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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] => 5282169 [patent_doc_number] => 20090095842 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2009-04-16 [patent_title] => 'Power distribution architecture for an ice protection system' [patent_app_type] => utility [patent_app_number] => 11/974697 [patent_app_country] => US [patent_app_date] => 2007-10-15 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 4 [patent_figures_cnt] => 4 [patent_no_of_words] => 4203 [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] => publications/A1/0095/20090095842.pdf [firstpage_image] =>[orig_patent_app_number] => 11974697 [rel_patent_id] =>[rel_patent_doc_number] =>)
11/974697
Power distribution architecture for an ice protection system Oct 14, 2007 Issued
Array ( [id] => 4603902 [patent_doc_number] => 07984880 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2011-07-26 [patent_title] => 'Mechanisms and methods for providing rudder control assist during symmetrical and asymmetrical thrust conditions' [patent_app_type] => utility [patent_app_number] => 11/869219 [patent_app_country] => US [patent_app_date] => 2007-10-09 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 9 [patent_figures_cnt] => 16 [patent_no_of_words] => 5180 [patent_no_of_claims] => 15 [patent_no_of_ind_claims] => 4 [patent_words_short_claim] => 304 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/07/984/07984880.pdf [firstpage_image] =>[orig_patent_app_number] => 11869219 [rel_patent_id] =>[rel_patent_doc_number] =>)
11/869219
Mechanisms and methods for providing rudder control assist during symmetrical and asymmetrical thrust conditions Oct 8, 2007 Issued
Array ( [id] => 4723678 [patent_doc_number] => 20080203219 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2008-08-28 [patent_title] => 'Hydrogen powered aircraft' [patent_app_type] => utility [patent_app_number] => 11/973092 [patent_app_country] => US [patent_app_date] => 2007-10-05 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 9 [patent_figures_cnt] => 9 [patent_no_of_words] => 8886 [patent_no_of_claims] => 5 [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/A1/0203/20080203219.pdf [firstpage_image] =>[orig_patent_app_number] => 11973092 [rel_patent_id] =>[rel_patent_doc_number] =>)
11/973092
Hydrogen powered aircraft Oct 4, 2007 Issued
Array ( [id] => 139600 [patent_doc_number] => 07686251 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2010-03-30 [patent_title] => 'Rib support for wing panels' [patent_app_type] => utility [patent_app_number] => 11/867158 [patent_app_country] => US [patent_app_date] => 2007-10-04 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 7 [patent_figures_cnt] => 11 [patent_no_of_words] => 4764 [patent_no_of_claims] => 14 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 182 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/07/686/07686251.pdf [firstpage_image] =>[orig_patent_app_number] => 11867158 [rel_patent_id] =>[rel_patent_doc_number] =>)
11/867158
Rib support for wing panels Oct 3, 2007 Issued
Array ( [id] => 4918977 [patent_doc_number] => 20080067287 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2008-03-20 [patent_title] => 'PROPULSION SYSTEM WITH INTEGRATED PYLON' [patent_app_type] => utility [patent_app_number] => 11/857735 [patent_app_country] => US [patent_app_date] => 2007-09-19 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 5 [patent_figures_cnt] => 5 [patent_no_of_words] => 2604 [patent_no_of_claims] => 19 [patent_no_of_ind_claims] => 11 [patent_words_short_claim] => 0 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] => publications/A1/0067/20080067287.pdf [firstpage_image] =>[orig_patent_app_number] => 11857735 [rel_patent_id] =>[rel_patent_doc_number] =>)
11/857735
Propulsion system with integrated pylon Sep 18, 2007 Issued
Array ( [id] => 4536231 [patent_doc_number] => 07959106 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2011-06-14 [patent_title] => 'Integrated propulsive system comprising a bypass turbojet engine' [patent_app_type] => utility [patent_app_number] => 11/856468 [patent_app_country] => US [patent_app_date] => 2007-09-17 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 3 [patent_figures_cnt] => 5 [patent_no_of_words] => 2155 [patent_no_of_claims] => 17 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 188 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/07/959/07959106.pdf [firstpage_image] =>[orig_patent_app_number] => 11856468 [rel_patent_id] =>[rel_patent_doc_number] =>)
11/856468
Integrated propulsive system comprising a bypass turbojet engine Sep 16, 2007 Issued
Array ( [id] => 5319497 [patent_doc_number] => 20090057487 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2009-03-05 [patent_title] => 'COMPOSITE FABRIC WITH RIGID MEMBER STRUCTURE' [patent_app_type] => utility [patent_app_number] => 11/849794 [patent_app_country] => US [patent_app_date] => 2007-09-04 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 9 [patent_figures_cnt] => 9 [patent_no_of_words] => 5285 [patent_no_of_claims] => 41 [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/A1/0057/20090057487.pdf [firstpage_image] =>[orig_patent_app_number] => 11849794 [rel_patent_id] =>[rel_patent_doc_number] =>)
11/849794
Composite fabric with rigid member structure Sep 3, 2007 Issued
Array ( [id] => 9310212 [patent_doc_number] => 08651423 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2014-02-18 [patent_title] => 'Fireproof bulkhead of a highly porous structure with intumescent coating and method for its production' [patent_app_type] => utility [patent_app_number] => 11/897321 [patent_app_country] => US [patent_app_date] => 2007-08-30 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 2 [patent_figures_cnt] => 3 [patent_no_of_words] => 3243 [patent_no_of_claims] => 15 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 87 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 11897321 [rel_patent_id] =>[rel_patent_doc_number] =>)
11/897321
Fireproof bulkhead of a highly porous structure with intumescent coating and method for its production Aug 29, 2007 Issued
Array ( [id] => 5319491 [patent_doc_number] => 20090057481 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2009-03-05 [patent_title] => 'Dual-Power Transmission Device for a Twin-Rotor Helicopter' [patent_app_type] => utility [patent_app_number] => 11/846564 [patent_app_country] => US [patent_app_date] => 2007-08-29 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 3 [patent_figures_cnt] => 3 [patent_no_of_words] => 2286 [patent_no_of_claims] => 9 [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/A1/0057/20090057481.pdf [firstpage_image] =>[orig_patent_app_number] => 11846564 [rel_patent_id] =>[rel_patent_doc_number] =>)
11/846564
Dual-Power Transmission Device for a Twin-Rotor Helicopter Aug 28, 2007 Abandoned
Array ( [id] => 4596761 [patent_doc_number] => 07975967 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2011-07-12 [patent_title] => 'Automatic activation device for a parachute and a method for activating an opening of a parachute' [patent_app_type] => utility [patent_app_number] => 11/892421 [patent_app_country] => US [patent_app_date] => 2007-08-22 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 5 [patent_figures_cnt] => 6 [patent_no_of_words] => 5330 [patent_no_of_claims] => 17 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 60 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/07/975/07975967.pdf [firstpage_image] =>[orig_patent_app_number] => 11892421 [rel_patent_id] =>[rel_patent_doc_number] =>)
11/892421
Automatic activation device for a parachute and a method for activating an opening of a parachute Aug 21, 2007 Issued
Array ( [id] => 4586083 [patent_doc_number] => 07851734 [patent_country] => US [patent_kind] => B1 [patent_issue_date] => 2010-12-14 [patent_title] => 'Acceleration activated fin release mechanism' [patent_app_type] => utility [patent_app_number] => 11/842647 [patent_app_country] => US [patent_app_date] => 2007-08-21 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 3 [patent_figures_cnt] => 7 [patent_no_of_words] => 1532 [patent_no_of_claims] => 9 [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] => patents/07/851/07851734.pdf [firstpage_image] =>[orig_patent_app_number] => 11842647 [rel_patent_id] =>[rel_patent_doc_number] =>)
11/842647
Acceleration activated fin release mechanism Aug 20, 2007 Issued
Array ( [id] => 5444058 [patent_doc_number] => 20090045284 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2009-02-19 [patent_title] => 'Corded Orientation System For Lighter-Than-Air Aircraft' [patent_app_type] => utility [patent_app_number] => 11/840607 [patent_app_country] => US [patent_app_date] => 2007-08-17 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 11 [patent_figures_cnt] => 11 [patent_no_of_words] => 1874 [patent_no_of_claims] => 12 [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/A1/0045/20090045284.pdf [firstpage_image] =>[orig_patent_app_number] => 11840607 [rel_patent_id] =>[rel_patent_doc_number] =>)
11/840607
Corded Orientation System For Lighter-Than-Air Aircraft Aug 16, 2007 Abandoned
Array ( [id] => 5413320 [patent_doc_number] => 20090039207 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2009-02-12 [patent_title] => 'FLYING OBJECT' [patent_app_type] => utility [patent_app_number] => 11/836652 [patent_app_country] => US [patent_app_date] => 2007-08-09 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 18 [patent_figures_cnt] => 18 [patent_no_of_words] => 4805 [patent_no_of_claims] => 32 [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/A1/0039/20090039207.pdf [firstpage_image] =>[orig_patent_app_number] => 11836652 [rel_patent_id] =>[rel_patent_doc_number] =>)
11/836652
Flying object Aug 8, 2007 Issued
Array ( [id] => 8100919 [patent_doc_number] => 08152105 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2012-04-10 [patent_title] => 'Parachute canopy packing sleeve and method of use' [patent_app_type] => utility [patent_app_number] => 11/830965 [patent_app_country] => US [patent_app_date] => 2007-07-31 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 3 [patent_figures_cnt] => 9 [patent_no_of_words] => 3945 [patent_no_of_claims] => 19 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 97 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/08/152/08152105.pdf [firstpage_image] =>[orig_patent_app_number] => 11830965 [rel_patent_id] =>[rel_patent_doc_number] =>)
11/830965
Parachute canopy packing sleeve and method of use Jul 30, 2007 Issued
Array ( [id] => 5518336 [patent_doc_number] => 20090026317 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2009-01-29 [patent_title] => 'TRANSLATING FLAP DRIVE DOOR' [patent_app_type] => utility [patent_app_number] => 11/829780 [patent_app_country] => US [patent_app_date] => 2007-07-27 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 9 [patent_figures_cnt] => 9 [patent_no_of_words] => 2895 [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/A1/0026/20090026317.pdf [firstpage_image] =>[orig_patent_app_number] => 11829780 [rel_patent_id] =>[rel_patent_doc_number] =>)
11/829780
Translating flap drive door Jul 26, 2007 Issued
Array ( [id] => 4748870 [patent_doc_number] => 20080156940 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2008-07-03 [patent_title] => 'DEVICE FOR INTERCONNECTING FIRST AND SECOND CONTROL STICKS OF AN AIRCRAFT IN ROLL AND IN PITCH' [patent_app_type] => utility [patent_app_number] => 11/779332 [patent_app_country] => US [patent_app_date] => 2007-07-18 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 3 [patent_figures_cnt] => 3 [patent_no_of_words] => 4236 [patent_no_of_claims] => 14 [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/A1/0156/20080156940.pdf [firstpage_image] =>[orig_patent_app_number] => 11779332 [rel_patent_id] =>[rel_patent_doc_number] =>)
11/779332
Device for interconnecting first and second control sticks of an aircraft in roll and in pitch Jul 17, 2007 Issued
Array ( [id] => 4918982 [patent_doc_number] => 20080067292 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2008-03-20 [patent_title] => 'VORTEX GENERATOR AT HOT GAS OUTPUT' [patent_app_type] => utility [patent_app_number] => 11/775483 [patent_app_country] => US [patent_app_date] => 2007-07-10 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 5 [patent_figures_cnt] => 5 [patent_no_of_words] => 2721 [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/A1/0067/20080067292.pdf [firstpage_image] =>[orig_patent_app_number] => 11775483 [rel_patent_id] =>[rel_patent_doc_number] =>)
11/775483
Vortex generator at hot gas output Jul 9, 2007 Issued
Array ( [id] => 4800312 [patent_doc_number] => 20080011899 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2008-01-17 [patent_title] => 'Light weight vertical takeoff and landing aircraft' [patent_app_type] => utility [patent_app_number] => 11/825622 [patent_app_country] => US [patent_app_date] => 2007-07-09 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 4 [patent_figures_cnt] => 4 [patent_no_of_words] => 2327 [patent_no_of_claims] => 20 [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/A1/0011/20080011899.pdf [firstpage_image] =>[orig_patent_app_number] => 11825622 [rel_patent_id] =>[rel_patent_doc_number] =>)
11/825622
Light weight vertical takeoff and landing aircraft Jul 8, 2007 Abandoned
Array ( [id] => 4723682 [patent_doc_number] => 20080203223 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2008-08-28 [patent_title] => 'AIRCRAFT STABILIZER ACTUATOR' [patent_app_type] => utility [patent_app_number] => 11/766815 [patent_app_country] => US [patent_app_date] => 2007-06-22 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 3 [patent_figures_cnt] => 3 [patent_no_of_words] => 1985 [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] => publications/A1/0203/20080203223.pdf [firstpage_image] =>[orig_patent_app_number] => 11766815 [rel_patent_id] =>[rel_patent_doc_number] =>)
11/766815
AIRCRAFT STABILIZER ACTUATOR Jun 21, 2007 Abandoned
Array ( [id] => 4849297 [patent_doc_number] => 20080315039 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2008-12-25 [patent_title] => 'System and methods for space vehicle torque balancing' [patent_app_type] => utility [patent_app_number] => 11/820916 [patent_app_country] => US [patent_app_date] => 2007-06-21 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 6 [patent_figures_cnt] => 6 [patent_no_of_words] => 5901 [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] => publications/A1/0315/20080315039.pdf [firstpage_image] =>[orig_patent_app_number] => 11820916 [rel_patent_id] =>[rel_patent_doc_number] =>)
11/820916
System and methods for space vehicle torque balancing Jun 20, 2007 Abandoned
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