Search

Truc T Nguyen

Examiner (ID: 4647, Phone: (571)272-2011 , Office: P/2833 )

Most Active Art Unit
2833
Art Unit(s)
2834, 2832, 2833
Total Applications
2486
Issued Applications
2152
Pending Applications
102
Abandoned Applications
232

Applications

Application numberTitle of the applicationFiling DateStatus
Array ( [id] => 8338696 [patent_doc_number] => 08240616 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2012-08-14 [patent_title] => 'Method and system for global flow field management using distributed, surface-embedded, nano-scale boundary layer actuation' [patent_app_type] => utility [patent_app_number] => 12/428135 [patent_app_country] => US [patent_app_date] => 2009-04-22 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 11 [patent_figures_cnt] => 22 [patent_no_of_words] => 6208 [patent_no_of_claims] => 20 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 196 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 12428135 [rel_patent_id] =>[rel_patent_doc_number] =>)
12/428135
Method and system for global flow field management using distributed, surface-embedded, nano-scale boundary layer actuation Apr 21, 2009 Issued
Array ( [id] => 7703278 [patent_doc_number] => 08089034 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2012-01-03 [patent_title] => 'Mechanism for folding, sweeping, and locking vehicle wings about a single pivot' [patent_app_type] => utility [patent_app_number] => 12/425844 [patent_app_country] => US [patent_app_date] => 2009-04-17 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 9 [patent_figures_cnt] => 9 [patent_no_of_words] => 4601 [patent_no_of_claims] => 11 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 156 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/08/089/08089034.pdf [firstpage_image] =>[orig_patent_app_number] => 12425844 [rel_patent_id] =>[rel_patent_doc_number] =>)
12/425844
Mechanism for folding, sweeping, and locking vehicle wings about a single pivot Apr 16, 2009 Issued
Array ( [id] => 6541454 [patent_doc_number] => 20100044494 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2010-02-25 [patent_title] => 'Space launcher' [patent_app_type] => utility [patent_app_number] => 12/386455 [patent_app_country] => US [patent_app_date] => 2009-04-17 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 2 [patent_figures_cnt] => 2 [patent_no_of_words] => 6135 [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/A1/0044/20100044494.pdf [firstpage_image] =>[orig_patent_app_number] => 12386455 [rel_patent_id] =>[rel_patent_doc_number] =>)
12/386455
Space launcher Apr 16, 2009 Abandoned
12/386232 Adjustable wing line apparatus for inflatable airfoils Apr 14, 2009 Abandoned
Array ( [id] => 8100905 [patent_doc_number] => 08152098 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2012-04-10 [patent_title] => 'Torque limiter with brake' [patent_app_type] => utility [patent_app_number] => 12/414866 [patent_app_country] => US [patent_app_date] => 2009-03-31 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 3 [patent_figures_cnt] => 3 [patent_no_of_words] => 2159 [patent_no_of_claims] => 12 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 78 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/08/152/08152098.pdf [firstpage_image] =>[orig_patent_app_number] => 12414866 [rel_patent_id] =>[rel_patent_doc_number] =>)
12/414866
Torque limiter with brake Mar 30, 2009 Issued
Array ( [id] => 6319889 [patent_doc_number] => 20100243815 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2010-09-30 [patent_title] => 'Payload Quick Release for an Aerial System' [patent_app_type] => utility [patent_app_number] => 12/415463 [patent_app_country] => US [patent_app_date] => 2009-03-31 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 6 [patent_figures_cnt] => 6 [patent_no_of_words] => 2157 [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/A1/0243/20100243815.pdf [firstpage_image] =>[orig_patent_app_number] => 12415463 [rel_patent_id] =>[rel_patent_doc_number] =>)
12/415463
Payload quick release for an aerial system Mar 30, 2009 Issued
Array ( [id] => 5469526 [patent_doc_number] => 20090242692 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2009-10-01 [patent_title] => 'Clutch Arrangement' [patent_app_type] => utility [patent_app_number] => 12/414872 [patent_app_country] => US [patent_app_date] => 2009-03-31 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 3 [patent_figures_cnt] => 3 [patent_no_of_words] => 2084 [patent_no_of_claims] => 9 [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/A1/0242/20090242692.pdf [firstpage_image] =>[orig_patent_app_number] => 12414872 [rel_patent_id] =>[rel_patent_doc_number] =>)
12/414872
Clutch arrangement Mar 30, 2009 Issued
Array ( [id] => 5469532 [patent_doc_number] => 20090242698 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2009-10-01 [patent_title] => 'AERODYNAMIC BRAKING DEVICE FOR AIRCRAFT' [patent_app_type] => utility [patent_app_number] => 12/415088 [patent_app_country] => US [patent_app_date] => 2009-03-31 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 7 [patent_figures_cnt] => 7 [patent_no_of_words] => 2824 [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/A1/0242/20090242698.pdf [firstpage_image] =>[orig_patent_app_number] => 12415088 [rel_patent_id] =>[rel_patent_doc_number] =>)
12/415088
Aerodynamic braking device for aircraft Mar 30, 2009 Issued
Array ( [id] => 5455873 [patent_doc_number] => 20090256025 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2009-10-15 [patent_title] => 'STABILIZING AND DIRECTIONAL-CONTROL SURFACE OF AIRCRAFT' [patent_app_type] => utility [patent_app_number] => 12/415485 [patent_app_country] => US [patent_app_date] => 2009-03-31 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 9 [patent_figures_cnt] => 9 [patent_no_of_words] => 6238 [patent_no_of_claims] => 14 [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/A1/0256/20090256025.pdf [firstpage_image] =>[orig_patent_app_number] => 12415485 [rel_patent_id] =>[rel_patent_doc_number] =>)
12/415485
Stabilizing and directional-control surface of aircraft Mar 30, 2009 Issued
Array ( [id] => 5555361 [patent_doc_number] => 20090266938 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2009-10-29 [patent_title] => 'METHOD AND DEVICE FOR AN AIRCRAFT BUFFET REDUCTION' [patent_app_type] => utility [patent_app_number] => 12/413986 [patent_app_country] => US [patent_app_date] => 2009-03-30 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 3 [patent_figures_cnt] => 3 [patent_no_of_words] => 3115 [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/A1/0266/20090266938.pdf [firstpage_image] =>[orig_patent_app_number] => 12413986 [rel_patent_id] =>[rel_patent_doc_number] =>)
12/413986
Method and device for an aircraft buffet reduction Mar 29, 2009 Issued
Array ( [id] => 7974687 [patent_doc_number] => 08070089 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2011-12-06 [patent_title] => 'Hybrid helicopter that is fast and has long range' [patent_app_type] => utility [patent_app_number] => 12/409948 [patent_app_country] => US [patent_app_date] => 2009-03-24 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 1 [patent_figures_cnt] => 3 [patent_no_of_words] => 5548 [patent_no_of_claims] => 14 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 173 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/08/070/08070089.pdf [firstpage_image] =>[orig_patent_app_number] => 12409948 [rel_patent_id] =>[rel_patent_doc_number] =>)
12/409948
Hybrid helicopter that is fast and has long range Mar 23, 2009 Issued
Array ( [id] => 5388888 [patent_doc_number] => 20090206200 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2009-08-20 [patent_title] => 'ASSEMBLY AND METHOD FOR STOWING AWAY AND REMOVING A SURVIVAL KIT IN A PASSENGER CABIN OF AN AIRCRAFT' [patent_app_type] => utility [patent_app_number] => 12/388754 [patent_app_country] => US [patent_app_date] => 2009-02-19 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 7 [patent_figures_cnt] => 7 [patent_no_of_words] => 2826 [patent_no_of_claims] => 15 [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/A1/0206/20090206200.pdf [firstpage_image] =>[orig_patent_app_number] => 12388754 [rel_patent_id] =>[rel_patent_doc_number] =>)
12/388754
Assembly and method for stowing away and removing a survival kit in a passenger cabin of an aircraft Feb 18, 2009 Issued
Array ( [id] => 6568283 [patent_doc_number] => 20100320331 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2010-12-23 [patent_title] => 'Unitary, Self-Stiffened and Pivoting Composite Panel, in Particular for a Mobile Part of an Aircraft' [patent_app_type] => utility [patent_app_number] => 12/866751 [patent_app_country] => US [patent_app_date] => 2009-02-19 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 4 [patent_figures_cnt] => 4 [patent_no_of_words] => 5609 [patent_no_of_claims] => 15 [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/A1/0320/20100320331.pdf [firstpage_image] =>[orig_patent_app_number] => 12866751 [rel_patent_id] =>[rel_patent_doc_number] =>)
12/866751
Unitary, Self-Stiffened and Pivoting Composite Panel, in Particular for a Mobile Part of an Aircraft Feb 18, 2009 Abandoned
Array ( [id] => 8651795 [patent_doc_number] => 08371537 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2013-02-12 [patent_title] => 'Aircraft structure with hinge rib assembly' [patent_app_type] => utility [patent_app_number] => 12/370657 [patent_app_country] => US [patent_app_date] => 2009-02-13 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 14 [patent_figures_cnt] => 20 [patent_no_of_words] => 4360 [patent_no_of_claims] => 14 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 101 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 12370657 [rel_patent_id] =>[rel_patent_doc_number] =>)
12/370657
Aircraft structure with hinge rib assembly Feb 12, 2009 Issued
Array ( [id] => 8292972 [patent_doc_number] => 08220755 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2012-07-17 [patent_title] => 'Hinge rib' [patent_app_type] => utility [patent_app_number] => 12/370623 [patent_app_country] => US [patent_app_date] => 2009-02-13 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 3 [patent_figures_cnt] => 4 [patent_no_of_words] => 1678 [patent_no_of_claims] => 15 [patent_no_of_ind_claims] => 4 [patent_words_short_claim] => 100 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 12370623 [rel_patent_id] =>[rel_patent_doc_number] =>)
12/370623
Hinge rib Feb 12, 2009 Issued
Array ( [id] => 8712771 [patent_doc_number] => 08398910 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2013-03-19 [patent_title] => 'Method for manufacturing a fibre-composite component, fibre-composite component and fibre-composite fuselage component of an aircraft' [patent_app_type] => utility [patent_app_number] => 12/866375 [patent_app_country] => US [patent_app_date] => 2009-02-09 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 3 [patent_figures_cnt] => 4 [patent_no_of_words] => 11666 [patent_no_of_claims] => 25 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 188 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 12866375 [rel_patent_id] =>[rel_patent_doc_number] =>)
12/866375
Method for manufacturing a fibre-composite component, fibre-composite component and fibre-composite fuselage component of an aircraft Feb 8, 2009 Issued
Array ( [id] => 6129932 [patent_doc_number] => 20110006162 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2011-01-13 [patent_title] => 'ACTUATOR DEVICE FOR VARYING THE ATTITUDE OF A SPACECRAFT' [patent_app_type] => utility [patent_app_number] => 12/866875 [patent_app_country] => US [patent_app_date] => 2009-02-03 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 7 [patent_figures_cnt] => 7 [patent_no_of_words] => 8798 [patent_no_of_claims] => 17 [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/A1/0006/20110006162.pdf [firstpage_image] =>[orig_patent_app_number] => 12866875 [rel_patent_id] =>[rel_patent_doc_number] =>)
12/866875
Actuator device for varying the attitude of a spacecraft Feb 2, 2009 Issued
Array ( [id] => 6326636 [patent_doc_number] => 20100327110 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2010-12-30 [patent_title] => 'GUIDING SYSTEM FOR AIRCRAFT NACELLE MAINTENANCE' [patent_app_type] => utility [patent_app_number] => 12/864925 [patent_app_country] => US [patent_app_date] => 2009-01-21 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 9 [patent_figures_cnt] => 9 [patent_no_of_words] => 4600 [patent_no_of_claims] => 15 [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/A1/0327/20100327110.pdf [firstpage_image] =>[orig_patent_app_number] => 12864925 [rel_patent_id] =>[rel_patent_doc_number] =>)
12/864925
Guiding system for aircraft nacelle maintenance Jan 20, 2009 Issued
Array ( [id] => 9355745 [patent_doc_number] => 08674278 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2014-03-18 [patent_title] => 'Control of projectiles or the like' [patent_app_type] => utility [patent_app_number] => 12/867868 [patent_app_country] => US [patent_app_date] => 2009-01-13 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 4 [patent_figures_cnt] => 7 [patent_no_of_words] => 2522 [patent_no_of_claims] => 12 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 127 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 12867868 [rel_patent_id] =>[rel_patent_doc_number] =>)
12/867868
Control of projectiles or the like Jan 12, 2009 Issued
Array ( [id] => 6582313 [patent_doc_number] => 20100308162 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2010-12-09 [patent_title] => 'LANDING FLAP KINEMATICS DRIVEN BY WAY OF A PINION DRIVE' [patent_app_type] => utility [patent_app_number] => 12/743895 [patent_app_country] => US [patent_app_date] => 2008-11-21 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 6 [patent_figures_cnt] => 6 [patent_no_of_words] => 3185 [patent_no_of_claims] => 20 [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/A1/0308/20100308162.pdf [firstpage_image] =>[orig_patent_app_number] => 12743895 [rel_patent_id] =>[rel_patent_doc_number] =>)
12/743895
Landing flap kinematics driven by way of a pinion drive Nov 20, 2008 Issued
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