
Tho Dac Ta
Examiner (ID: 4422, Phone: (571)272-2014 , Office: P/2831 )
| Most Active Art Unit | 2833 |
| Art Unit(s) | 3202, 2831, 2839, 2833, 2834, 2832, 2899 |
| Total Applications | 4120 |
| Issued Applications | 3646 |
| Pending Applications | 156 |
| Abandoned Applications | 358 |
Applications
| Application number | Title of the application | Filing Date | Status |
|---|---|---|---|
Array
(
[id] => 8519502
[patent_doc_number] => 20120318910
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2012-12-20
[patent_title] => 'Propulsive Anti-Torque Nozzle System with External Rotating Sleeve for a Rotorcraft'
[patent_app_type] => utility
[patent_app_number] => 13/579002
[patent_app_country] => US
[patent_app_date] => 2010-11-12
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 6
[patent_figures_cnt] => 6
[patent_no_of_words] => 3283
[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] => 13579002
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/579002 | Propulsive anti-torque nozzle system with external rotating sleeve for a rotorcraft | Nov 11, 2010 | Issued |
Array
(
[id] => 8519503
[patent_doc_number] => 20120318911
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2012-12-20
[patent_title] => 'Anti-Torque Nozzle System with Internal Sleeve Valve for a Rotorcraft'
[patent_app_type] => utility
[patent_app_number] => 13/580532
[patent_app_country] => US
[patent_app_date] => 2010-11-12
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 6
[patent_figures_cnt] => 6
[patent_no_of_words] => 3190
[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] =>[firstpage_image] =>[orig_patent_app_number] => 13580532
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/580532 | Anti-torque nozzle system with internal sleeve valve for a rotorcraft | Nov 11, 2010 | Issued |
Array
(
[id] => 5940513
[patent_doc_number] => 20110101166
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2011-05-05
[patent_title] => 'CONTROL UNIT AND METHOD FOR CONTROLLING THE SUPPLY OF A VEHICLE WITH MULTIPLE FUELS'
[patent_app_type] => utility
[patent_app_number] => 12/940091
[patent_app_country] => US
[patent_app_date] => 2010-11-05
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
[patent_figures_cnt] => 5
[patent_no_of_words] => 6126
[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/A1/0101/20110101166.pdf
[firstpage_image] =>[orig_patent_app_number] => 12940091
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/940091 | Control unit and method for controlling the supply of a vehicle with multiple fuels | Nov 4, 2010 | Issued |
Array
(
[id] => 8506289
[patent_doc_number] => 20120305698
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2012-12-06
[patent_title] => 'Method and Apparatus for Actively Manipulating Aerodynamic Surfaces'
[patent_app_type] => utility
[patent_app_number] => 13/577633
[patent_app_country] => US
[patent_app_date] => 2010-11-04
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 13
[patent_figures_cnt] => 13
[patent_no_of_words] => 5146
[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] => 13577633
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/577633 | Method and apparatus for actively manipulating aerodynamic surfaces | Nov 3, 2010 | Issued |
Array
(
[id] => 9322215
[patent_doc_number] => 08657229
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2014-02-25
[patent_title] => 'Method and apparatus for actively manipulating aerodynamic surfaces'
[patent_app_type] => utility
[patent_app_number] => 13/703813
[patent_app_country] => US
[patent_app_date] => 2010-11-01
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 7
[patent_figures_cnt] => 7
[patent_no_of_words] => 3144
[patent_no_of_claims] => 16
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 107
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13703813
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/703813 | Method and apparatus for actively manipulating aerodynamic surfaces | Oct 31, 2010 | Issued |
Array
(
[id] => 7805082
[patent_doc_number] => 20120056034
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2012-03-08
[patent_title] => 'VARIABLE CYCLE VTOL POWERPLANT'
[patent_app_type] => utility
[patent_app_number] => 12/807311
[patent_app_country] => US
[patent_app_date] => 2010-09-02
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
[patent_figures_cnt] => 5
[patent_no_of_words] => 7703
[patent_no_of_claims] => 8
[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/A1/0056/20120056034.pdf
[firstpage_image] =>[orig_patent_app_number] => 12807311
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/807311 | Variable cycle VTOL powerplant | Sep 1, 2010 | Issued |
Array
(
[id] => 8328996
[patent_doc_number] => 08237096
[patent_country] => US
[patent_kind] => B1
[patent_issue_date] => 2012-08-07
[patent_title] => 'Mortar round glide kit'
[patent_app_type] => utility
[patent_app_number] => 12/806742
[patent_app_country] => US
[patent_app_date] => 2010-08-19
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 16
[patent_figures_cnt] => 16
[patent_no_of_words] => 6203
[patent_no_of_claims] => 14
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 198
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 12806742
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/806742 | Mortar round glide kit | Aug 18, 2010 | Issued |
Array
(
[id] => 8179617
[patent_doc_number] => 20120111995
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2012-05-10
[patent_title] => 'ENGINE ASSEMBLY FOR AN AIRCRAFT THE ENGINE ATTACHMENT STRUT OF WHICH INCLUDES A STRUCTURAL CASE FORMING AN INTERNAL RADIAL DELIMITATION OF THE SECONDARY FLOW'
[patent_app_type] => utility
[patent_app_number] => 13/383542
[patent_app_country] => US
[patent_app_date] => 2010-07-29
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 9
[patent_figures_cnt] => 9
[patent_no_of_words] => 3770
[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] => publications/A1/0111/20120111995.pdf
[firstpage_image] =>[orig_patent_app_number] => 13383542
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/383542 | Engine assembly for an aircraft the engine attachment strut of which includes a structural case forming an internal radial delimitation of the secondary flow | Jul 28, 2010 | Issued |
Array
(
[id] => 6177045
[patent_doc_number] => 20110121138
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2011-05-26
[patent_title] => 'LOW PAYLOAD WEIGHT PARACHUTE RELEASE-AWAY STATIC LINE'
[patent_app_type] => utility
[patent_app_number] => 12/842742
[patent_app_country] => US
[patent_app_date] => 2010-07-23
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 10
[patent_figures_cnt] => 10
[patent_no_of_words] => 7813
[patent_no_of_claims] => 23
[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/A1/0121/20110121138.pdf
[firstpage_image] =>[orig_patent_app_number] => 12842742
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/842742 | LOW PAYLOAD WEIGHT PARACHUTE RELEASE-AWAY STATIC LINE | Jul 22, 2010 | Abandoned |
Array
(
[id] => 7727861
[patent_doc_number] => 20120012701
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2012-01-19
[patent_title] => 'SENSOR FOR MEASURING LARGE MECHANICAL STRAINS WITH FINE ADJUSTMENT DEVICE'
[patent_app_type] => utility
[patent_app_number] => 12/839401
[patent_app_country] => US
[patent_app_date] => 2010-07-19
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 8
[patent_figures_cnt] => 8
[patent_no_of_words] => 2812
[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/A1/0012/20120012701.pdf
[firstpage_image] =>[orig_patent_app_number] => 12839401
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/839401 | Sensor for measuring large mechanical strains with fine adjustment device | Jul 18, 2010 | Issued |
Array
(
[id] => 8673939
[patent_doc_number] => 08382043
[patent_country] => US
[patent_kind] => B1
[patent_issue_date] => 2013-02-26
[patent_title] => 'Method and apparatus for aerodynamic flow control using compact high-frequency fluidic actuator arrays'
[patent_app_type] => utility
[patent_app_number] => 12/804225
[patent_app_country] => US
[patent_app_date] => 2010-07-16
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 8
[patent_figures_cnt] => 12
[patent_no_of_words] => 3631
[patent_no_of_claims] => 12
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 107
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 12804225
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/804225 | Method and apparatus for aerodynamic flow control using compact high-frequency fluidic actuator arrays | Jul 15, 2010 | Issued |
Array
(
[id] => 5962640
[patent_doc_number] => 20110147529
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2011-06-23
[patent_title] => 'METHOD AND SYSTEM FOR ENHANCED VISION IN AERIAL REFUELLING OPERATIONS'
[patent_app_type] => utility
[patent_app_number] => 12/837547
[patent_app_country] => US
[patent_app_date] => 2010-07-16
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 6
[patent_figures_cnt] => 6
[patent_no_of_words] => 5485
[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/A1/0147/20110147529.pdf
[firstpage_image] =>[orig_patent_app_number] => 12837547
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/837547 | METHOD AND SYSTEM FOR ENHANCED VISION IN AERIAL REFUELLING OPERATIONS | Jul 15, 2010 | Abandoned |
Array
(
[id] => 8943038
[patent_doc_number] => 08496207
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2013-07-30
[patent_title] => 'Connection of cabin components, cabin component and method for connecting cabin components'
[patent_app_type] => utility
[patent_app_number] => 12/836641
[patent_app_country] => US
[patent_app_date] => 2010-07-15
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 1
[patent_figures_cnt] => 2
[patent_no_of_words] => 2324
[patent_no_of_claims] => 11
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 99
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 12836641
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/836641 | Connection of cabin components, cabin component and method for connecting cabin components | Jul 14, 2010 | Issued |
Array
(
[id] => 7727851
[patent_doc_number] => 20120012694
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2012-01-19
[patent_title] => 'FAIL-SAFE AIRCRAFT ENGINE MOUNTING APPARATUS'
[patent_app_type] => utility
[patent_app_number] => 12/836197
[patent_app_country] => US
[patent_app_date] => 2010-07-14
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 11
[patent_figures_cnt] => 11
[patent_no_of_words] => 4202
[patent_no_of_claims] => 21
[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/A1/0012/20120012694.pdf
[firstpage_image] =>[orig_patent_app_number] => 12836197
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/836197 | Fail-safe aircraft engine mounting apparatus | Jul 13, 2010 | Issued |
Array
(
[id] => 8338682
[patent_doc_number] => 08240602
[patent_country] => US
[patent_kind] => B1
[patent_issue_date] => 2012-08-14
[patent_title] => 'Subsea deployment of aerial payloads utilizing long-term storage of lighter than air gases'
[patent_app_type] => utility
[patent_app_number] => 12/835435
[patent_app_country] => US
[patent_app_date] => 2010-07-13
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 8
[patent_figures_cnt] => 13
[patent_no_of_words] => 2781
[patent_no_of_claims] => 17
[patent_no_of_ind_claims] => 3
[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] => 12835435
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/835435 | Subsea deployment of aerial payloads utilizing long-term storage of lighter than air gases | Jul 12, 2010 | Issued |
Array
(
[id] => 8547773
[patent_doc_number] => 08322649
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2012-12-04
[patent_title] => 'Saucer-shaped gyroscopically stabilized vertical take-off and landing aircraft'
[patent_app_type] => utility
[patent_app_number] => 12/804011
[patent_app_country] => US
[patent_app_date] => 2010-07-09
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 39
[patent_figures_cnt] => 48
[patent_no_of_words] => 8641
[patent_no_of_claims] => 20
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 166
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 12804011
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/804011 | Saucer-shaped gyroscopically stabilized vertical take-off and landing aircraft | Jul 8, 2010 | Issued |
Array
(
[id] => 9025032
[patent_doc_number] => 08534606
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2013-09-17
[patent_title] => 'Pipe coupling device for aircraft wing'
[patent_app_type] => utility
[patent_app_number] => 12/832118
[patent_app_country] => US
[patent_app_date] => 2010-07-08
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 2
[patent_figures_cnt] => 5
[patent_no_of_words] => 1590
[patent_no_of_claims] => 10
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 103
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 12832118
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/832118 | Pipe coupling device for aircraft wing | Jul 7, 2010 | Issued |
Array
(
[id] => 8576249
[patent_doc_number] => 08342454
[patent_country] => US
[patent_kind] => B1
[patent_issue_date] => 2013-01-01
[patent_title] => 'Cooling systems'
[patent_app_type] => utility
[patent_app_number] => 12/826627
[patent_app_country] => US
[patent_app_date] => 2010-06-29
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 9
[patent_figures_cnt] => 15
[patent_no_of_words] => 12510
[patent_no_of_claims] => 20
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 249
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 12826627
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/826627 | Cooling systems | Jun 28, 2010 | Issued |
Array
(
[id] => 8231430
[patent_doc_number] => 08196867
[patent_country] => US
[patent_kind] => B1
[patent_issue_date] => 2012-06-12
[patent_title] => 'Space elevator propulsion system using mechanical waves'
[patent_app_type] => utility
[patent_app_number] => 12/822993
[patent_app_country] => US
[patent_app_date] => 2010-06-24
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 11
[patent_figures_cnt] => 11
[patent_no_of_words] => 3747
[patent_no_of_claims] => 19
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 49
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/08/196/08196867.pdf
[firstpage_image] =>[orig_patent_app_number] => 12822993
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/822993 | Space elevator propulsion system using mechanical waves | Jun 23, 2010 | Issued |
Array
(
[id] => 8179627
[patent_doc_number] => 20120112000
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2012-05-10
[patent_title] => 'NOSE GEAR OF AN AIRCRAFT COMPRISING A SINGLE CONTROL DEVICE FOR RETRACTION AND STEERING'
[patent_app_type] => utility
[patent_app_number] => 13/383874
[patent_app_country] => US
[patent_app_date] => 2010-06-23
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 2
[patent_figures_cnt] => 2
[patent_no_of_words] => 3182
[patent_no_of_claims] => 11
[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/A1/0112/20120112000.pdf
[firstpage_image] =>[orig_patent_app_number] => 13383874
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/383874 | Nose gear of an aircraft comprising a single control device for retraction and steering | Jun 22, 2010 | Issued |