Search

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 numberTitle of the applicationFiling DateStatus
Array ( [id] => 5256579 [patent_doc_number] => 20070210211 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2007-09-13 [patent_title] => 'Airplane body and method for manufacturing it' [patent_app_type] => utility [patent_app_number] => 11/703206 [patent_app_country] => US [patent_app_date] => 2007-02-07 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 5 [patent_figures_cnt] => 5 [patent_no_of_words] => 4347 [patent_no_of_claims] => 33 [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/A1/0210/20070210211.pdf [firstpage_image] =>[orig_patent_app_number] => 11703206 [rel_patent_id] =>[rel_patent_doc_number] =>)
11/703206
Airplane body and method for manufacturing it Feb 6, 2007 Abandoned
Array ( [id] => 41240 [patent_doc_number] => 07775480 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2010-08-17 [patent_title] => 'Flying object for transonic or supersonic velocities' [patent_app_type] => utility [patent_app_number] => 11/698321 [patent_app_country] => US [patent_app_date] => 2007-01-26 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 16 [patent_figures_cnt] => 24 [patent_no_of_words] => 6313 [patent_no_of_claims] => 9 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 190 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/07/775/07775480.pdf [firstpage_image] =>[orig_patent_app_number] => 11698321 [rel_patent_id] =>[rel_patent_doc_number] =>)
11/698321
Flying object for transonic or supersonic velocities Jan 25, 2007 Issued
Array ( [id] => 4843044 [patent_doc_number] => 20080179452 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2008-07-31 [patent_title] => 'Air Vehicle Propulsion System on Gimbaled Truss' [patent_app_type] => utility [patent_app_number] => 11/627350 [patent_app_country] => US [patent_app_date] => 2007-01-25 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 15 [patent_figures_cnt] => 15 [patent_no_of_words] => 4283 [patent_no_of_claims] => 30 [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/A1/0179/20080179452.pdf [firstpage_image] =>[orig_patent_app_number] => 11627350 [rel_patent_id] =>[rel_patent_doc_number] =>)
11/627350
Air vehicle propulsion system on gimbaled truss Jan 24, 2007 Issued
Array ( [id] => 4762555 [patent_doc_number] => 20080173764 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2008-07-24 [patent_title] => 'Out-door jacket connected parachute for low altitude deployment' [patent_app_type] => utility [patent_app_number] => 11/656368 [patent_app_country] => US [patent_app_date] => 2007-01-23 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 12 [patent_figures_cnt] => 12 [patent_no_of_words] => 3447 [patent_no_of_claims] => 3 [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/A1/0173/20080173764.pdf [firstpage_image] =>[orig_patent_app_number] => 11656368 [rel_patent_id] =>[rel_patent_doc_number] =>)
11/656368
Out-door jacket connected parachute for low altitude deployment Jan 22, 2007 Abandoned
Array ( [id] => 4805371 [patent_doc_number] => 20080168949 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2008-07-17 [patent_title] => 'Electronic Animal Containment System with Direction of Approach Determination' [patent_app_type] => utility [patent_app_number] => 11/624133 [patent_app_country] => US [patent_app_date] => 2007-01-17 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 9 [patent_figures_cnt] => 9 [patent_no_of_words] => 8827 [patent_no_of_claims] => 31 [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/A1/0168/20080168949.pdf [firstpage_image] =>[orig_patent_app_number] => 11624133 [rel_patent_id] =>[rel_patent_doc_number] =>)
11/624133
Electronic animal containment system with direction of approach determination Jan 16, 2007 Issued
Array ( [id] => 4457122 [patent_doc_number] => 07878461 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2011-02-01 [patent_title] => 'System and method for an integrated backup control system' [patent_app_type] => utility [patent_app_number] => 11/654474 [patent_app_country] => US [patent_app_date] => 2007-01-17 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 3 [patent_figures_cnt] => 5 [patent_no_of_words] => 5459 [patent_no_of_claims] => 40 [patent_no_of_ind_claims] => 5 [patent_words_short_claim] => 243 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/07/878/07878461.pdf [firstpage_image] =>[orig_patent_app_number] => 11654474 [rel_patent_id] =>[rel_patent_doc_number] =>)
11/654474
System and method for an integrated backup control system Jan 16, 2007 Issued
Array ( [id] => 4805806 [patent_doc_number] => 20080169384 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2008-07-17 [patent_title] => 'FLIGHT CONTROL SYSTEM AND METHOD OF USING PIEZOELECTRIC MODAL SENSORS TO MITIGATE FLEXIBLE BODY DYNAMICS' [patent_app_type] => utility [patent_app_number] => 11/623196 [patent_app_country] => US [patent_app_date] => 2007-01-15 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 12 [patent_figures_cnt] => 12 [patent_no_of_words] => 4816 [patent_no_of_claims] => 24 [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/A1/0169/20080169384.pdf [firstpage_image] =>[orig_patent_app_number] => 11623196 [rel_patent_id] =>[rel_patent_doc_number] =>)
11/623196
Flight control system and method of using piezoelectric modal sensors to mitigate flexible body dynamics Jan 14, 2007 Issued
Array ( [id] => 5227991 [patent_doc_number] => 20070290098 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2007-12-20 [patent_title] => 'AIRFOIL HAVING A MOVABLE CONTROL SURFACE' [patent_app_type] => utility [patent_app_number] => 11/620890 [patent_app_country] => US [patent_app_date] => 2007-01-08 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 8 [patent_figures_cnt] => 8 [patent_no_of_words] => 4397 [patent_no_of_claims] => 23 [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/A1/0290/20070290098.pdf [firstpage_image] =>[orig_patent_app_number] => 11620890 [rel_patent_id] =>[rel_patent_doc_number] =>)
11/620890
AIRFOIL HAVING A MOVABLE CONTROL SURFACE Jan 7, 2007 Abandoned
Array ( [id] => 4946076 [patent_doc_number] => 20080302202 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2008-12-11 [patent_title] => 'Device for Protecting and Guiding a Cable from a Direct-Vision Window of an Aircraft Flight Deck' [patent_app_type] => utility [patent_app_number] => 12/159988 [patent_app_country] => US [patent_app_date] => 2007-01-08 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 5 [patent_figures_cnt] => 5 [patent_no_of_words] => 2315 [patent_no_of_claims] => 4 [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/A1/0302/20080302202.pdf [firstpage_image] =>[orig_patent_app_number] => 12159988 [rel_patent_id] =>[rel_patent_doc_number] =>)
12/159988
Device for protecting and guiding a cable from a direct-vision window of an aircraft flight deck Jan 7, 2007 Issued
Array ( [id] => 5185849 [patent_doc_number] => 20070164155 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2007-07-19 [patent_title] => 'TELESCOPIC STOWAGE BIN' [patent_app_type] => utility [patent_app_number] => 11/618290 [patent_app_country] => US [patent_app_date] => 2006-12-29 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 7 [patent_figures_cnt] => 7 [patent_no_of_words] => 4891 [patent_no_of_claims] => 22 [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/A1/0164/20070164155.pdf [firstpage_image] =>[orig_patent_app_number] => 11618290 [rel_patent_id] =>[rel_patent_doc_number] =>)
11/618290
Telescopic stowage bin Dec 28, 2006 Issued
Array ( [id] => 5098484 [patent_doc_number] => 20070181744 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2007-08-09 [patent_title] => 'Rotorcraft skid undercarriage and a rotorcraft including such an undercarriage' [patent_app_type] => utility [patent_app_number] => 11/644844 [patent_app_country] => US [patent_app_date] => 2006-12-26 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 7 [patent_figures_cnt] => 7 [patent_no_of_words] => 3770 [patent_no_of_claims] => 17 [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/A1/0181/20070181744.pdf [firstpage_image] =>[orig_patent_app_number] => 11644844 [rel_patent_id] =>[rel_patent_doc_number] =>)
11/644844
Rotorcraft skid undercarriage and a rotorcraft including such an undercarriage Dec 25, 2006 Issued
Array ( [id] => 8256361 [patent_doc_number] => 08205833 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2012-06-26 [patent_title] => 'Composite leg structure for a lightweight aircraft seat assembly' [patent_app_type] => utility [patent_app_number] => 11/614978 [patent_app_country] => US [patent_app_date] => 2006-12-22 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 24 [patent_figures_cnt] => 31 [patent_no_of_words] => 13474 [patent_no_of_claims] => 18 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 215 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 11614978 [rel_patent_id] =>[rel_patent_doc_number] =>)
11/614978
Composite leg structure for a lightweight aircraft seat assembly Dec 21, 2006 Issued
Array ( [id] => 139591 [patent_doc_number] => 07686247 [patent_country] => US [patent_kind] => B1 [patent_issue_date] => 2010-03-30 [patent_title] => 'Vehicle recovery' [patent_app_type] => utility [patent_app_number] => 11/644141 [patent_app_country] => US [patent_app_date] => 2006-12-22 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 9 [patent_figures_cnt] => 12 [patent_no_of_words] => 7601 [patent_no_of_claims] => 21 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 145 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/07/686/07686247.pdf [firstpage_image] =>[orig_patent_app_number] => 11644141 [rel_patent_id] =>[rel_patent_doc_number] =>)
11/644141
Vehicle recovery Dec 21, 2006 Issued
Array ( [id] => 8338694 [patent_doc_number] => 08240614 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2012-08-14 [patent_title] => 'Elastomer-based modular multi-axis vibration/shock isolation device' [patent_app_type] => utility [patent_app_number] => 12/158083 [patent_app_country] => US [patent_app_date] => 2006-12-21 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 9 [patent_figures_cnt] => 17 [patent_no_of_words] => 11028 [patent_no_of_claims] => 36 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 213 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 12158083 [rel_patent_id] =>[rel_patent_doc_number] =>)
12/158083
Elastomer-based modular multi-axis vibration/shock isolation device Dec 20, 2006 Issued
Array ( [id] => 7709193 [patent_doc_number] => 08091828 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2012-01-10 [patent_title] => 'Structural element and method of manufacture' [patent_app_type] => utility [patent_app_number] => 12/093151 [patent_app_country] => US [patent_app_date] => 2006-12-15 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 10 [patent_figures_cnt] => 13 [patent_no_of_words] => 5955 [patent_no_of_claims] => 30 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 284 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/08/091/08091828.pdf [firstpage_image] =>[orig_patent_app_number] => 12093151 [rel_patent_id] =>[rel_patent_doc_number] =>)
12/093151
Structural element and method of manufacture Dec 14, 2006 Issued
Array ( [id] => 100140 [patent_doc_number] => 07721995 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2010-05-25 [patent_title] => 'Rib support for wing panels' [patent_app_type] => utility [patent_app_number] => 11/610444 [patent_app_country] => US [patent_app_date] => 2006-12-13 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 4 [patent_figures_cnt] => 4 [patent_no_of_words] => 1148 [patent_no_of_claims] => 9 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 131 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/07/721/07721995.pdf [firstpage_image] =>[orig_patent_app_number] => 11610444 [rel_patent_id] =>[rel_patent_doc_number] =>)
11/610444
Rib support for wing panels Dec 12, 2006 Issued
Array ( [id] => 4544901 [patent_doc_number] => 07837153 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2010-11-23 [patent_title] => 'Local observable area and self inspection system' [patent_app_type] => utility [patent_app_number] => 11/638021 [patent_app_country] => US [patent_app_date] => 2006-12-13 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 8 [patent_figures_cnt] => 10 [patent_no_of_words] => 3707 [patent_no_of_claims] => 21 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 92 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/07/837/07837153.pdf [firstpage_image] =>[orig_patent_app_number] => 11638021 [rel_patent_id] =>[rel_patent_doc_number] =>)
11/638021
Local observable area and self inspection system Dec 12, 2006 Issued
Array ( [id] => 183419 [patent_doc_number] => 07648103 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2010-01-19 [patent_title] => 'Aircraft fuel tanks, systems and methods for increasing an aircraft\'s on-board fuel capacity' [patent_app_type] => utility [patent_app_number] => 11/637922 [patent_app_country] => US [patent_app_date] => 2006-12-13 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 11 [patent_figures_cnt] => 11 [patent_no_of_words] => 7701 [patent_no_of_claims] => 32 [patent_no_of_ind_claims] => 4 [patent_words_short_claim] => 362 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/07/648/07648103.pdf [firstpage_image] =>[orig_patent_app_number] => 11637922 [rel_patent_id] =>[rel_patent_doc_number] =>)
11/637922
Aircraft fuel tanks, systems and methods for increasing an aircraft's on-board fuel capacity Dec 12, 2006 Issued
Array ( [id] => 6541718 [patent_doc_number] => 20100044518 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2010-02-25 [patent_title] => 'METHOD AND DEVICE FOR PROVIDING AUTOMATIC LOAD ALLEVIATION TO A HIGH LIFT SURFACE SYSTEM, IN PARTICULAR TO A LANDING FLAP SYSTEM, OF AN AIRCRAFT' [patent_app_type] => utility [patent_app_number] => 12/086467 [patent_app_country] => US [patent_app_date] => 2006-12-08 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 6 [patent_figures_cnt] => 6 [patent_no_of_words] => 4505 [patent_no_of_claims] => 22 [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/A1/0044/20100044518.pdf [firstpage_image] =>[orig_patent_app_number] => 12086467 [rel_patent_id] =>[rel_patent_doc_number] =>)
12/086467
Method and device for providing automatic load alleviation to a high lift surface system, in particular to a landing flap system, of an aircraft Dec 7, 2006 Issued
Array ( [id] => 6541718 [patent_doc_number] => 20100044518 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2010-02-25 [patent_title] => 'METHOD AND DEVICE FOR PROVIDING AUTOMATIC LOAD ALLEVIATION TO A HIGH LIFT SURFACE SYSTEM, IN PARTICULAR TO A LANDING FLAP SYSTEM, OF AN AIRCRAFT' [patent_app_type] => utility [patent_app_number] => 12/086467 [patent_app_country] => US [patent_app_date] => 2006-12-08 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 6 [patent_figures_cnt] => 6 [patent_no_of_words] => 4505 [patent_no_of_claims] => 22 [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/A1/0044/20100044518.pdf [firstpage_image] =>[orig_patent_app_number] => 12086467 [rel_patent_id] =>[rel_patent_doc_number] =>)
12/086467
Method and device for providing automatic load alleviation to a high lift surface system, in particular to a landing flap system, of an aircraft Dec 7, 2006 Issued
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