![](/images/general/no_picture/200_user.png)
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 number | Title of the application | Filing Date | Status |
---|---|---|---|
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
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[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
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[patent_no_of_words] => 6135
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[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
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[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
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[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
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[patent_no_of_words] => 2084
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[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
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[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
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[patent_no_of_words] => 6238
[patent_no_of_claims] => 14
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[patent_maintenance] => 1
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[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
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[patent_no_of_words] => 3115
[patent_no_of_claims] => 8
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[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
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[patent_no_of_words] => 5548
[patent_no_of_claims] => 14
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[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
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[patent_no_of_words] => 2826
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[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
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[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
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[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
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[patent_issue_date] => 2012-07-17
[patent_title] => 'Hinge rib'
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[patent_app_number] => 12/370623
[patent_app_country] => US
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[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
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[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
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[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
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[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
(
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[patent_title] => 'Control of projectiles or the like'
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Array
(
[id] => 6582313
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[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
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[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 |