Minh Chau Thi Pham
Examiner (ID: 10502, Phone: (571)272-1163 , Office: P/1776 )
Most Active Art Unit | 1776 |
Art Unit(s) | 1773, 1724, 3621, 1776, 1305, 1797 |
Total Applications | 2849 |
Issued Applications | 2227 |
Pending Applications | 153 |
Abandoned Applications | 469 |
Applications
Application number | Title of the application | Filing Date | Status |
---|---|---|---|
Array
(
[id] => 6319830
[patent_doc_number] => 20100243792
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2010-09-30
[patent_title] => 'METHOD AND A DEVICE FOR OPTIMIZING THE OPERATION OF PROPULSIVE PROPELLERS DISPOSED ON EITHER SIDE OF A ROTORCRAFT FUSELAGE'
[patent_app_type] => utility
[patent_app_number] => 12/724453
[patent_app_country] => US
[patent_app_date] => 2010-03-16
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 4
[patent_no_of_words] => 8679
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[patent_maintenance] => 1
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[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0243/20100243792.pdf
[firstpage_image] =>[orig_patent_app_number] => 12724453
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/724453 | Method and a device for optimizing the operation of propulsive propellers disposed on either side of a rotorcraft fuselage | Mar 15, 2010 | Issued |
Array
(
[id] => 9400060
[patent_doc_number] => 08690106
[patent_country] => US
[patent_kind] => B1
[patent_issue_date] => 2014-04-08
[patent_title] => 'Ejector driven flow control for reducing velocity deficit profile downstream of an aerodynamic body'
[patent_app_type] => utility
[patent_app_number] => 12/723678
[patent_app_country] => US
[patent_app_date] => 2010-03-14
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 7
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[patent_no_of_words] => 6340
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[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 12723678
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/723678 | Ejector driven flow control for reducing velocity deficit profile downstream of an aerodynamic body | Mar 13, 2010 | Issued |
Array
(
[id] => 8444870
[patent_doc_number] => 08286914
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2012-10-16
[patent_title] => 'Conveyor device for airplanes'
[patent_app_type] => utility
[patent_app_number] => 12/723386
[patent_app_country] => US
[patent_app_date] => 2010-03-12
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 2
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[patent_no_of_words] => 2728
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[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 12723386
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/723386 | Conveyor device for airplanes | Mar 11, 2010 | Issued |
Array
(
[id] => 9272324
[patent_doc_number] => 08636250
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2014-01-28
[patent_title] => 'External cargo hook system for rotary-wing aircraft'
[patent_app_type] => utility
[patent_app_number] => 13/258545
[patent_app_country] => US
[patent_app_date] => 2010-03-08
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 10
[patent_figures_cnt] => 10
[patent_no_of_words] => 2174
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[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13258545
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/258545 | External cargo hook system for rotary-wing aircraft | Mar 7, 2010 | Issued |
Array
(
[id] => 10896491
[patent_doc_number] => 08919692
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2014-12-30
[patent_title] => 'Proximity sensor valve and lock system using same'
[patent_app_type] => utility
[patent_app_number] => 13/258506
[patent_app_country] => US
[patent_app_date] => 2010-03-04
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 16
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[patent_no_of_words] => 6540
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[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13258506
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/258506 | Proximity sensor valve and lock system using same | Mar 3, 2010 | Issued |
Array
(
[id] => 8736736
[patent_doc_number] => 08408495
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2013-04-02
[patent_title] => 'Fittings for attaching the vertical tail stabilizer of an aircraft'
[patent_app_type] => utility
[patent_app_number] => 12/714333
[patent_app_country] => US
[patent_app_date] => 2010-02-26
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
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[patent_no_of_words] => 2343
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[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 12714333
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/714333 | Fittings for attaching the vertical tail stabilizer of an aircraft | Feb 25, 2010 | Issued |
Array
(
[id] => 6476494
[patent_doc_number] => 20100213319
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2010-08-26
[patent_title] => 'Craft and Method of Coupling a Propulsion System to a Regenerative Fuel Cell System'
[patent_app_type] => utility
[patent_app_number] => 12/711955
[patent_app_country] => US
[patent_app_date] => 2010-02-24
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
[patent_figures_cnt] => 5
[patent_no_of_words] => 4814
[patent_no_of_claims] => 9
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[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0213/20100213319.pdf
[firstpage_image] =>[orig_patent_app_number] => 12711955
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/711955 | Craft and method of coupling a propulsion system to a regenerative fuel cell system | Feb 23, 2010 | Issued |
Array
(
[id] => 5962628
[patent_doc_number] => 20110147517
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2011-06-23
[patent_title] => 'PIVOTING STABILISING SURFACE FOR AIRCRAFT'
[patent_app_type] => utility
[patent_app_number] => 12/710849
[patent_app_country] => US
[patent_app_date] => 2010-02-23
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
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[patent_no_of_words] => 3772
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[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0147/20110147517.pdf
[firstpage_image] =>[orig_patent_app_number] => 12710849
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/710849 | Pivoting stabilising surface for aircraft | Feb 22, 2010 | Issued |
Array
(
[id] => 7727872
[patent_doc_number] => 20120012709
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2012-01-19
[patent_title] => 'FIRING PREVENTION STRUCTURE OF FUEL TANK'
[patent_app_type] => utility
[patent_app_number] => 13/203323
[patent_app_country] => US
[patent_app_date] => 2010-02-17
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
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[pdf_file] => publications/A1/0012/20120012709.pdf
[firstpage_image] =>[orig_patent_app_number] => 13203323
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/203323 | Firing prevention structure of fuel tank | Feb 16, 2010 | Issued |
Array
(
[id] => 9873341
[patent_doc_number] => 08960600
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2015-02-24
[patent_title] => 'Variable surface landing platform (VARSLAP)'
[patent_app_type] => utility
[patent_app_number] => 13/576830
[patent_app_country] => US
[patent_app_date] => 2010-02-08
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 21
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[patent_no_of_words] => 13340
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[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13576830
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/576830 | Variable surface landing platform (VARSLAP) | Feb 7, 2010 | Issued |
Array
(
[id] => 9816091
[patent_doc_number] => 08925867
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2015-01-06
[patent_title] => 'Modular adaptive electrical freight loading system'
[patent_app_type] => utility
[patent_app_number] => 13/148821
[patent_app_country] => US
[patent_app_date] => 2010-02-04
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[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13148821
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/148821 | Modular adaptive electrical freight loading system | Feb 3, 2010 | Issued |
Array
(
[id] => 6233092
[patent_doc_number] => 20100185346
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2010-07-22
[patent_title] => 'AERIAL PAYLOAD DEPLOYMENT METHOD'
[patent_app_type] => utility
[patent_app_number] => 12/690840
[patent_app_country] => US
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[firstpage_image] =>[orig_patent_app_number] => 12690840
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/690840 | AERIAL PAYLOAD DEPLOYMENT METHOD | Jan 19, 2010 | Abandoned |
Array
(
[id] => 6207915
[patent_doc_number] => 20110133023
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2011-06-09
[patent_title] => 'COLLAPSIBLE AERIAL PAYLOAD DEPLOYMENT SYSTEM AND METHOD'
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[patent_app_number] => 12/690835
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[pdf_file] => publications/A1/0133/20110133023.pdf
[firstpage_image] =>[orig_patent_app_number] => 12690835
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/690835 | COLLAPSIBLE AERIAL PAYLOAD DEPLOYMENT SYSTEM AND METHOD | Jan 19, 2010 | Abandoned |
Array
(
[id] => 10025793
[patent_doc_number] => 09067677
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2015-06-30
[patent_title] => 'Dismountable helicopter'
[patent_app_type] => utility
[patent_app_number] => 13/513722
[patent_app_country] => US
[patent_app_date] => 2009-12-02
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[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13513722
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/513722 | Dismountable helicopter | Dec 1, 2009 | Issued |
Array
(
[id] => 8621713
[patent_doc_number] => 08354627
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2013-01-15
[patent_title] => 'Torsion stop deployment system for airborne object'
[patent_app_type] => utility
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[rel_patent_id] =>[rel_patent_doc_number] =>) 12/579970 | Torsion stop deployment system for airborne object | Oct 14, 2009 | Issued |
Array
(
[id] => 6294306
[patent_doc_number] => 20100065689
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2010-03-18
[patent_title] => 'LOAD INTRODUCING ELEMENT'
[patent_app_type] => utility
[patent_app_number] => 12/560980
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[pdf_file] => publications/A1/0065/20100065689.pdf
[firstpage_image] =>[orig_patent_app_number] => 12560980
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/560980 | Load introducing element | Sep 15, 2009 | Issued |
Array
(
[id] => 9587629
[patent_doc_number] => 08777163
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2014-07-15
[patent_title] => 'Ice protection system and method'
[patent_app_type] => utility
[patent_app_number] => 12/553481
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[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 12553481
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/553481 | Ice protection system and method | Sep 2, 2009 | Issued |
Array
(
[id] => 9573546
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[patent_issue_date] => 2014-07-01
[patent_title] => 'Method and apparatus for controlling a refueling drogue'
[patent_app_type] => utility
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[rel_patent_id] =>[rel_patent_doc_number] =>) 12/551177 | Method and apparatus for controlling a refueling drogue | Aug 30, 2009 | Issued |
Array
(
[id] => 8100913
[patent_doc_number] => 08152102
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[patent_issue_date] => 2012-04-10
[patent_title] => 'Module for accommodation of crew members having a stowage bin usable from inside the module'
[patent_app_type] => utility
[patent_app_number] => 12/547223
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[rel_patent_id] =>[rel_patent_doc_number] =>) 12/547223 | Module for accommodation of crew members having a stowage bin usable from inside the module | Aug 24, 2009 | Issued |
Array
(
[id] => 8192381
[patent_doc_number] => 20120119027
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[patent_issue_date] => 2012-05-17
[patent_title] => 'FLOOR ELEMENT FOR A LOADING DECK OF AN AIRCRAFT'
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[pdf_file] => publications/A1/0119/20120119027.pdf
[firstpage_image] =>[orig_patent_app_number] => 13386325
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/386325 | Floor element for a loading deck of an aircraft | Jul 20, 2009 | Issued |