures_cnt] => 25 [patent_no_of_words] => 10891 [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/A1/0104/20120104156.pdf [firstpage_image] =>[orig_patent_app_number] => 13282985 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 8165608 [patent_doc_number] => 20120104157 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2012-05-03 [patent_title] => 'ROTOR DRIVEN AUXILIARY POWER APPARATUS AND METHOD' [patent_app_type] => utility [patent_app_number] => 13/282938 [patent_app_country] => US [patent_app_date] => 2011-10-27 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 25 [patent_figures_cnt] => 25 [patent_no_of_words] => 10700 [patent_no_of_claims] => 19 [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/A1/0104/20120104157.pdf [firstpage_image] =>[orig_patent_app_number] => 13282938 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 8165606 [patent_doc_number] => 20120104154 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2012-05-03 [patent_title] => 'TAIL FAN APPARATUS AND METHODS FOR LOW SPEED YAW CONTROL OF A ROTORCRAFT' [patent_app_type] => utility [patent_app_number] => 13/282749 [patent_app_country] => US [patent_app_date] => 2011-10-27 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 25 [patent_figures_cnt] => 25 [patent_no_of_words] => 10891 [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/A1/0104/20120104154.pdf [firstpage_image] =>[orig_patent_app_number] => 13282749 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 8165603 [patent_doc_number] => 20120104155 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2012-05-03 [patent_title] => 'TAIL JET APPARATUS AND METHOD FOR LOW SPEED YAW CONTROL OF A ROTORCRAFT' [patent_app_type] => utility [patent_app_number] => 13/282815 [patent_app_country] => US [patent_app_date] => 2011-10-27 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 25 [patent_figures_cnt] => 25 [patent_no_of_words] => 10753 [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/A1/0104/20120104155.pdf [firstpage_image] =>[orig_patent_app_number] => 13282815 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 8248752 [patent_doc_number] => 20120153073 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2012-06-21 [patent_title] => 'MISSION-ADAPTIVE ROTOR BLADE' [patent_app_type] => utility [patent_app_number] => 13/282877 [patent_app_country] => US [patent_app_date] => 2011-10-27 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 10 [patent_figures_cnt] => 10 [patent_no_of_words] => 8710 [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/A1/0153/20120153073.pdf [firstpage_image] =>[orig_patent_app_number] => 13282877 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 8165597 [patent_doc_number] => 20120104153 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2012-05-03 [patent_title] => 'GYROPLANE PREROTATION BY COMPRESSED AIR' [patent_app_type] => utility [patent_app_number] => 13/282780 [patent_app_country] => US [patent_app_date] => 2011-10-27 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 11 [patent_figures_cnt] => 11 [patent_no_of_words] => 8729 [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] => publications/A1/0104/20120104153.pdf [firstpage_image] =>[orig_patent_app_number] => 13282780 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 9921083 [patent_doc_number] => 08979032 [patent_country] => US [patent_kind] => B1 [patent_issue_date] => 2015-03-17 [patent_title] => 'Methods and systems for retrieving personnel' [patent_app_type] => utility [patent_app_number] => 13/275974 [patent_app_country] => US [patent_app_date] => 2011-10-18 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 7 [patent_figures_cnt] => 7 [patent_no_of_words] => 5416 [patent_no_of_claims] => 14 [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] => 13275974 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 8764754 [patent_doc_number] => 20130092791 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2013-04-18 [patent_title] => 'METHOD FOR A NOISE ABATEMENT PROCEDURE FOR AN AIRCRAFT' [patent_app_type] => utility [patent_app_number] => 13/276007 [patent_app_country] => US [patent_app_date] => 2011-10-18 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 7 [patent_figures_cnt] => 7 [patent_no_of_words] => 3728 [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] => 13276007 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 7749994 [patent_doc_number] => 20120025012 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2012-02-02 [patent_title] => 'ROTARY WING VEHICLE' [patent_app_type] => utility [patent_app_number] => 13/270872 [patent_app_country] => US [patent_app_date] => 2011-10-11 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 30 [patent_figures_cnt] => 30 [patent_no_of_words] => 7832 [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/A1/0025/20120025012.pdf [firstpage_image] =>[orig_patent_app_number] => 13270872 [rel_patent_id] =>[rel_patent_doc_number] =>)