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] => 11218507
[patent_doc_number] => 09446834
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2016-09-20
[patent_title] => 'Self-stiffened skin for aircraft fuselage including stringers with a closed section and associated manufacturing method'
[patent_app_type] => utility
[patent_app_number] => 14/140513
[patent_app_country] => US
[patent_app_date] => 2013-12-25
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 7
[patent_figures_cnt] => 13
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[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14140513
[rel_patent_id] =>[rel_patent_doc_number] =>) 14/140513 | Self-stiffened skin for aircraft fuselage including stringers with a closed section and associated manufacturing method | Dec 24, 2013 | Issued |
Array
(
[id] => 9565586
[patent_doc_number] => 20140183299
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2014-07-03
[patent_title] => 'AN AIRCRAFT COMPRISING A COCKPIT DELOCALIZED OUTSIDED THE NOSE'
[patent_app_type] => utility
[patent_app_number] => 14/138417
[patent_app_country] => US
[patent_app_date] => 2013-12-23
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 2
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[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14138417
[rel_patent_id] =>[rel_patent_doc_number] =>) 14/138417 | AN AIRCRAFT COMPRISING A COCKPIT DELOCALIZED OUTSIDED THE NOSE | Dec 22, 2013 | Abandoned |
Array
(
[id] => 10628390
[patent_doc_number] => 09346534
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2016-05-24
[patent_title] => 'Support assembly'
[patent_app_type] => utility
[patent_app_number] => 14/101791
[patent_app_country] => US
[patent_app_date] => 2013-12-10
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 7
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[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14101791
[rel_patent_id] =>[rel_patent_doc_number] =>) 14/101791 | Support assembly | Dec 9, 2013 | Issued |
Array
(
[id] => 10274590
[patent_doc_number] => 20150159587
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2015-06-11
[patent_title] => 'CLUSTER ROCKET MOTOR BOOSTERS'
[patent_app_type] => utility
[patent_app_number] => 14/100362
[patent_app_country] => US
[patent_app_date] => 2013-12-09
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 11
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[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14100362
[rel_patent_id] =>[rel_patent_doc_number] =>) 14/100362 | Cluster rocket motor boosters | Dec 8, 2013 | Issued |
Array
(
[id] => 10594180
[patent_doc_number] => 09315254
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2016-04-19
[patent_title] => 'Joint assembly and method of assembling same'
[patent_app_type] => utility
[patent_app_number] => 14/051926
[patent_app_country] => US
[patent_app_date] => 2013-10-11
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 8
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[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14051926
[rel_patent_id] =>[rel_patent_doc_number] =>) 14/051926 | Joint assembly and method of assembling same | Oct 10, 2013 | Issued |
Array
(
[id] => 10198879
[patent_doc_number] => 20150083865
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2015-03-26
[patent_title] => 'MULTIPLE SPACECRAFT LAUNCH SYSTEM'
[patent_app_type] => utility
[patent_app_number] => 14/034328
[patent_app_country] => US
[patent_app_date] => 2013-09-23
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
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[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14034328
[rel_patent_id] =>[rel_patent_doc_number] =>) 14/034328 | MULTIPLE SPACECRAFT LAUNCH SYSTEM | Sep 22, 2013 | Abandoned |
Array
(
[id] => 10044974
[patent_doc_number] => 09085361
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2015-07-21
[patent_title] => 'Landing gear provided with a stiffener for increasing its stiffness in roll, and an aircraft'
[patent_app_type] => utility
[patent_app_number] => 14/033630
[patent_app_country] => US
[patent_app_date] => 2013-09-23
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
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[patent_no_of_words] => 4971
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[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14033630
[rel_patent_id] =>[rel_patent_doc_number] =>) 14/033630 | Landing gear provided with a stiffener for increasing its stiffness in roll, and an aircraft | Sep 22, 2013 | Issued |
Array
(
[id] => 9220004
[patent_doc_number] => 20140014779
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2014-01-16
[patent_title] => 'Direct Flight Far Space Shuttle'
[patent_app_type] => utility
[patent_app_number] => 14/026791
[patent_app_country] => US
[patent_app_date] => 2013-09-13
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 18
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[patent_no_of_words] => 6432
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[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14026791
[rel_patent_id] =>[rel_patent_doc_number] =>) 14/026791 | Direct Flight Far Space Shuttle | Sep 12, 2013 | Abandoned |
Array
(
[id] => 10361728
[patent_doc_number] => 20150246733
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2015-09-03
[patent_title] => 'DEVICE AND METHOD FOR SUPPLYING NON-PROPULSIVE POWER FOR AN AIRCRAFT'
[patent_app_type] => utility
[patent_app_number] => 14/427625
[patent_app_country] => US
[patent_app_date] => 2013-09-10
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
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[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14427625
[rel_patent_id] =>[rel_patent_doc_number] =>) 14/427625 | DEVICE AND METHOD FOR SUPPLYING NON-PROPULSIVE POWER FOR AN AIRCRAFT | Sep 9, 2013 | Abandoned |
Array
(
[id] => 10340078
[patent_doc_number] => 20150225082
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2015-08-13
[patent_title] => 'CARGO HANDLING SYSTEM, METHOD AND APPARATUS'
[patent_app_type] => utility
[patent_app_number] => 14/430505
[patent_app_country] => US
[patent_app_date] => 2013-09-09
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 21
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[patent_no_of_words] => 20447
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[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14430505
[rel_patent_id] =>[rel_patent_doc_number] =>) 14/430505 | Cargo handling system, method and apparatus | Sep 8, 2013 | Issued |
Array
(
[id] => 9861574
[patent_doc_number] => 20150041591
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2015-02-12
[patent_title] => 'MULTIPURPOSE FLYING BOOM'
[patent_app_type] => utility
[patent_app_number] => 13/960614
[patent_app_country] => US
[patent_app_date] => 2013-08-06
[patent_effective_date] => 0000-00-00
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[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13960614
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/960614 | Multipurpose flying boom | Aug 5, 2013 | Issued |
Array
(
[id] => 9343307
[patent_doc_number] => 08662445
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2014-03-04
[patent_title] => 'Hybrid power system architecture for an aircraft'
[patent_app_type] => utility
[patent_app_number] => 13/953164
[patent_app_country] => US
[patent_app_date] => 2013-07-29
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[rel_patent_id] =>[rel_patent_doc_number] =>) 13/953164 | Hybrid power system architecture for an aircraft | Jul 28, 2013 | Issued |
Array
(
[id] => 9343301
[patent_doc_number] => 08662439
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2014-03-04
[patent_title] => 'System and method for limiting cyclic control inputs'
[patent_app_type] => utility
[patent_app_number] => 13/949814
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[rel_patent_id] =>[rel_patent_doc_number] =>) 13/949814 | System and method for limiting cyclic control inputs | Jul 23, 2013 | Issued |
Array
(
[id] => 9277600
[patent_doc_number] => 20140027568
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2014-01-30
[patent_title] => 'METHOD FOR GENERATING HYDRAULIC POWER IN AN AIRCRAFT, USE OF A HYBRID POWER CONTROL UNIT AND DRIVE SYSTEM'
[patent_app_type] => utility
[patent_app_number] => 13/946422
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[rel_patent_id] =>[rel_patent_doc_number] =>) 13/946422 | Method for generating hydraulic power in an aircraft, use of a hybrid power control unit and drive system | Jul 18, 2013 | Issued |
Array
(
[id] => 9474054
[patent_doc_number] => 20140131517
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2014-05-15
[patent_title] => 'AERODYNAMIC, BLUNT AFT BODY'
[patent_app_type] => utility
[patent_app_number] => 13/944144
[patent_app_country] => US
[patent_app_date] => 2013-07-17
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[rel_patent_id] =>[rel_patent_doc_number] =>) 13/944144 | Aerodynamic, blunt aft body | Jul 16, 2013 | Issued |
Array
(
[id] => 10175733
[patent_doc_number] => 09205922
[patent_country] => US
[patent_kind] => B1
[patent_issue_date] => 2015-12-08
[patent_title] => 'Systems and methods for implementing a payload distribution system'
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[rel_patent_id] =>[rel_patent_doc_number] =>) 13/943965 | Systems and methods for implementing a payload distribution system | Jul 16, 2013 | Issued |
Array
(
[id] => 10169012
[patent_doc_number] => 09199713
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2015-12-01
[patent_title] => 'Pressure panels'
[patent_app_type] => utility
[patent_app_number] => 13/936468
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[rel_patent_id] =>[rel_patent_doc_number] =>) 13/936468 | Pressure panels | Jul 7, 2013 | Issued |
Array
(
[id] => 10514516
[patent_doc_number] => 09241545
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2016-01-26
[patent_title] => 'Buckle assembly'
[patent_app_type] => utility
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Array
(
[id] => 9272320
[patent_doc_number] => 08636246
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[patent_issue_date] => 2014-01-28
[patent_title] => 'Aircraft wing extension and nozzle system'
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Array
(
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[patent_issue_date] => 2018-08-28
[patent_title] => Method and architecture for the optimized transfer of power between an auxiliary power motor and the main engines of a helicopter
[patent_app_type] => utility
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[rel_patent_id] =>[rel_patent_doc_number] =>) 14/406054 | Method and architecture for the optimized transfer of power between an auxiliary power motor and the main engines of a helicopter | Jun 11, 2013 | Issued |