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] => 9111564 [patent_doc_number] => 08567726 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2013-10-29 [patent_title] => 'Aircraft trailing edge devices, including devices having forwardly positioned hinge lines, and associated methods' [patent_app_type] => utility [patent_app_number] => 13/252011 [patent_app_country] => US [patent_app_date] => 2011-10-03 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 7 [patent_figures_cnt] => 14 [patent_no_of_words] => 5963 [patent_no_of_claims] => 13 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 300 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13252011 [rel_patent_id] =>[rel_patent_doc_number] =>)
13/252011
Aircraft trailing edge devices, including devices having forwardly positioned hinge lines, and associated methods Oct 2, 2011 Issued
Array ( [id] => 8204632 [patent_doc_number] => 20120126056 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2012-05-24 [patent_title] => 'Compact cargo lift for commercial aircraft' [patent_app_type] => utility [patent_app_number] => 13/199696 [patent_app_country] => US [patent_app_date] => 2011-09-06 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 29 [patent_figures_cnt] => 29 [patent_no_of_words] => 11072 [patent_no_of_claims] => 20 [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/A1/0126/20120126056.pdf [firstpage_image] =>[orig_patent_app_number] => 13199696 [rel_patent_id] =>[rel_patent_doc_number] =>)
13/199696
Compact cargo lift for commercial aircraft Sep 5, 2011 Abandoned
Array ( [id] => 8537346 [patent_doc_number] => 08313063 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2012-11-20 [patent_title] => 'Parachute release system and method' [patent_app_type] => utility [patent_app_number] => 13/216448 [patent_app_country] => US [patent_app_date] => 2011-08-24 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 11 [patent_figures_cnt] => 14 [patent_no_of_words] => 8431 [patent_no_of_claims] => 20 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 75 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13216448 [rel_patent_id] =>[rel_patent_doc_number] =>)
13/216448
Parachute release system and method Aug 23, 2011 Issued
Array ( [id] => 8531957 [patent_doc_number] => 08308107 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2012-11-13 [patent_title] => 'Infrared communication system for activating power drive units in an aircraft cargo loading system' [patent_app_type] => utility [patent_app_number] => 13/188241 [patent_app_country] => US [patent_app_date] => 2011-07-21 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 18 [patent_figures_cnt] => 26 [patent_no_of_words] => 16249 [patent_no_of_claims] => 50 [patent_no_of_ind_claims] => 10 [patent_words_short_claim] => 226 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13188241 [rel_patent_id] =>[rel_patent_doc_number] =>)
13/188241
Infrared communication system for activating power drive units in an aircraft cargo loading system Jul 20, 2011 Issued
Array ( [id] => 7583890 [patent_doc_number] => 20110278400 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2011-11-17 [patent_title] => 'CONFORMAL AIRLOCK ASSEMBLY AND METHOD' [patent_app_type] => utility [patent_app_number] => 13/186312 [patent_app_country] => US [patent_app_date] => 2011-07-19 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 14 [patent_figures_cnt] => 14 [patent_no_of_words] => 6749 [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/A1/0278/20110278400.pdf [firstpage_image] =>[orig_patent_app_number] => 13186312 [rel_patent_id] =>[rel_patent_doc_number] =>)
13/186312
Conformal airlock assembly and method Jul 18, 2011 Issued
Array ( [id] => 7787451 [patent_doc_number] => 20120049007 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2012-03-01 [patent_title] => 'AIRCRAFT WING MODIFICATION AND RELATED METHODS' [patent_app_type] => utility [patent_app_number] => 13/171390 [patent_app_country] => US [patent_app_date] => 2011-06-28 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 12 [patent_figures_cnt] => 12 [patent_no_of_words] => 9552 [patent_no_of_claims] => 32 [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/A1/0049/20120049007.pdf [firstpage_image] =>[orig_patent_app_number] => 13171390 [rel_patent_id] =>[rel_patent_doc_number] =>)
13/171390
AIRCRAFT WING MODIFICATION AND RELATED METHODS Jun 27, 2011 Abandoned
Array ( [id] => 7758969 [patent_doc_number] => 08113468 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2012-02-14 [patent_title] => 'Precision attitude control system for gimbaled thruster' [patent_app_type] => utility [patent_app_number] => 13/165655 [patent_app_country] => US [patent_app_date] => 2011-06-21 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 8 [patent_figures_cnt] => 8 [patent_no_of_words] => 3171 [patent_no_of_claims] => 4 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 138 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/08/113/08113468.pdf [firstpage_image] =>[orig_patent_app_number] => 13165655 [rel_patent_id] =>[rel_patent_doc_number] =>)
13/165655
Precision attitude control system for gimbaled thruster Jun 20, 2011 Issued
Array ( [id] => 8694573 [patent_doc_number] => 20130056582 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2013-03-07 [patent_title] => 'LANDING GEAR MOUNTED UNDER AN AIRCRAFT WING' [patent_app_type] => utility [patent_app_number] => 13/698204 [patent_app_country] => US [patent_app_date] => 2011-05-16 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 3 [patent_figures_cnt] => 3 [patent_no_of_words] => 2548 [patent_no_of_claims] => 10 [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] => 13698204 [rel_patent_id] =>[rel_patent_doc_number] =>)
13/698204
LANDING GEAR MOUNTED UNDER AN AIRCRAFT WING May 15, 2011 Abandoned
Array ( [id] => 5931820 [patent_doc_number] => 20110210212 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2011-09-01 [patent_title] => 'Tilt rotor aircraft with tilting tail rotor - TT' [patent_app_type] => utility [patent_app_number] => 13/064855 [patent_app_country] => US [patent_app_date] => 2011-04-21 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 15 [patent_figures_cnt] => 15 [patent_no_of_words] => 2787 [patent_no_of_claims] => 7 [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/A1/0210/20110210212.pdf [firstpage_image] =>[orig_patent_app_number] => 13064855 [rel_patent_id] =>[rel_patent_doc_number] =>)
13/064855
Tilt rotor aircraft with tilting tail rotor—TT Apr 20, 2011 Issued
Array ( [id] => 8049051 [patent_doc_number] => 20120074256 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2012-03-29 [patent_title] => 'COMPRESSION SPRING WING DEPLOYMENT INITIATOR' [patent_app_type] => utility [patent_app_number] => 13/376747 [patent_app_country] => US [patent_app_date] => 2011-04-04 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 27 [patent_figures_cnt] => 27 [patent_no_of_words] => 4510 [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] => publications/A1/0074/20120074256.pdf [firstpage_image] =>[orig_patent_app_number] => 13376747 [rel_patent_id] =>[rel_patent_doc_number] =>)
13/376747
Compression spring wing deployment initiator Apr 3, 2011 Issued
Array ( [id] => 6164519 [patent_doc_number] => 20110194934 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2011-08-11 [patent_title] => 'Rotor Hub Vibration Attenuator' [patent_app_type] => utility [patent_app_number] => 13/076581 [patent_app_country] => US [patent_app_date] => 2011-03-31 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 13 [patent_figures_cnt] => 13 [patent_no_of_words] => 5182 [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/A1/0194/20110194934.pdf [firstpage_image] =>[orig_patent_app_number] => 13076581 [rel_patent_id] =>[rel_patent_doc_number] =>)
13/076581
Rotor hub vibration attenuator Mar 30, 2011 Issued
Array ( [id] => 6169241 [patent_doc_number] => 20110174920 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2011-07-21 [patent_title] => 'FLIGHT CONTROL SYSTEM ESPECIALLY SUITED FOR VTOL VEHICLES' [patent_app_type] => utility [patent_app_number] => 13/071858 [patent_app_country] => US [patent_app_date] => 2011-03-25 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 28 [patent_figures_cnt] => 28 [patent_no_of_words] => 13321 [patent_no_of_claims] => 25 [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/A1/0174/20110174920.pdf [firstpage_image] =>[orig_patent_app_number] => 13071858 [rel_patent_id] =>[rel_patent_doc_number] =>)
13/071858
FLIGHT CONTROL SYSTEM ESPECIALLY SUITED FOR VTOL VEHICLES Mar 24, 2011 Abandoned
Array ( [id] => 6083126 [patent_doc_number] => 20110215195 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2011-09-08 [patent_title] => 'AIRCRAFT CONTROL SURFACE METHODS' [patent_app_type] => utility [patent_app_number] => 13/035909 [patent_app_country] => US [patent_app_date] => 2011-02-25 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 5 [patent_figures_cnt] => 5 [patent_no_of_words] => 4976 [patent_no_of_claims] => 9 [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/A1/0215/20110215195.pdf [firstpage_image] =>[orig_patent_app_number] => 13035909 [rel_patent_id] =>[rel_patent_doc_number] =>)
13/035909
Aircraft control surface methods Feb 24, 2011 Issued
Array ( [id] => 8434277 [patent_doc_number] => 08282043 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2012-10-09 [patent_title] => 'Simultaneous momentum dumping and orbit control' [patent_app_type] => utility [patent_app_number] => 13/033170 [patent_app_country] => US [patent_app_date] => 2011-02-23 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 1 [patent_figures_cnt] => 1 [patent_no_of_words] => 7146 [patent_no_of_claims] => 16 [patent_no_of_ind_claims] => 4 [patent_words_short_claim] => 65 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13033170 [rel_patent_id] =>[rel_patent_doc_number] =>)
13/033170
Simultaneous momentum dumping and orbit control Feb 22, 2011 Issued
Array ( [id] => 8356444 [patent_doc_number] => 20120211605 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2012-08-23 [patent_title] => 'SYSTEM AND METHOD FOR CONVERTING A PASSENGER AIRCRAFT TO A CARGO AIRCRAFT' [patent_app_type] => utility [patent_app_number] => 13/010468 [patent_app_country] => US [patent_app_date] => 2011-01-20 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 0 [patent_figures_cnt] => 0 [patent_no_of_words] => 339 [patent_no_of_claims] => 5 [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] => 13010468 [rel_patent_id] =>[rel_patent_doc_number] =>)
13/010468
SYSTEM AND METHOD FOR CONVERTING A PASSENGER AIRCRAFT TO A CARGO AIRCRAFT Jan 19, 2011 Abandoned
Array ( [id] => 8243848 [patent_doc_number] => 08201771 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2012-06-19 [patent_title] => 'Helicopter rotor control system with individual blade control' [patent_app_type] => utility [patent_app_number] => 12/986664 [patent_app_country] => US [patent_app_date] => 2011-01-07 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 10 [patent_figures_cnt] => 15 [patent_no_of_words] => 9778 [patent_no_of_claims] => 5 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 161 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/08/201/08201771.pdf [firstpage_image] =>[orig_patent_app_number] => 12986664 [rel_patent_id] =>[rel_patent_doc_number] =>)
12/986664
Helicopter rotor control system with individual blade control Jan 6, 2011 Issued
Array ( [id] => 9494884 [patent_doc_number] => 08733694 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2014-05-27 [patent_title] => 'Arrangement for maintaining flow to an air inlet of an auxiliary power unit assembly' [patent_app_type] => utility [patent_app_number] => 12/985537 [patent_app_country] => US [patent_app_date] => 2011-01-06 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 4 [patent_figures_cnt] => 10 [patent_no_of_words] => 1706 [patent_no_of_claims] => 5 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 144 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 12985537 [rel_patent_id] =>[rel_patent_doc_number] =>)
12/985537
Arrangement for maintaining flow to an air inlet of an auxiliary power unit assembly Jan 5, 2011 Issued
Array ( [id] => 6152657 [patent_doc_number] => 20110155845 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2011-06-30 [patent_title] => 'RETRACTABLE HELICOPTER LANDING GEAR' [patent_app_type] => utility [patent_app_number] => 12/980967 [patent_app_country] => US [patent_app_date] => 2010-12-29 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 8 [patent_figures_cnt] => 8 [patent_no_of_words] => 2506 [patent_no_of_claims] => 11 [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/A1/0155/20110155845.pdf [firstpage_image] =>[orig_patent_app_number] => 12980967 [rel_patent_id] =>[rel_patent_doc_number] =>)
12/980967
Retractable helicopter landing gear Dec 28, 2010 Issued
Array ( [id] => 6152669 [patent_doc_number] => 20110155851 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2011-06-30 [patent_title] => 'AIRCRAFT OBSERVATION WINDOW' [patent_app_type] => utility [patent_app_number] => 12/979157 [patent_app_country] => US [patent_app_date] => 2010-12-27 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 10 [patent_figures_cnt] => 10 [patent_no_of_words] => 3156 [patent_no_of_claims] => 13 [patent_no_of_ind_claims] => 9 [patent_words_short_claim] => 0 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] => publications/A1/0155/20110155851.pdf [firstpage_image] =>[orig_patent_app_number] => 12979157 [rel_patent_id] =>[rel_patent_doc_number] =>)
12/979157
AIRCRAFT OBSERVATION WINDOW Dec 26, 2010 Abandoned
Array ( [id] => 5962643 [patent_doc_number] => 20110147532 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2011-06-23 [patent_title] => 'Device for Deploying and Aiming Structural Elements in a Space Environment' [patent_app_type] => utility [patent_app_number] => 12/970520 [patent_app_country] => US [patent_app_date] => 2010-12-16 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 8 [patent_figures_cnt] => 8 [patent_no_of_words] => 5067 [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/A1/0147/20110147532.pdf [firstpage_image] =>[orig_patent_app_number] => 12970520 [rel_patent_id] =>[rel_patent_doc_number] =>)
12/970520
Device for deploying and aiming structural elements in a space environment Dec 15, 2010 Issued
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