Search

Tien Quang Dinh

Supervisory Patent Examiner (ID: 10795, Phone: (571)272-6899 , Office: P/3647 )

Most Active Art Unit
3644
Art Unit(s)
3641, 3644, 3647, 3104, 3613
Total Applications
1457
Issued Applications
1028
Pending Applications
118
Abandoned Applications
313

Applications

Application numberTitle of the applicationFiling DateStatus
Array ( [id] => 9515016 [patent_doc_number] => 20140151508 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2014-06-05 [patent_title] => 'METHOD OF LANDING OF A SURVEILLANCE UNMANNED AERIAL VEHICLE AND A SURVEILLANCE UNMANNED AERIAL VEHICLE' [patent_app_type] => utility [patent_app_number] => 13/689853 [patent_app_country] => US [patent_app_date] => 2012-11-30 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 3 [patent_figures_cnt] => 3 [patent_no_of_words] => 1705 [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] =>[firstpage_image] =>[orig_patent_app_number] => 13689853 [rel_patent_id] =>[rel_patent_doc_number] =>)
13/689853
METHOD OF LANDING OF A SURVEILLANCE UNMANNED AERIAL VEHICLE AND A SURVEILLANCE UNMANNED AERIAL VEHICLE Nov 29, 2012 Abandoned
Array ( [id] => 8824398 [patent_doc_number] => 20130125443 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2013-05-23 [patent_title] => 'ANIMAL CONDITIONING DEVICE' [patent_app_type] => utility [patent_app_number] => 13/680633 [patent_app_country] => US [patent_app_date] => 2012-11-19 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 6 [patent_figures_cnt] => 6 [patent_no_of_words] => 3896 [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] =>[firstpage_image] =>[orig_patent_app_number] => 13680633 [rel_patent_id] =>[rel_patent_doc_number] =>)
13/680633
ANIMAL CONDITIONING DEVICE Nov 18, 2012 Abandoned
Array ( [id] => 8777080 [patent_doc_number] => 20130099055 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2013-04-25 [patent_title] => 'INTEGRATED LAVATORY PAN FOR COMMERCIAL AIRCRAFT' [patent_app_type] => utility [patent_app_number] => 13/659085 [patent_app_country] => US [patent_app_date] => 2012-10-24 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 2 [patent_figures_cnt] => 2 [patent_no_of_words] => 915 [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] =>[firstpage_image] =>[orig_patent_app_number] => 13659085 [rel_patent_id] =>[rel_patent_doc_number] =>)
13/659085
INTEGRATED LAVATORY PAN FOR COMMERCIAL AIRCRAFT Oct 23, 2012 Abandoned
Array ( [id] => 8668808 [patent_doc_number] => 20130043346 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2013-02-21 [patent_title] => 'AIRCRAFT FUSELAGE STRUCTURAL COMPONENTS AND METHODS OF MAKING SAME' [patent_app_type] => utility [patent_app_number] => 13/645398 [patent_app_country] => US [patent_app_date] => 2012-10-04 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 7 [patent_figures_cnt] => 7 [patent_no_of_words] => 2347 [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] =>[firstpage_image] =>[orig_patent_app_number] => 13645398 [rel_patent_id] =>[rel_patent_doc_number] =>)
13/645398
Aircraft fuselage structural components and methods of making same Oct 3, 2012 Issued
Array ( [id] => 9125594 [patent_doc_number] => 08573533 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2013-11-05 [patent_title] => 'Method and apparatus for operating an aircraft landing system' [patent_app_type] => utility [patent_app_number] => 13/611118 [patent_app_country] => US [patent_app_date] => 2012-09-12 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 4 [patent_figures_cnt] => 5 [patent_no_of_words] => 3800 [patent_no_of_claims] => 9 [patent_no_of_ind_claims] => 4 [patent_words_short_claim] => 74 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13611118 [rel_patent_id] =>[rel_patent_doc_number] =>)
13/611118
Method and apparatus for operating an aircraft landing system Sep 11, 2012 Issued
Array ( [id] => 8513516 [patent_doc_number] => 20120312924 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2012-12-13 [patent_title] => 'ICE SHED REDUCTION FOR LEADING EDGE STRUCTURES' [patent_app_type] => utility [patent_app_number] => 13/590970 [patent_app_country] => US [patent_app_date] => 2012-08-21 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 10 [patent_figures_cnt] => 10 [patent_no_of_words] => 2012 [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] =>[firstpage_image] =>[orig_patent_app_number] => 13590970 [rel_patent_id] =>[rel_patent_doc_number] =>)
13/590970
ICE SHED REDUCTION FOR LEADING EDGE STRUCTURES Aug 20, 2012 Abandoned
Array ( [id] => 9064709 [patent_doc_number] => 20130256465 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2013-10-03 [patent_title] => 'Rotorcraft with Variable Incident Wing' [patent_app_type] => utility [patent_app_number] => 13/586020 [patent_app_country] => US [patent_app_date] => 2012-08-15 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 6 [patent_figures_cnt] => 6 [patent_no_of_words] => 2851 [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] =>[firstpage_image] =>[orig_patent_app_number] => 13586020 [rel_patent_id] =>[rel_patent_doc_number] =>)
13/586020
Rotorcraft with variable incident wing Aug 14, 2012 Issued
Array ( [id] => 8513509 [patent_doc_number] => 20120312917 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2012-12-13 [patent_title] => 'Tilt rotor vertical take-off aircraft - K' [patent_app_type] => utility [patent_app_number] => 13/507084 [patent_app_country] => US [patent_app_date] => 2012-06-04 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 15 [patent_figures_cnt] => 15 [patent_no_of_words] => 2746 [patent_no_of_claims] => 9 [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] =>[firstpage_image] =>[orig_patent_app_number] => 13507084 [rel_patent_id] =>[rel_patent_doc_number] =>)
13/507084
Tilt rotor vertical take-off aircraft - K Jun 3, 2012 Abandoned
Array ( [id] => 8857066 [patent_doc_number] => 08459591 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2013-06-11 [patent_title] => 'Methods and apparatus for aerial recovery of flying apparatus' [patent_app_type] => utility [patent_app_number] => 13/465220 [patent_app_country] => US [patent_app_date] => 2012-05-07 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 11 [patent_figures_cnt] => 11 [patent_no_of_words] => 4257 [patent_no_of_claims] => 16 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 91 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13465220 [rel_patent_id] =>[rel_patent_doc_number] =>)
13/465220
Methods and apparatus for aerial recovery of flying apparatus May 6, 2012 Issued
Array ( [id] => 9046538 [patent_doc_number] => 08541091 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2013-09-24 [patent_title] => 'Composite leg for landing gear assembly' [patent_app_type] => utility [patent_app_number] => 13/429630 [patent_app_country] => US [patent_app_date] => 2012-03-26 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 4 [patent_figures_cnt] => 8 [patent_no_of_words] => 2899 [patent_no_of_claims] => 20 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 57 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13429630 [rel_patent_id] =>[rel_patent_doc_number] =>)
13/429630
Composite leg for landing gear assembly Mar 25, 2012 Issued
Array ( [id] => 8273723 [patent_doc_number] => 20120167592 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2012-07-05 [patent_title] => 'MOUNTING SYSTEM FOR A GAS TURBINE ENGINE' [patent_app_type] => utility [patent_app_number] => 13/414763 [patent_app_country] => US [patent_app_date] => 2012-03-08 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 8 [patent_figures_cnt] => 8 [patent_no_of_words] => 3057 [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] =>[firstpage_image] =>[orig_patent_app_number] => 13414763 [rel_patent_id] =>[rel_patent_doc_number] =>)
13/414763
Mounting system for a gas turbine engine Mar 7, 2012 Issued
Array ( [id] => 8673933 [patent_doc_number] => 08382037 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2013-02-26 [patent_title] => 'Composite barrel sections for aircraft fuselages and other structures' [patent_app_type] => utility [patent_app_number] => 13/411439 [patent_app_country] => US [patent_app_date] => 2012-03-02 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 11 [patent_figures_cnt] => 21 [patent_no_of_words] => 7728 [patent_no_of_claims] => 4 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 108 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13411439 [rel_patent_id] =>[rel_patent_doc_number] =>)
13/411439
Composite barrel sections for aircraft fuselages and other structures Mar 1, 2012 Issued
Array ( [id] => 9842468 [patent_doc_number] => 08944370 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2015-02-03 [patent_title] => 'Plasma actuating propulsion system for aerial vehicles' [patent_app_type] => utility [patent_app_number] => 13/346467 [patent_app_country] => US [patent_app_date] => 2012-01-09 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 8 [patent_figures_cnt] => 12 [patent_no_of_words] => 2522 [patent_no_of_claims] => 8 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 118 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13346467 [rel_patent_id] =>[rel_patent_doc_number] =>)
13/346467
Plasma actuating propulsion system for aerial vehicles Jan 8, 2012 Issued
Array ( [id] => 9702155 [patent_doc_number] => 08827209 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2014-09-09 [patent_title] => 'Methods and systems for propelling an externally powered vehicle' [patent_app_type] => utility [patent_app_number] => 13/311667 [patent_app_country] => US [patent_app_date] => 2011-12-06 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 2 [patent_figures_cnt] => 3 [patent_no_of_words] => 3175 [patent_no_of_claims] => 13 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 122 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13311667 [rel_patent_id] =>[rel_patent_doc_number] =>)
13/311667
Methods and systems for propelling an externally powered vehicle Dec 5, 2011 Issued
Array ( [id] => 8224541 [patent_doc_number] => 20120138746 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2012-06-07 [patent_title] => 'OBLIQUE PANEL AT THE REAR OF A CENTRAL BOX OF AN AIRCRAFT FUSELAGE' [patent_app_type] => utility [patent_app_number] => 13/307394 [patent_app_country] => US [patent_app_date] => 2011-11-30 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 4 [patent_figures_cnt] => 4 [patent_no_of_words] => 1965 [patent_no_of_claims] => 12 [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] =>[firstpage_image] =>[orig_patent_app_number] => 13307394 [rel_patent_id] =>[rel_patent_doc_number] =>)
13/307394
Oblique panel at the rear of a central box of an aircraft fuselage Nov 29, 2011 Issued
Array ( [id] => 8825636 [patent_doc_number] => 20130126680 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2013-05-23 [patent_title] => 'UNMANNED AIR VEHICLE FAULT TOLERANT FLIGHT CONTROL SYSTEM AND METHOD' [patent_app_type] => utility [patent_app_number] => 13/299088 [patent_app_country] => US [patent_app_date] => 2011-11-17 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 6 [patent_figures_cnt] => 6 [patent_no_of_words] => 7658 [patent_no_of_claims] => 15 [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] =>[firstpage_image] =>[orig_patent_app_number] => 13299088 [rel_patent_id] =>[rel_patent_doc_number] =>)
13/299088
UNMANNED AIR VEHICLE FAULT TOLERANT FLIGHT CONTROL SYSTEM AND METHOD Nov 16, 2011 Abandoned
Array ( [id] => 8204633 [patent_doc_number] => 20120126052 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2012-05-24 [patent_title] => 'FLIGHT DEVICE' [patent_app_type] => utility [patent_app_number] => 13/299105 [patent_app_country] => US [patent_app_date] => 2011-11-17 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 17 [patent_figures_cnt] => 17 [patent_no_of_words] => 15552 [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/A1/0126/20120126052.pdf [firstpage_image] =>[orig_patent_app_number] => 13299105 [rel_patent_id] =>[rel_patent_doc_number] =>)
13/299105
FLIGHT DEVICE Nov 16, 2011 Abandoned
Array ( [id] => 9374067 [patent_doc_number] => 08678318 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2014-03-25 [patent_title] => 'Insulation arrangement in an aircraft' [patent_app_type] => utility [patent_app_number] => 13/298393 [patent_app_country] => US [patent_app_date] => 2011-11-17 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 5 [patent_figures_cnt] => 6 [patent_no_of_words] => 3141 [patent_no_of_claims] => 11 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 162 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13298393 [rel_patent_id] =>[rel_patent_doc_number] =>)
13/298393
Insulation arrangement in an aircraft Nov 16, 2011 Issued
Array ( [id] => 8216900 [patent_doc_number] => 20120132748 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2012-05-31 [patent_title] => 'AIRCRAFT STRUCTURE' [patent_app_type] => utility [patent_app_number] => 13/297581 [patent_app_country] => US [patent_app_date] => 2011-11-16 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 10 [patent_figures_cnt] => 10 [patent_no_of_words] => 7313 [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] =>[firstpage_image] =>[orig_patent_app_number] => 13297581 [rel_patent_id] =>[rel_patent_doc_number] =>)
13/297581
Aircraft structure comprising a skin panel Nov 15, 2011 Issued
Array ( [id] => 9165162 [patent_doc_number] => 08590834 [patent_country] => US [patent_kind] => B1 [patent_issue_date] => 2013-11-26 [patent_title] => 'Aircraft control surface actuation system with helical actuation path' [patent_app_type] => utility [patent_app_number] => 13/295187 [patent_app_country] => US [patent_app_date] => 2011-11-14 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 6 [patent_figures_cnt] => 6 [patent_no_of_words] => 3637 [patent_no_of_claims] => 14 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 55 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13295187 [rel_patent_id] =>[rel_patent_doc_number] =>)
13/295187
Aircraft control surface actuation system with helical actuation path Nov 13, 2011 Issued
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