
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 number | Title of the application | Filing Date | Status |
|---|---|---|---|
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
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[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
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[patent_no_of_words] => 8431
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[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
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[patent_maintenance] => 1
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[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
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[patent_no_of_words] => 6749
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[patent_no_of_ind_claims] => 2
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[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
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[patent_no_of_words] => 9552
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[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
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[patent_no_of_words] => 3171
[patent_no_of_claims] => 4
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[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
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[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
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[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
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[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
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[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
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[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'
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[patent_app_number] => 13/035909
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[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
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[patent_issue_date] => 2012-10-09
[patent_title] => 'Simultaneous momentum dumping and orbit control'
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[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
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[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'
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[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
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[patent_app_date] => 2011-01-06
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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'
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[rel_patent_id] =>[rel_patent_doc_number] =>) 12/980967 | Retractable helicopter landing gear | Dec 28, 2010 | Issued |
Array
(
[id] => 6152669
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[rel_patent_id] =>[rel_patent_doc_number] =>) 12/979157 | AIRCRAFT OBSERVATION WINDOW | Dec 26, 2010 | Abandoned |
Array
(
[id] => 5962643
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[patent_title] => 'Device for Deploying and Aiming Structural Elements in a Space Environment'
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[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 |