Donovan C Bui-huynh

Array ( [id] => 9349280 [patent_doc_number] => 08668166 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2014-03-11 [patent_title] => 'Shape memory riblets' [patent_app_type] => utility [patent_app_number] => 12/361882 [patent_app_country] => US [patent_app_date] => 2009-01-29 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 13 [patent_figures_cnt] => 21 [patent_no_of_words] => 7498 [patent_no_of_claims] => 4 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 81 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 12361882 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 6430636 [patent_doc_number] => 20100187365 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2010-07-29 [patent_title] => 'CRYOGENIC PROPELLANT DEPOT AND DEPLOYABLE SUNSHIELD' [patent_app_type] => utility [patent_app_number] => 12/359033 [patent_app_country] => US [patent_app_date] => 2009-01-23 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 17 [patent_figures_cnt] => 17 [patent_no_of_words] => 5841 [patent_no_of_claims] => 22 [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/A1/0187/20100187365.pdf [firstpage_image] =>[orig_patent_app_number] => 12359033 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 6430629 [patent_doc_number] => 20100187364 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2010-07-29 [patent_title] => 'CRYOGENIC PROPELLANT DEPOT AND INTEGRAL SUNSHIELD' [patent_app_type] => utility [patent_app_number] => 12/359015 [patent_app_country] => US [patent_app_date] => 2009-01-23 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 17 [patent_figures_cnt] => 17 [patent_no_of_words] => 5841 [patent_no_of_claims] => 14 [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/A1/0187/20100187364.pdf [firstpage_image] =>[orig_patent_app_number] => 12359015 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 8894975 [patent_doc_number] => 08474486 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2013-07-02 [patent_title] => 'Actuator system' [patent_app_type] => utility [patent_app_number] => 12/350479 [patent_app_country] => US [patent_app_date] => 2009-01-08 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 11 [patent_figures_cnt] => 18 [patent_no_of_words] => 3549 [patent_no_of_claims] => 20 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 145 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 12350479 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 5352864 [patent_doc_number] => 20090184208 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2009-07-23 [patent_title] => 'AERODYNAMIC SEALING MEMBER FOR AIRCRAFT' [patent_app_type] => utility [patent_app_number] => 12/349054 [patent_app_country] => US [patent_app_date] => 2009-01-06 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 5 [patent_figures_cnt] => 5 [patent_no_of_words] => 2305 [patent_no_of_claims] => 18 [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/A1/0184/20090184208.pdf [firstpage_image] =>[orig_patent_app_number] => 12349054 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 7659149 [patent_doc_number] => 20110308418 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2011-12-22 [patent_title] => 'Projectile Having Deployable Fin' [patent_app_type] => utility [patent_app_number] => 12/344245 [patent_app_country] => US [patent_app_date] => 2008-12-25 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 7 [patent_figures_cnt] => 7 [patent_no_of_words] => 4377 [patent_no_of_claims] => 18 [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/A1/0308/20110308418.pdf [firstpage_image] =>[orig_patent_app_number] => 12344245 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 6421043 [patent_doc_number] => 20100102174 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2010-04-29 [patent_title] => 'Wingless Hovering Of Micro Air Vehicle' [patent_app_type] => utility [patent_app_number] => 12/342583 [patent_app_country] => US [patent_app_date] => 2008-12-23 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 22 [patent_figures_cnt] => 22 [patent_no_of_words] => 7174 [patent_no_of_claims] => 42 [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/A1/0102/20100102174.pdf [firstpage_image] =>[orig_patent_app_number] => 12342583 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 5499065 [patent_doc_number] => 20090159753 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2009-06-25 [patent_title] => 'MOMENTUM MANAGEMENT SYSTEM FOR REACTION WHEEL BY USING NULL SPACE VECTOR AND METHOD' [patent_app_type] => utility [patent_app_number] => 12/341393 [patent_app_country] => US [patent_app_date] => 2008-12-22 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 3 [patent_figures_cnt] => 3 [patent_no_of_words] => 2596 [patent_no_of_claims] => 8 [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/A1/0159/20090159753.pdf [firstpage_image] =>[orig_patent_app_number] => 12341393 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 8576239 [patent_doc_number] => 08342444 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2013-01-01 [patent_title] => 'Fail safe extended torque box strut-to-wing mount' [patent_app_type] => utility [patent_app_number] => 12/336213 [patent_app_country] => US [patent_app_date] => 2008-12-16 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 11 [patent_figures_cnt] => 13 [patent_no_of_words] => 5504 [patent_no_of_claims] => 21 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 207 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 12336213 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 6090462 [patent_doc_number] => 20110001002 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2011-01-06 [patent_title] => 'SUSPENSION FOR MOUNTING A TURBOJET ENGINE ON AN AIRCRAFT' [patent_app_type] => utility [patent_app_number] => 12/329136 [patent_app_country] => US [patent_app_date] => 2008-12-05 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 7 [patent_figures_cnt] => 7 [patent_no_of_words] => 3794 [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/A1/0001/20110001002.pdf [firstpage_image] =>[orig_patent_app_number] => 12329136 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 9284667 [patent_doc_number] => 08640986 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2014-02-04 [patent_title] => 'Turbojet nacelle and method for controlling separation in a turbojet nacelle' [patent_app_type] => utility [patent_app_number] => 12/326604 [patent_app_country] => US [patent_app_date] => 2008-12-02 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 5 [patent_figures_cnt] => 15 [patent_no_of_words] => 3604 [patent_no_of_claims] => 13 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 87 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 12326604 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 6546356 [patent_doc_number] => 20100127116 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2010-05-27 [patent_title] => 'NACELLE AND METHOD OF ASSEMBLING THE SAME' [patent_app_type] => utility [patent_app_number] => 12/324429 [patent_app_country] => US [patent_app_date] => 2008-11-26 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 9 [patent_figures_cnt] => 9 [patent_no_of_words] => 5358 [patent_no_of_claims] => 20 [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/A1/0127/20100127116.pdf [firstpage_image] =>[orig_patent_app_number] => 12324429 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 6445163 [patent_doc_number] => 20100038471 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2010-02-18 [patent_title] => 'Suspension system for aircraft auxiliary power unit with elastomeric member' [patent_app_type] => utility [patent_app_number] => 12/288434 [patent_app_country] => US [patent_app_date] => 2008-10-20 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 15 [patent_figures_cnt] => 15 [patent_no_of_words] => 40614 [patent_no_of_claims] => 44 [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/A1/0038/20100038471.pdf [firstpage_image] =>[orig_patent_app_number] => 12288434 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 7549317 [patent_doc_number] => 08061646 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2011-11-22 [patent_title] => 'Wing tip docking system for aircraft' [patent_app_type] => utility [patent_app_number] => 12/210711 [patent_app_country] => US [patent_app_date] => 2008-09-15 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 12 [patent_figures_cnt] => 12 [patent_no_of_words] => 6630 [patent_no_of_claims] => 12 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 218 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/08/061/08061646.pdf [firstpage_image] =>[orig_patent_app_number] => 12210711 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 5461375 [patent_doc_number] => 20090321575 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2009-12-31 [patent_title] => 'STRUCTURE OF AN AIRCRAFT AEROFOIL' [patent_app_type] => utility [patent_app_number] => 12/201310 [patent_app_country] => US [patent_app_date] => 2008-08-29 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 5 [patent_figures_cnt] => 5 [patent_no_of_words] => 2079 [patent_no_of_claims] => 6 [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/A1/0321/20090321575.pdf [firstpage_image] =>[orig_patent_app_number] => 12201310 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 6319836 [patent_doc_number] => 20100243795 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2010-09-30 [patent_title] => 'OBLIQUE BLENDED WING BODY AIRCRAFT' [patent_app_type] => utility [patent_app_number] => 12/675165 [patent_app_country] => US [patent_app_date] => 2008-08-29 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 6 [patent_figures_cnt] => 6 [patent_no_of_words] => 8297 [patent_no_of_claims] => 26 [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/A1/0243/20100243795.pdf [firstpage_image] =>[orig_patent_app_number] => 12675165 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 6215401 [patent_doc_number] => 20100051749 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2010-03-04 [patent_title] => 'AIRCRAFT SPILLOVER FUEL TANK' [patent_app_type] => utility [patent_app_number] => 12/199069 [patent_app_country] => US [patent_app_date] => 2008-08-27 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 7 [patent_figures_cnt] => 7 [patent_no_of_words] => 4908 [patent_no_of_claims] => 20 [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/A1/0051/20100051749.pdf [firstpage_image] =>[orig_patent_app_number] => 12199069 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 6541675 [patent_doc_number] => 20100044515 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2010-02-25 [patent_title] => 'CONTINUAL TRANSFERENCE OF FUEL BETWEEN FUEL TANKS AT A RATE COMMENSURATE WITH FUEL BURN DURING CRUISE FLIGHT OPERATION TO MAINTAIN THE AIRCRAFT CENTER OF GRAVITY WITHIN A PRE-SELECTED AFT CENTER OF GRAVITY ENVELOPE' [patent_app_type] => utility [patent_app_number] => 12/197737 [patent_app_country] => US [patent_app_date] => 2008-08-25 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 8 [patent_figures_cnt] => 8 [patent_no_of_words] => 4172 [patent_no_of_claims] => 20 [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/A1/0044/20100044515.pdf [firstpage_image] =>[orig_patent_app_number] => 12197737 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 6445334 [patent_doc_number] => 20100038492 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2010-02-18 [patent_title] => 'RETRACTABLE NACELLE CHINE' [patent_app_type] => utility [patent_app_number] => 12/192407 [patent_app_country] => US [patent_app_date] => 2008-08-15 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 8 [patent_figures_cnt] => 8 [patent_no_of_words] => 5878 [patent_no_of_claims] => 20 [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/A1/0038/20100038492.pdf [firstpage_image] =>[orig_patent_app_number] => 12192407 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 6445240 [patent_doc_number] => 20100038480 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2010-02-18 [patent_title] => 'JET/EFFLUX OUTWASH BARRIER SYSTEM FOR STOVL, TILTROTOR, AND HELICOPTER AIRCRAFT' [patent_app_type] => utility [patent_app_number] => 12/191914 [patent_app_country] => US [patent_app_date] => 2008-08-14 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 6 [patent_figures_cnt] => 6 [patent_no_of_words] => 5153 [patent_no_of_claims] => 45 [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/A1/0038/20100038480.pdf [firstpage_image] =>[orig_patent_app_number] => 12191914 [rel_patent_id] =>[rel_patent_doc_number] =>)