Tien Quang Dinh

Array ( [id] => 5339947 [patent_doc_number] => 20090178597 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2009-07-16 [patent_title] => 'Physical threat containment, neutralization and protection means applicable to terrorism, combat and disaster mitigation' [patent_app_type] => utility [patent_app_number] => 12/381595 [patent_app_country] => US [patent_app_date] => 2009-03-12 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 8 [patent_figures_cnt] => 8 [patent_no_of_words] => 16298 [patent_no_of_claims] => 12 [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/A1/0178/20090178597.pdf [firstpage_image] =>[orig_patent_app_number] => 12381595 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 6000352 [patent_doc_number] => 20110116905 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2011-05-19 [patent_title] => 'METHOD AND APPARATUS FOR TRANSPORTING ELONGATED, CUMBERSOME LOADS' [patent_app_type] => utility [patent_app_number] => 12/922086 [patent_app_country] => US [patent_app_date] => 2009-03-09 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 9 [patent_figures_cnt] => 9 [patent_no_of_words] => 3312 [patent_no_of_claims] => 10 [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/A1/0116/20110116905.pdf [firstpage_image] =>[orig_patent_app_number] => 12922086 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 89758 [patent_doc_number] => 07731125 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2010-06-08 [patent_title] => 'Compact stowage of transport aircraft' [patent_app_type] => utility [patent_app_number] => 12/399206 [patent_app_country] => US [patent_app_date] => 2009-03-06 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 6 [patent_figures_cnt] => 10 [patent_no_of_words] => 4848 [patent_no_of_claims] => 19 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 91 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/07/731/07731125.pdf [firstpage_image] =>[orig_patent_app_number] => 12399206 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 6568192 [patent_doc_number] => 20100320322 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2010-12-23 [patent_title] => 'TRANSVERSE BUTT CONNECTION BETWEEN TWO FUSELAGE SECTIONS' [patent_app_type] => utility [patent_app_number] => 12/735799 [patent_app_country] => US [patent_app_date] => 2009-02-16 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 3 [patent_figures_cnt] => 3 [patent_no_of_words] => 4147 [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] => publications/A1/0320/20100320322.pdf [firstpage_image] =>[orig_patent_app_number] => 12735799 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 8362240 [patent_doc_number] => 08251305 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2012-08-28 [patent_title] => 'Rotorcraft with variable incident wing' [patent_app_type] => utility [patent_app_number] => 12/866904 [patent_app_country] => US [patent_app_date] => 2009-02-11 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 5 [patent_figures_cnt] => 13 [patent_no_of_words] => 2789 [patent_no_of_claims] => 8 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 148 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 12866904 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 9350614 [patent_doc_number] => 08669506 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2014-03-11 [patent_title] => 'Apparatus and method for controlling a vehicle, and vehicle controlled thereby' [patent_app_type] => utility [patent_app_number] => 12/921603 [patent_app_country] => US [patent_app_date] => 2008-12-25 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 4 [patent_figures_cnt] => 9 [patent_no_of_words] => 6187 [patent_no_of_claims] => 25 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 128 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 12921603 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 8146362 [patent_doc_number] => 08163368 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2012-04-24 [patent_title] => 'Composite leg for landing gear assembly' [patent_app_type] => utility [patent_app_number] => 12/341885 [patent_app_country] => US [patent_app_date] => 2008-12-22 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 4 [patent_figures_cnt] => 8 [patent_no_of_words] => 2761 [patent_no_of_claims] => 11 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 82 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/08/163/08163368.pdf [firstpage_image] =>[orig_patent_app_number] => 12341885 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 9007814 [patent_doc_number] => 08523103 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2013-09-03 [patent_title] => 'Retractable lifting blades for aircraft' [patent_app_type] => utility [patent_app_number] => 12/337189 [patent_app_country] => US [patent_app_date] => 2008-12-17 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 21 [patent_figures_cnt] => 32 [patent_no_of_words] => 7521 [patent_no_of_claims] => 13 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 78 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 12337189 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 5499064 [patent_doc_number] => 20090159752 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2009-06-25 [patent_title] => 'Spreader bar lateral kite control' [patent_app_type] => utility [patent_app_number] => 12/314371 [patent_app_country] => US [patent_app_date] => 2008-12-09 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 8 [patent_figures_cnt] => 8 [patent_no_of_words] => 2409 [patent_no_of_claims] => 13 [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/A1/0159/20090159752.pdf [firstpage_image] =>[orig_patent_app_number] => 12314371 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 5572740 [patent_doc_number] => 20090140100 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2009-06-04 [patent_title] => 'REUSABLE ORBITAL VEHICLE WITH INTERCHANGEABLE CARGO MODULES' [patent_app_type] => utility [patent_app_number] => 12/324746 [patent_app_country] => US [patent_app_date] => 2008-11-26 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 19 [patent_figures_cnt] => 19 [patent_no_of_words] => 7192 [patent_no_of_claims] => 13 [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/A1/0140/20090140100.pdf [firstpage_image] =>[orig_patent_app_number] => 12324746 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 6129907 [patent_doc_number] => 20110006153 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2011-01-13 [patent_title] => 'Internet linked environmental data collection system and method' [patent_app_type] => utility [patent_app_number] => 12/292018 [patent_app_country] => US [patent_app_date] => 2008-11-10 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 24 [patent_figures_cnt] => 24 [patent_no_of_words] => 11595 [patent_no_of_claims] => 50 [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/A1/0006/20110006153.pdf [firstpage_image] =>[orig_patent_app_number] => 12292018 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 4617819 [patent_doc_number] => 07997533 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2011-08-16 [patent_title] => 'Fire barrier for an aircraft fuselage' [patent_app_type] => utility [patent_app_number] => 12/260902 [patent_app_country] => US [patent_app_date] => 2008-10-29 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 4 [patent_figures_cnt] => 8 [patent_no_of_words] => 3139 [patent_no_of_claims] => 10 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 146 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/07/997/07997533.pdf [firstpage_image] =>[orig_patent_app_number] => 12260902 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 8268979 [patent_doc_number] => 08210474 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2012-07-03 [patent_title] => 'Multi-path inlet for aircraft engine' [patent_app_type] => utility [patent_app_number] => 12/259379 [patent_app_country] => US [patent_app_date] => 2008-10-28 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 7 [patent_figures_cnt] => 10 [patent_no_of_words] => 3611 [patent_no_of_claims] => 13 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 120 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 12259379 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 139605 [patent_doc_number] => 07690599 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2010-04-06 [patent_title] => 'Method of illumination for in-flight refueling' [patent_app_type] => utility [patent_app_number] => 12/237588 [patent_app_country] => US [patent_app_date] => 2008-09-25 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 3 [patent_figures_cnt] => 3 [patent_no_of_words] => 6326 [patent_no_of_claims] => 20 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 137 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/07/690/07690599.pdf [firstpage_image] =>[orig_patent_app_number] => 12237588 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 6113819 [patent_doc_number] => 20110073708 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2011-03-31 [patent_title] => 'Composite Barrel Sections for Aircraft Fuselages and Other Structures, and Methods and Systems for Manufacturing Such Barrel Sections' [patent_app_type] => utility [patent_app_number] => 12/236355 [patent_app_country] => US [patent_app_date] => 2008-09-23 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 12 [patent_figures_cnt] => 12 [patent_no_of_words] => 7641 [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/A1/0073/20110073708.pdf [firstpage_image] =>[orig_patent_app_number] => 12236355 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 5293575 [patent_doc_number] => 20090008501 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2009-01-08 [patent_title] => 'LANDING GEAR' [patent_app_type] => utility [patent_app_number] => 12/233229 [patent_app_country] => US [patent_app_date] => 2008-09-18 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 16 [patent_figures_cnt] => 16 [patent_no_of_words] => 14162 [patent_no_of_claims] => 28 [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/A1/0008/20090008501.pdf [firstpage_image] =>[orig_patent_app_number] => 12233229 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 6492554 [patent_doc_number] => 20100200698 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2010-08-12 [patent_title] => 'FUSELAGE AND A METHOD FOR REDESIGNING IT' [patent_app_type] => utility [patent_app_number] => 12/676360 [patent_app_country] => US [patent_app_date] => 2008-09-12 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 3 [patent_figures_cnt] => 3 [patent_no_of_words] => 1581 [patent_no_of_claims] => 7 [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/A1/0200/20100200698.pdf [firstpage_image] =>[orig_patent_app_number] => 12676360 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 5407179 [patent_doc_number] => 20090121077 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2009-05-14 [patent_title] => 'Method and apparatus for operating an aircraft landing system' [patent_app_type] => utility [patent_app_number] => 12/230255 [patent_app_country] => US [patent_app_date] => 2008-08-26 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 5 [patent_figures_cnt] => 5 [patent_no_of_words] => 3746 [patent_no_of_claims] => 36 [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/A1/0121/20090121077.pdf [firstpage_image] =>[orig_patent_app_number] => 12230255 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 5319496 [patent_doc_number] => 20090057486 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2009-03-05 [patent_title] => 'Modular helicopter deck for offshore oil drilling/production platforms' [patent_app_type] => utility [patent_app_number] => 12/229580 [patent_app_country] => US [patent_app_date] => 2008-08-25 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 7 [patent_figures_cnt] => 7 [patent_no_of_words] => 2213 [patent_no_of_claims] => 15 [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/A1/0057/20090057486.pdf [firstpage_image] =>[orig_patent_app_number] => 12229580 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 5334282 [patent_doc_number] => 20090050746 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2009-02-26 [patent_title] => 'METHOD AND DEVICE FOR AUTOMATICALLY PROTECTING AN AIRCRAFT AGAINST A HARD LANDING' [patent_app_type] => utility [patent_app_number] => 12/193467 [patent_app_country] => US [patent_app_date] => 2008-08-18 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 3 [patent_figures_cnt] => 3 [patent_no_of_words] => 3107 [patent_no_of_claims] => 8 [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/A1/0050/20090050746.pdf [firstpage_image] =>[orig_patent_app_number] => 12193467 [rel_patent_id] =>[rel_patent_doc_number] =>)