Ronald Baum

Array ( [id] => 7086420 [patent_doc_number] => 20050006532 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2005-01-13 [patent_title] => 'Propeller system for kite' [patent_app_type] => utility [patent_app_number] => 10/617220 [patent_app_country] => US [patent_app_date] => 2003-07-10 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 5 [patent_figures_cnt] => 5 [patent_no_of_words] => 1633 [patent_no_of_claims] => 27 [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/A1/0006/20050006532.pdf [firstpage_image] =>[orig_patent_app_number] => 10617220 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 7086415 [patent_doc_number] => 20050006527 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2005-01-13 [patent_title] => 'Background radiation masking system' [patent_app_type] => utility [patent_app_number] => 10/614567 [patent_app_country] => US [patent_app_date] => 2003-07-07 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 0 [patent_figures_cnt] => 0 [patent_no_of_words] => 109 [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] => publications/A1/0006/20050006527.pdf [firstpage_image] =>[orig_patent_app_number] => 10614567 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 7204102 [patent_doc_number] => 20040069900 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2004-04-15 [patent_title] => 'Reverse velocity, differential pressure, hydraulic, travel from earth to outer space and back' [patent_app_type] => new [patent_app_number] => 10/612259 [patent_app_country] => US [patent_app_date] => 2003-07-03 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 8 [patent_figures_cnt] => 8 [patent_no_of_words] => 3699 [patent_no_of_claims] => 12 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 26 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] => publications/A1/0069/20040069900.pdf [firstpage_image] =>[orig_patent_app_number] => 10612259 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 1102289 [patent_doc_number] => 06811119 [patent_country] => US [patent_kind] => B1 [patent_issue_date] => 2004-11-02 [patent_title] => 'Aircraft service pit latch' [patent_app_type] => B1 [patent_app_number] => 10/613469 [patent_app_country] => US [patent_app_date] => 2003-07-02 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 7 [patent_figures_cnt] => 7 [patent_no_of_words] => 4887 [patent_no_of_claims] => 20 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 208 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/06/811/06811119.pdf [firstpage_image] =>[orig_patent_app_number] => 10613469 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 1090181 [patent_doc_number] => 06824105 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2004-11-30 [patent_title] => 'Drogue for in-flight refueling' [patent_app_type] => B2 [patent_app_number] => 10/451907 [patent_app_country] => US [patent_app_date] => 2003-06-27 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 3 [patent_figures_cnt] => 6 [patent_no_of_words] => 2946 [patent_no_of_claims] => 19 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 112 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/06/824/06824105.pdf [firstpage_image] =>[orig_patent_app_number] => 10451907 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 7455290 [patent_doc_number] => 20040118969 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2004-06-24 [patent_title] => 'Hydrogen powered aircraft' [patent_app_type] => new [patent_app_number] => 10/600258 [patent_app_country] => US [patent_app_date] => 2003-06-20 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 9 [patent_figures_cnt] => 9 [patent_no_of_words] => 9000 [patent_no_of_claims] => 39 [patent_no_of_ind_claims] => 5 [patent_words_short_claim] => 51 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] => publications/A1/0118/20040118969.pdf [firstpage_image] =>[orig_patent_app_number] => 10600258 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 7385701 [patent_doc_number] => 20040021041 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2004-02-05 [patent_title] => 'Sparkjet actuator' [patent_app_type] => new [patent_app_number] => 10/464160 [patent_app_country] => US [patent_app_date] => 2003-06-18 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 9 [patent_figures_cnt] => 9 [patent_no_of_words] => 2051 [patent_no_of_claims] => 12 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 23 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] => publications/A1/0021/20040021041.pdf [firstpage_image] =>[orig_patent_app_number] => 10464160 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 7190579 [patent_doc_number] => 20050040284 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2005-02-24 [patent_title] => 'THRUST REVERSER SYSTEM ACTUATOR HAVING AN INTEGRAL TORQUE LIMITER' [patent_app_type] => utility [patent_app_number] => 10/465413 [patent_app_country] => US [patent_app_date] => 2003-06-18 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 6 [patent_figures_cnt] => 6 [patent_no_of_words] => 3801 [patent_no_of_claims] => 31 [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] => publications/A1/0040/20050040284.pdf [firstpage_image] =>[orig_patent_app_number] => 10465413 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 453907 [patent_doc_number] => 07243880 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2007-07-17 [patent_title] => 'Landing gear door assembly' [patent_app_type] => utility [patent_app_number] => 10/518657 [patent_app_country] => US [patent_app_date] => 2003-06-18 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 5 [patent_figures_cnt] => 7 [patent_no_of_words] => 4895 [patent_no_of_claims] => 20 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 184 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/07/243/07243880.pdf [firstpage_image] =>[orig_patent_app_number] => 10518657 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 7058744 [patent_doc_number] => 20050001103 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2005-01-06 [patent_title] => 'VARIABLE TRAILING EDGE GEOMETRY AND SPANLOAD CONTROL' [patent_app_type] => utility [patent_app_number] => 10/463469 [patent_app_country] => US [patent_app_date] => 2003-06-17 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 9 [patent_figures_cnt] => 9 [patent_no_of_words] => 3630 [patent_no_of_claims] => 26 [patent_no_of_ind_claims] => 8 [patent_words_short_claim] => 0 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] => publications/A1/0001/20050001103.pdf [firstpage_image] =>[orig_patent_app_number] => 10463469 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 7139762 [patent_doc_number] => 20050116087 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2005-06-02 [patent_title] => 'Aircraft converts drag to lift' [patent_app_type] => utility [patent_app_number] => 10/460275 [patent_app_country] => US [patent_app_date] => 2003-06-11 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 3 [patent_figures_cnt] => 3 [patent_no_of_words] => 4006 [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] => publications/A1/0116/20050116087.pdf [firstpage_image] =>[orig_patent_app_number] => 10460275 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 417672 [patent_doc_number] => 07275720 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2007-10-02 [patent_title] => 'Actively cooled ceramic thermal protection system' [patent_app_type] => utility [patent_app_number] => 10/457594 [patent_app_country] => US [patent_app_date] => 2003-06-09 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 2 [patent_figures_cnt] => 3 [patent_no_of_words] => 1813 [patent_no_of_claims] => 12 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 155 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/07/275/07275720.pdf [firstpage_image] =>[orig_patent_app_number] => 10457594 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 1120314 [patent_doc_number] => 06793176 [patent_country] => US [patent_kind] => B1 [patent_issue_date] => 2004-09-21 [patent_title] => 'Automatic control of air vehicle during catapult launch' [patent_app_type] => B1 [patent_app_number] => 10/456727 [patent_app_country] => US [patent_app_date] => 2003-06-06 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 4 [patent_figures_cnt] => 5 [patent_no_of_words] => 3802 [patent_no_of_claims] => 19 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 152 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/06/793/06793176.pdf [firstpage_image] =>[orig_patent_app_number] => 10456727 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 750165 [patent_doc_number] => 07017860 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2006-03-28 [patent_title] => 'Control and fixing device for the sail of a kite' [patent_app_type] => utility [patent_app_number] => 10/505763 [patent_app_country] => US [patent_app_date] => 2003-06-03 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 7 [patent_figures_cnt] => 7 [patent_no_of_words] => 3490 [patent_no_of_claims] => 19 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 179 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/07/017/07017860.pdf [firstpage_image] =>[orig_patent_app_number] => 10505763 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 1172333 [patent_doc_number] => 06739554 [patent_country] => US [patent_kind] => B1 [patent_issue_date] => 2004-05-25 [patent_title] => 'Aircraft weapons bay acoustic resonance suppression system' [patent_app_type] => B1 [patent_app_number] => 10/456143 [patent_app_country] => US [patent_app_date] => 2003-06-02 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 4 [patent_figures_cnt] => 8 [patent_no_of_words] => 3746 [patent_no_of_claims] => 12 [patent_no_of_ind_claims] => 6 [patent_words_short_claim] => 96 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/06/739/06739554.pdf [firstpage_image] =>[orig_patent_app_number] => 10456143 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 1149812 [patent_doc_number] => 06761334 [patent_country] => US [patent_kind] => B1 [patent_issue_date] => 2004-07-13 [patent_title] => 'Aircraft passenger safety module' [patent_app_type] => B1 [patent_app_number] => 10/445446 [patent_app_country] => US [patent_app_date] => 2003-05-28 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 3 [patent_figures_cnt] => 4 [patent_no_of_words] => 3699 [patent_no_of_claims] => 2 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 156 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/06/761/06761334.pdf [firstpage_image] =>[orig_patent_app_number] => 10445446 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 1011753 [patent_doc_number] => 06896220 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2005-05-24 [patent_title] => 'Munition with integrity gated go/no-go decision' [patent_app_type] => utility [patent_app_number] => 10/444937 [patent_app_country] => US [patent_app_date] => 2003-05-23 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 8 [patent_figures_cnt] => 8 [patent_no_of_words] => 7140 [patent_no_of_claims] => 12 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 77 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/06/896/06896220.pdf [firstpage_image] =>[orig_patent_app_number] => 10444937 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 6819934 [patent_doc_number] => 20030218095 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2003-11-27 [patent_title] => 'Individual module for aircraft passengers' [patent_app_type] => new [patent_app_number] => 10/441399 [patent_app_country] => US [patent_app_date] => 2003-05-20 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 5 [patent_figures_cnt] => 5 [patent_no_of_words] => 4299 [patent_no_of_claims] => 39 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 73 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] => publications/A1/0218/20030218095.pdf [firstpage_image] =>[orig_patent_app_number] => 10441399 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 1190656 [patent_doc_number] => 06729583 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2004-05-04 [patent_title] => 'Device for articulating a flap to an aircraft aerodynamic surface' [patent_app_type] => B2 [patent_app_number] => 10/440300 [patent_app_country] => US [patent_app_date] => 2003-05-19 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 3 [patent_figures_cnt] => 8 [patent_no_of_words] => 2873 [patent_no_of_claims] => 16 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 305 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/06/729/06729583.pdf [firstpage_image] =>[orig_patent_app_number] => 10440300 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 1149750 [patent_doc_number] => 06761330 [patent_country] => US [patent_kind] => B1 [patent_issue_date] => 2004-07-13 [patent_title] => 'Rocket accuracy improvement device' [patent_app_type] => B1 [patent_app_number] => 10/457695 [patent_app_country] => US [patent_app_date] => 2003-05-19 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 2 [patent_figures_cnt] => 2 [patent_no_of_words] => 1053 [patent_no_of_claims] => 6 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 137 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/06/761/06761330.pdf [firstpage_image] =>[orig_patent_app_number] => 10457695 [rel_patent_id] =>[rel_patent_doc_number] =>)