Hsien Ming Lee

Array ( [id] => 7617940 [patent_doc_number] => 06945499 [patent_country] => US [patent_kind] => B1 [patent_issue_date] => 2005-09-20 [patent_title] => 'Satellite stand-off tether system' [patent_app_type] => utility [patent_app_number] => 10/804911 [patent_app_country] => US [patent_app_date] => 2004-03-19 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 3 [patent_figures_cnt] => 4 [patent_no_of_words] => 2250 [patent_no_of_claims] => 10 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 88 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/06/945/06945499.pdf [firstpage_image] =>[orig_patent_app_number] => 10804911 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 681336 [patent_doc_number] => 07080807 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2006-07-25 [patent_title] => 'Window frame/seal assembly and method of forming the same' [patent_app_type] => utility [patent_app_number] => 10/788198 [patent_app_country] => US [patent_app_date] => 2004-02-26 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 4 [patent_figures_cnt] => 9 [patent_no_of_words] => 3805 [patent_no_of_claims] => 30 [patent_no_of_ind_claims] => 4 [patent_words_short_claim] => 108 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/07/080/07080807.pdf [firstpage_image] =>[orig_patent_app_number] => 10788198 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 608308 [patent_doc_number] => 07150435 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2006-12-19 [patent_title] => 'Type aircraft' [patent_app_type] => utility [patent_app_number] => 10/774460 [patent_app_country] => US [patent_app_date] => 2004-02-10 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 1 [patent_figures_cnt] => 2 [patent_no_of_words] => 703 [patent_no_of_claims] => 2 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 112 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/07/150/07150435.pdf [firstpage_image] =>[orig_patent_app_number] => 10774460 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 650235 [patent_doc_number] => 07111810 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2006-09-26 [patent_title] => 'Forward pivoted full flying control tail boom' [patent_app_type] => utility [patent_app_number] => 10/774932 [patent_app_country] => US [patent_app_date] => 2004-02-09 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 4 [patent_figures_cnt] => 8 [patent_no_of_words] => 4168 [patent_no_of_claims] => 8 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 93 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/07/111/07111810.pdf [firstpage_image] =>[orig_patent_app_number] => 10774932 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 660802 [patent_doc_number] => 07100867 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2006-09-05 [patent_title] => 'Lifting foil' [patent_app_type] => utility [patent_app_number] => 10/774865 [patent_app_country] => US [patent_app_date] => 2004-02-09 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 14 [patent_figures_cnt] => 34 [patent_no_of_words] => 4885 [patent_no_of_claims] => 17 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 194 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/07/100/07100867.pdf [firstpage_image] =>[orig_patent_app_number] => 10774865 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 7132520 [patent_doc_number] => 20050178886 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2005-08-18 [patent_title] => 'Thrust vector actuation control system and method' [patent_app_type] => utility [patent_app_number] => 10/766994 [patent_app_country] => US [patent_app_date] => 2004-01-28 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 4 [patent_figures_cnt] => 4 [patent_no_of_words] => 3999 [patent_no_of_claims] => 23 [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/A1/0178/20050178886.pdf [firstpage_image] =>[orig_patent_app_number] => 10766994 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 611791 [patent_doc_number] => 07147183 [patent_country] => US [patent_kind] => B1 [patent_issue_date] => 2006-12-12 [patent_title] => 'Lift system for an aerial crane and propulsion system for a vehicle' [patent_app_type] => utility [patent_app_number] => 10/762711 [patent_app_country] => US [patent_app_date] => 2004-01-22 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 4 [patent_figures_cnt] => 9 [patent_no_of_words] => 3065 [patent_no_of_claims] => 35 [patent_no_of_ind_claims] => 4 [patent_words_short_claim] => 166 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/07/147/07147183.pdf [firstpage_image] =>[orig_patent_app_number] => 10762711 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 670537 [patent_doc_number] => 07090166 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2006-08-15 [patent_title] => 'Methods and apparatuses for launching unmanned aircraft, including methods and apparatuses for transmitting forces to the aircraft during launch' [patent_app_type] => utility [patent_app_number] => 10/758948 [patent_app_country] => US [patent_app_date] => 2004-01-16 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 26 [patent_figures_cnt] => 59 [patent_no_of_words] => 12247 [patent_no_of_claims] => 50 [patent_no_of_ind_claims] => 8 [patent_words_short_claim] => 65 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/07/090/07090166.pdf [firstpage_image] =>[orig_patent_app_number] => 10758948 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 704654 [patent_doc_number] => 07059564 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2006-06-13 [patent_title] => 'Methods and apparatuses for capturing and recovering unmanned aircraft, including a cleat for capturing aircraft on a line' [patent_app_type] => utility [patent_app_number] => 10/758940 [patent_app_country] => US [patent_app_date] => 2004-01-16 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 26 [patent_figures_cnt] => 59 [patent_no_of_words] => 12246 [patent_no_of_claims] => 32 [patent_no_of_ind_claims] => 5 [patent_words_short_claim] => 137 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/07/059/07059564.pdf [firstpage_image] =>[orig_patent_app_number] => 10758940 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 696516 [patent_doc_number] => 07066430 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2006-06-27 [patent_title] => 'Methods and apparatuses for capturing and recovering unmanned aircraft, including extendable capture devices' [patent_app_type] => utility [patent_app_number] => 10/758956 [patent_app_country] => US [patent_app_date] => 2004-01-16 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 26 [patent_figures_cnt] => 59 [patent_no_of_words] => 12252 [patent_no_of_claims] => 33 [patent_no_of_ind_claims] => 6 [patent_words_short_claim] => 31 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/07/066/07066430.pdf [firstpage_image] =>[orig_patent_app_number] => 10758956 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 647502 [patent_doc_number] => 07114680 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2006-10-03 [patent_title] => 'Methods and apparatuses for launching and capturing unmanned aircraft, including a combined launch and recovery system' [patent_app_type] => utility [patent_app_number] => 10/759742 [patent_app_country] => US [patent_app_date] => 2004-01-16 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 26 [patent_figures_cnt] => 59 [patent_no_of_words] => 12142 [patent_no_of_claims] => 32 [patent_no_of_ind_claims] => 5 [patent_words_short_claim] => 48 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/07/114/07114680.pdf [firstpage_image] =>[orig_patent_app_number] => 10759742 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 618745 [patent_doc_number] => 07140575 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2006-11-28 [patent_title] => 'Methods and apparatuses for launching unmanned aircraft, including methods and apparatuses for releasably gripping aircraft during launch' [patent_app_type] => utility [patent_app_number] => 10/758955 [patent_app_country] => US [patent_app_date] => 2004-01-16 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 26 [patent_figures_cnt] => 59 [patent_no_of_words] => 12285 [patent_no_of_claims] => 28 [patent_no_of_ind_claims] => 5 [patent_words_short_claim] => 89 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/07/140/07140575.pdf [firstpage_image] =>[orig_patent_app_number] => 10758955 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 6963639 [patent_doc_number] => 20050230536 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2005-10-20 [patent_title] => 'METHODS AND APPARATUSES FOR CAPTURING AND STORING UNMANNED AIRCRAFT, INCLUDING METHODS AND APPARATUSES FOR SECURING THE AIRCRAFT AFTER CAPTURE' [patent_app_type] => utility [patent_app_number] => 10/758943 [patent_app_country] => US [patent_app_date] => 2004-01-16 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 27 [patent_figures_cnt] => 27 [patent_no_of_words] => 12287 [patent_no_of_claims] => 32 [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/A1/0230/20050230536.pdf [firstpage_image] =>[orig_patent_app_number] => 10758943 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 7132516 [patent_doc_number] => 20050178883 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2005-08-18 [patent_title] => 'Helicopter tail rotor pylon' [patent_app_type] => utility [patent_app_number] => 10/755051 [patent_app_country] => US [patent_app_date] => 2004-01-08 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 4 [patent_figures_cnt] => 4 [patent_no_of_words] => 1346 [patent_no_of_claims] => 19 [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/A1/0178/20050178883.pdf [firstpage_image] =>[orig_patent_app_number] => 10755051 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 1004142 [patent_doc_number] => 06905095 [patent_country] => US [patent_kind] => B1 [patent_issue_date] => 2005-06-14 [patent_title] => 'Multiple platform aircraft cargo loader' [patent_app_type] => utility [patent_app_number] => 10/753781 [patent_app_country] => US [patent_app_date] => 2004-01-08 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 4 [patent_figures_cnt] => 7 [patent_no_of_words] => 2755 [patent_no_of_claims] => 18 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 177 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/06/905/06905095.pdf [firstpage_image] =>[orig_patent_app_number] => 10753781 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 692551 [patent_doc_number] => 07070144 [patent_country] => US [patent_kind] => B1 [patent_issue_date] => 2006-07-04 [patent_title] => 'Aircraft and missile afterbody flow control device and method of controlling flow' [patent_app_type] => utility [patent_app_number] => 10/750422 [patent_app_country] => US [patent_app_date] => 2003-12-30 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 5 [patent_figures_cnt] => 8 [patent_no_of_words] => 5759 [patent_no_of_claims] => 20 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 94 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/07/070/07070144.pdf [firstpage_image] =>[orig_patent_app_number] => 10750422 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 933246 [patent_doc_number] => 06976658 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2005-12-20 [patent_title] => 'Cockpit door of aircraft' [patent_app_type] => utility [patent_app_number] => 10/747309 [patent_app_country] => US [patent_app_date] => 2003-12-30 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 12 [patent_figures_cnt] => 17 [patent_no_of_words] => 2547 [patent_no_of_claims] => 2 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 107 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/06/976/06976658.pdf [firstpage_image] =>[orig_patent_app_number] => 10747309 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 980872 [patent_doc_number] => 06926229 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2005-08-09 [patent_title] => 'Aircraft with thrust vectoring for switchably providing upper surface blowing' [patent_app_type] => utility [patent_app_number] => 10/730357 [patent_app_country] => US [patent_app_date] => 2003-12-08 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 5 [patent_figures_cnt] => 11 [patent_no_of_words] => 3164 [patent_no_of_claims] => 26 [patent_no_of_ind_claims] => 4 [patent_words_short_claim] => 121 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/06/926/06926229.pdf [firstpage_image] =>[orig_patent_app_number] => 10730357 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 7101201 [patent_doc_number] => 20050103927 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2005-05-19 [patent_title] => 'Ice detection assembly installed on an aircraft' [patent_app_type] => utility [patent_app_number] => 10/727819 [patent_app_country] => US [patent_app_date] => 2003-12-03 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 10 [patent_figures_cnt] => 10 [patent_no_of_words] => 6090 [patent_no_of_claims] => 17 [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/A1/0103/20050103927.pdf [firstpage_image] =>[orig_patent_app_number] => 10727819 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 677841 [patent_doc_number] => 07083141 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2006-08-01 [patent_title] => 'Self-propelled projectile' [patent_app_type] => utility [patent_app_number] => 10/725100 [patent_app_country] => US [patent_app_date] => 2003-12-02 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 6 [patent_figures_cnt] => 13 [patent_no_of_words] => 1138 [patent_no_of_claims] => 2 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 151 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/07/083/07083141.pdf [firstpage_image] =>[orig_patent_app_number] => 10725100 [rel_patent_id] =>[rel_patent_doc_number] =>)