
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] => 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 |