William L. Oen

Array ( [id] => 6718541 [patent_doc_number] => 20030052228 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2003-03-20 [patent_title] => 'Tri-body aircraft and methods for their manufacture' [patent_app_type] => new [patent_app_number] => 10/271631 [patent_app_country] => US [patent_app_date] => 2002-10-15 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 6 [patent_figures_cnt] => 6 [patent_no_of_words] => 4697 [patent_no_of_claims] => 52 [patent_no_of_ind_claims] => 5 [patent_words_short_claim] => 77 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] => publications/A1/0052/20030052228.pdf [firstpage_image] =>[orig_patent_app_number] => 10271631 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 6686242 [patent_doc_number] => 20030029965 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2003-02-13 [patent_title] => 'Telescopic vertical take-off aircraft' [patent_app_type] => new [patent_app_number] => 10/265378 [patent_app_country] => US [patent_app_date] => 2002-10-07 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 15 [patent_figures_cnt] => 15 [patent_no_of_words] => 3161 [patent_no_of_claims] => 23 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 307 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] => publications/A1/0029/20030029965.pdf [firstpage_image] =>[orig_patent_app_number] => 10265378 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 1120310 [patent_doc_number] => 06793173 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2004-09-21 [patent_title] => 'Automatic control device for a helicopter and automatic control system comprising such a device' [patent_app_type] => B2 [patent_app_number] => 10/264256 [patent_app_country] => US [patent_app_date] => 2002-10-04 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 4 [patent_figures_cnt] => 4 [patent_no_of_words] => 5868 [patent_no_of_claims] => 9 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 208 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/06/793/06793173.pdf [firstpage_image] =>[orig_patent_app_number] => 10264256 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 6858819 [patent_doc_number] => 20030089827 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2003-05-15 [patent_title] => 'Control device and method for emergency opening of an aircraft evacuation door' [patent_app_type] => new [patent_app_number] => 10/264610 [patent_app_country] => US [patent_app_date] => 2002-10-03 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 5 [patent_figures_cnt] => 5 [patent_no_of_words] => 3864 [patent_no_of_claims] => 12 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 47 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] => publications/A1/0089/20030089827.pdf [firstpage_image] =>[orig_patent_app_number] => 10264610 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 7278651 [patent_doc_number] => 20040061028 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2004-04-01 [patent_title] => 'METHOD OF OPERATING A SATELLITE FOR END-OF-LIFE MANEUVERS' [patent_app_type] => new [patent_app_number] => 10/255540 [patent_app_country] => US [patent_app_date] => 2002-09-26 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 3 [patent_figures_cnt] => 3 [patent_no_of_words] => 2260 [patent_no_of_claims] => 20 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 53 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] => publications/A1/0061/20040061028.pdf [firstpage_image] =>[orig_patent_app_number] => 10255540 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 1084598 [patent_doc_number] => 06830217 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2004-12-14 [patent_title] => 'Integrated cockpit door lock and access system' [patent_app_type] => B2 [patent_app_number] => 10/255916 [patent_app_country] => US [patent_app_date] => 2002-09-26 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 10 [patent_figures_cnt] => 15 [patent_no_of_words] => 5757 [patent_no_of_claims] => 27 [patent_no_of_ind_claims] => 5 [patent_words_short_claim] => 174 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/06/830/06830217.pdf [firstpage_image] =>[orig_patent_app_number] => 10255916 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 6646029 [patent_doc_number] => 20030075642 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2003-04-24 [patent_title] => 'Internet linked environment data collection system and method' [patent_app_type] => new [patent_app_number] => 10/254510 [patent_app_country] => US [patent_app_date] => 2002-09-26 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 24 [patent_figures_cnt] => 24 [patent_no_of_words] => 11666 [patent_no_of_claims] => 80 [patent_no_of_ind_claims] => 4 [patent_words_short_claim] => 40 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] => publications/A1/0075/20030075642.pdf [firstpage_image] =>[orig_patent_app_number] => 10254510 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 6867552 [patent_doc_number] => 20030080241 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2003-05-01 [patent_title] => 'Air launch of payload carrying vehicle from a transport aircraft' [patent_app_type] => new [patent_app_number] => 10/256249 [patent_app_country] => US [patent_app_date] => 2002-09-26 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 4 [patent_figures_cnt] => 4 [patent_no_of_words] => 2435 [patent_no_of_claims] => 20 [patent_no_of_ind_claims] => 4 [patent_words_short_claim] => 66 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] => publications/A1/0080/20030080241.pdf [firstpage_image] =>[orig_patent_app_number] => 10256249 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 1302515 [patent_doc_number] => 06612521 [patent_country] => US [patent_kind] => B1 [patent_issue_date] => 2003-09-02 [patent_title] => 'Safety pitot tube cover' [patent_app_type] => B1 [patent_app_number] => 10/253301 [patent_app_country] => US [patent_app_date] => 2002-09-24 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 3 [patent_figures_cnt] => 6 [patent_no_of_words] => 2008 [patent_no_of_claims] => 9 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 101 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/06/612/06612521.pdf [firstpage_image] =>[orig_patent_app_number] => 10253301 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 7444311 [patent_doc_number] => 20040051002 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2004-03-18 [patent_title] => 'Environmental control system' [patent_app_type] => new [patent_app_number] => 10/246157 [patent_app_country] => US [patent_app_date] => 2002-09-18 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 2 [patent_figures_cnt] => 2 [patent_no_of_words] => 2481 [patent_no_of_claims] => 14 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 173 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] => publications/A1/0051/20040051002.pdf [firstpage_image] =>[orig_patent_app_number] => 10246157 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 235645 [patent_doc_number] => 07594623 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2009-09-29 [patent_title] => 'Torsionally de-coupled engine mount system' [patent_app_type] => utility [patent_app_number] => 10/528213 [patent_app_country] => US [patent_app_date] => 2002-09-17 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 9 [patent_figures_cnt] => 17 [patent_no_of_words] => 5884 [patent_no_of_claims] => 5 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 244 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/07/594/07594623.pdf [firstpage_image] =>[orig_patent_app_number] => 10528213 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 7444297 [patent_doc_number] => 20040050999 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2004-03-18 [patent_title] => 'Active vibration control system' [patent_app_type] => new [patent_app_number] => 10/244583 [patent_app_country] => US [patent_app_date] => 2002-09-16 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 16 [patent_figures_cnt] => 16 [patent_no_of_words] => 11725 [patent_no_of_claims] => 16 [patent_no_of_ind_claims] => 4 [patent_words_short_claim] => 76 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] => publications/A1/0050/20040050999.pdf [firstpage_image] =>[orig_patent_app_number] => 10244583 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 1238577 [patent_doc_number] => 06682017 [patent_country] => US [patent_kind] => B1 [patent_issue_date] => 2004-01-27 [patent_title] => 'Aircraft with a detachable passenger escape cabin and an aircraft with airbags' [patent_app_type] => B1 [patent_app_number] => 10/220977 [patent_app_country] => US [patent_app_date] => 2002-09-09 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 18 [patent_figures_cnt] => 44 [patent_no_of_words] => 7654 [patent_no_of_claims] => 8 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 419 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/06/682/06682017.pdf [firstpage_image] =>[orig_patent_app_number] => 10220977 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 7335334 [patent_doc_number] => 20040244334 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2004-12-09 [patent_title] => 'Composite material structure' [patent_app_type] => new [patent_app_number] => 10/487457 [patent_app_country] => US [patent_app_date] => 2004-02-24 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 4 [patent_figures_cnt] => 4 [patent_no_of_words] => 3661 [patent_no_of_claims] => 11 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 2 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] => publications/A1/0244/20040244334.pdf [firstpage_image] =>[orig_patent_app_number] => 10487457 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 1145838 [patent_doc_number] => 06766987 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2004-07-27 [patent_title] => 'Satellite system and method of deploying same' [patent_app_type] => B2 [patent_app_number] => 10/230424 [patent_app_country] => US [patent_app_date] => 2002-08-28 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 8 [patent_figures_cnt] => 13 [patent_no_of_words] => 3452 [patent_no_of_claims] => 9 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 79 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/06/766/06766987.pdf [firstpage_image] =>[orig_patent_app_number] => 10230424 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 1108409 [patent_doc_number] => 06805320 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2004-10-19 [patent_title] => 'Aircraft landing gear with highly offset strut pivot axis' [patent_app_type] => B2 [patent_app_number] => 10/220526 [patent_app_country] => US [patent_app_date] => 2002-08-28 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 5 [patent_figures_cnt] => 14 [patent_no_of_words] => 4466 [patent_no_of_claims] => 13 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 213 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/06/805/06805320.pdf [firstpage_image] =>[orig_patent_app_number] => 10220526 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 1251525 [patent_doc_number] => 06669137 [patent_country] => US [patent_kind] => B1 [patent_issue_date] => 2003-12-30 [patent_title] => 'Air vehicle having rotor/scissors wing' [patent_app_type] => B1 [patent_app_number] => 10/227955 [patent_app_country] => US [patent_app_date] => 2002-08-26 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 5 [patent_figures_cnt] => 9 [patent_no_of_words] => 4719 [patent_no_of_claims] => 14 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 192 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/06/669/06669137.pdf [firstpage_image] =>[orig_patent_app_number] => 10227955 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 7379281 [patent_doc_number] => 20040035979 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2004-02-26 [patent_title] => 'Integrally stiffened axial load carrying skin panels for primary aircraft structure and closed loop manufacturing methods for making the same' [patent_app_type] => new [patent_app_number] => 10/226922 [patent_app_country] => US [patent_app_date] => 2002-08-23 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 11 [patent_figures_cnt] => 11 [patent_no_of_words] => 8026 [patent_no_of_claims] => 33 [patent_no_of_ind_claims] => 4 [patent_words_short_claim] => 14 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] => publications/A1/0035/20040035979.pdf [firstpage_image] =>[orig_patent_app_number] => 10226922 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 6747842 [patent_doc_number] => 20030042362 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2003-03-06 [patent_title] => 'Remediation of fan source production of smoke in an aircraft cabin' [patent_app_type] => new [patent_app_number] => 10/222494 [patent_app_country] => US [patent_app_date] => 2002-08-15 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 7 [patent_figures_cnt] => 7 [patent_no_of_words] => 1640 [patent_no_of_claims] => 13 [patent_no_of_ind_claims] => 4 [patent_words_short_claim] => 60 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] => publications/A1/0042/20030042362.pdf [firstpage_image] =>[orig_patent_app_number] => 10222494 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 7367763 [patent_doc_number] => 20040026567 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2004-02-12 [patent_title] => 'Fluid delivery system for heat exchange garments' [patent_app_type] => new [patent_app_number] => 10/215428 [patent_app_country] => US [patent_app_date] => 2002-08-09 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 9 [patent_figures_cnt] => 9 [patent_no_of_words] => 8663 [patent_no_of_claims] => 29 [patent_no_of_ind_claims] => 4 [patent_words_short_claim] => 108 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] => publications/A1/0026/20040026567.pdf [firstpage_image] =>[orig_patent_app_number] => 10215428 [rel_patent_id] =>[rel_patent_doc_number] =>)