William L. Oen

Array ( [id] => 980884 [patent_doc_number] => 06926234 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2005-08-09 [patent_title] => 'Electromechanical turbojet thrust reverser with continuous position control' [patent_app_type] => utility [patent_app_number] => 10/678104 [patent_app_country] => US [patent_app_date] => 2003-10-06 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 2 [patent_figures_cnt] => 2 [patent_no_of_words] => 3198 [patent_no_of_claims] => 6 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 154 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/06/926/06926234.pdf [firstpage_image] =>[orig_patent_app_number] => 10678104 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 1033110 [patent_doc_number] => 06874735 [patent_country] => US [patent_kind] => B1 [patent_issue_date] => 2005-04-05 [patent_title] => 'Automated airline baggage transportation system' [patent_app_type] => utility [patent_app_number] => 10/678923 [patent_app_country] => US [patent_app_date] => 2003-10-06 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 10 [patent_figures_cnt] => 13 [patent_no_of_words] => 2342 [patent_no_of_claims] => 15 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 193 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/06/874/06874735.pdf [firstpage_image] =>[orig_patent_app_number] => 10678923 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 7370733 [patent_doc_number] => 20040079840 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2004-04-29 [patent_title] => 'Aircraft lift control system' [patent_app_type] => new [patent_app_number] => 10/674367 [patent_app_country] => US [patent_app_date] => 2003-09-30 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 4 [patent_figures_cnt] => 4 [patent_no_of_words] => 1688 [patent_no_of_claims] => 28 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 68 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] => publications/A1/0079/20040079840.pdf [firstpage_image] =>[orig_patent_app_number] => 10674367 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 1004140 [patent_doc_number] => 06905093 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2005-06-14 [patent_title] => 'Deployment mechanism for stowable fins' [patent_app_type] => utility [patent_app_number] => 10/672533 [patent_app_country] => US [patent_app_date] => 2003-09-26 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 11 [patent_figures_cnt] => 26 [patent_no_of_words] => 8943 [patent_no_of_claims] => 20 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 67 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/06/905/06905093.pdf [firstpage_image] =>[orig_patent_app_number] => 10672533 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 6963624 [patent_doc_number] => 20050230521 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2005-10-20 [patent_title] => 'Powerchute apparatus' [patent_app_type] => utility [patent_app_number] => 10/669126 [patent_app_country] => US [patent_app_date] => 2003-09-23 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 8 [patent_figures_cnt] => 8 [patent_no_of_words] => 2648 [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] => publications/A1/0230/20050230521.pdf [firstpage_image] =>[orig_patent_app_number] => 10669126 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 7124980 [patent_doc_number] => 20050056724 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2005-03-17 [patent_title] => 'Helicopter turbine engine protection system' [patent_app_type] => utility [patent_app_number] => 10/659334 [patent_app_country] => US [patent_app_date] => 2003-09-11 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 5 [patent_figures_cnt] => 5 [patent_no_of_words] => 2296 [patent_no_of_claims] => 14 [patent_no_of_ind_claims] => 10 [patent_words_short_claim] => 0 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] => publications/A1/0056/20050056724.pdf [firstpage_image] =>[orig_patent_app_number] => 10659334 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 766851 [patent_doc_number] => 07004427 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2006-02-28 [patent_title] => 'Retractable lifting blades for aircraft' [patent_app_type] => utility [patent_app_number] => 10/657838 [patent_app_country] => US [patent_app_date] => 2003-09-09 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 17 [patent_figures_cnt] => 28 [patent_no_of_words] => 6928 [patent_no_of_claims] => 29 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 83 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/07/004/07004427.pdf [firstpage_image] =>[orig_patent_app_number] => 10657838 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 7143809 [patent_doc_number] => 20040169111 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2004-09-02 [patent_title] => 'Control unit for controlling paragliders, unlatching apparatus for triggering a flaring maneuver to be conducted by a load-bearing paraglider system, and a paraglider system' [patent_app_type] => new [patent_app_number] => 10/655544 [patent_app_country] => US [patent_app_date] => 2003-09-05 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 11 [patent_figures_cnt] => 11 [patent_no_of_words] => 5802 [patent_no_of_claims] => 26 [patent_no_of_ind_claims] => 4 [patent_words_short_claim] => 228 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] => publications/A1/0169/20040169111.pdf [firstpage_image] =>[orig_patent_app_number] => 10655544 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 7267630 [patent_doc_number] => 20040056148 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2004-03-25 [patent_title] => 'Satellite system and method of deploying same' [patent_app_type] => new [patent_app_number] => 10/657452 [patent_app_country] => US [patent_app_date] => 2003-09-05 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 9 [patent_figures_cnt] => 9 [patent_no_of_words] => 3529 [patent_no_of_claims] => 20 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 46 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] => publications/A1/0056/20040056148.pdf [firstpage_image] =>[orig_patent_app_number] => 10657452 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 7283500 [patent_doc_number] => 20040144891 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2004-07-29 [patent_title] => 'Vertical take-off aircraft - B' [patent_app_type] => new [patent_app_number] => 10/651948 [patent_app_country] => US [patent_app_date] => 2003-09-02 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 15 [patent_figures_cnt] => 15 [patent_no_of_words] => 2691 [patent_no_of_claims] => 36 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 287 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] => publications/A1/0144/20040144891.pdf [firstpage_image] =>[orig_patent_app_number] => 10651948 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 7080385 [patent_doc_number] => 20050045765 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2005-03-03 [patent_title] => 'Apparatus for increase of aircraft lift and maneuverability' [patent_app_type] => utility [patent_app_number] => 10/653013 [patent_app_country] => US [patent_app_date] => 2003-08-28 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 6 [patent_figures_cnt] => 6 [patent_no_of_words] => 4459 [patent_no_of_claims] => 66 [patent_no_of_ind_claims] => 7 [patent_words_short_claim] => 0 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] => publications/A1/0045/20050045765.pdf [firstpage_image] =>[orig_patent_app_number] => 10653013 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 5675351 [patent_doc_number] => 20060180706 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2006-08-17 [patent_title] => 'Method for seizing an object' [patent_app_type] => utility [patent_app_number] => 10/525692 [patent_app_country] => US [patent_app_date] => 2003-08-20 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 7 [patent_figures_cnt] => 7 [patent_no_of_words] => 5074 [patent_no_of_claims] => 20 [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/A1/0180/20060180706.pdf [firstpage_image] =>[orig_patent_app_number] => 10525692 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 492273 [patent_doc_number] => 07207522 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2007-04-24 [patent_title] => 'Safety device trigger for activating a safety device' [patent_app_type] => utility [patent_app_number] => 10/641915 [patent_app_country] => US [patent_app_date] => 2003-08-15 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 10 [patent_figures_cnt] => 15 [patent_no_of_words] => 4733 [patent_no_of_claims] => 13 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 78 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/07/207/07207522.pdf [firstpage_image] =>[orig_patent_app_number] => 10641915 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 7396134 [patent_doc_number] => 20040104305 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2004-06-03 [patent_title] => 'AIRCRAFT WHEEL SPIN-UP ROTOR' [patent_app_type] => new [patent_app_number] => 10/604724 [patent_app_country] => US [patent_app_date] => 2003-08-13 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 5 [patent_figures_cnt] => 5 [patent_no_of_words] => 1716 [patent_no_of_claims] => 5 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 19 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] => publications/A1/0104/20040104305.pdf [firstpage_image] =>[orig_patent_app_number] => 10604724 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 5773686 [patent_doc_number] => 20060102799 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2006-05-18 [patent_title] => 'Device for the generation of eddies and method for operation of said device' [patent_app_type] => utility [patent_app_number] => 10/523512 [patent_app_country] => US [patent_app_date] => 2003-08-12 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 8 [patent_figures_cnt] => 8 [patent_no_of_words] => 6760 [patent_no_of_claims] => 21 [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] => publications/A1/0102/20060102799.pdf [firstpage_image] =>[orig_patent_app_number] => 10523512 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 7309825 [patent_doc_number] => 20040031880 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2004-02-19 [patent_title] => 'Aircraft and propulsion system for an aircraft, and operating method' [patent_app_type] => new [patent_app_number] => 10/275211 [patent_app_country] => US [patent_app_date] => 2003-08-04 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 6 [patent_figures_cnt] => 6 [patent_no_of_words] => 4649 [patent_no_of_claims] => 44 [patent_no_of_ind_claims] => 44 [patent_words_short_claim] => 15 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] => publications/A1/0031/20040031880.pdf [firstpage_image] =>[orig_patent_app_number] => 10275211 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 7030592 [patent_doc_number] => 20050029398 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2005-02-10 [patent_title] => 'Flying craft camera and sensor mechanized lift platform' [patent_app_type] => utility [patent_app_number] => 10/633347 [patent_app_country] => US [patent_app_date] => 2003-08-04 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 4 [patent_figures_cnt] => 4 [patent_no_of_words] => 1431 [patent_no_of_claims] => 23 [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/A1/0029/20050029398.pdf [firstpage_image] =>[orig_patent_app_number] => 10633347 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 6969532 [patent_doc_number] => 20050035242 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2005-02-17 [patent_title] => 'Proactive optical trajectory following system' [patent_app_type] => utility [patent_app_number] => 10/633353 [patent_app_country] => US [patent_app_date] => 2003-07-31 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 9 [patent_figures_cnt] => 9 [patent_no_of_words] => 3347 [patent_no_of_claims] => 78 [patent_no_of_ind_claims] => 12 [patent_words_short_claim] => 0 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] => publications/A1/0035/20050035242.pdf [firstpage_image] =>[orig_patent_app_number] => 10633353 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 7147226 [patent_doc_number] => 20050023409 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2005-02-03 [patent_title] => 'System and method for munition impact assessment' [patent_app_type] => utility [patent_app_number] => 10/627630 [patent_app_country] => US [patent_app_date] => 2003-07-28 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 6 [patent_figures_cnt] => 6 [patent_no_of_words] => 5308 [patent_no_of_claims] => 24 [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/A1/0023/20050023409.pdf [firstpage_image] =>[orig_patent_app_number] => 10627630 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 7030604 [patent_doc_number] => 20050029405 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2005-02-10 [patent_title] => 'Predicting, bounding and mitigating satellite attitude disturbances arising from infrared earth sensors for satellites in inclined, elliptical orbits' [patent_app_type] => utility [patent_app_number] => 10/627534 [patent_app_country] => US [patent_app_date] => 2003-07-25 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 7 [patent_figures_cnt] => 7 [patent_no_of_words] => 2236 [patent_no_of_claims] => 7 [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] => publications/A1/0029/20050029405.pdf [firstpage_image] =>[orig_patent_app_number] => 10627534 [rel_patent_id] =>[rel_patent_doc_number] =>)