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] => 9445989
[patent_doc_number] => 20140117157
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2014-05-01
[patent_title] => 'Circumference Splice for Joining Shell Structures'
[patent_app_type] => utility
[patent_app_number] => 13/665664
[patent_app_country] => US
[patent_app_date] => 2012-10-31
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 11
[patent_figures_cnt] => 11
[patent_no_of_words] => 5339
[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] =>[firstpage_image] =>[orig_patent_app_number] => 13665664
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/665664 | Circumference splice for joining shell structures | Oct 30, 2012 | Issued |
Array
(
[id] => 9445985
[patent_doc_number] => 20140117153
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2014-05-01
[patent_title] => 'SYSTEMS AND METHODS TO LAUNCH AIRCRAFT'
[patent_app_type] => utility
[patent_app_number] => 13/662269
[patent_app_country] => US
[patent_app_date] => 2012-10-26
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
[patent_figures_cnt] => 5
[patent_no_of_words] => 1668
[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] =>[firstpage_image] =>[orig_patent_app_number] => 13662269
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/662269 | Systems and methods to launch aircraft | Oct 25, 2012 | Issued |
Array
(
[id] => 10607805
[patent_doc_number] => 09327826
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2016-05-03
[patent_title] => 'Self-centering aircraft flap position command apparatus'
[patent_app_type] => utility
[patent_app_number] => 13/660729
[patent_app_country] => US
[patent_app_date] => 2012-10-25
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 6
[patent_figures_cnt] => 6
[patent_no_of_words] => 3056
[patent_no_of_claims] => 16
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 183
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13660729
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/660729 | Self-centering aircraft flap position command apparatus | Oct 24, 2012 | Issued |
Array
(
[id] => 9334592
[patent_doc_number] => 20140061374
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2014-03-06
[patent_title] => 'METHOD FOR INCREASING LANDING GEAR EFFECTIVE LIFE AND AIRCRAFT LANDING CYCLES'
[patent_app_type] => utility
[patent_app_number] => 13/659893
[patent_app_country] => US
[patent_app_date] => 2012-10-24
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 2
[patent_figures_cnt] => 2
[patent_no_of_words] => 5341
[patent_no_of_claims] => 18
[patent_no_of_ind_claims] => 8
[patent_words_short_claim] => 0
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13659893
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/659893 | METHOD FOR INCREASING LANDING GEAR EFFECTIVE LIFE AND AIRCRAFT LANDING CYCLES | Oct 23, 2012 | Abandoned |
Array
(
[id] => 8788665
[patent_doc_number] => 20130105634
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2013-05-02
[patent_title] => 'COMPACT TWO AXIS GIMBAL FOR CONTROL STICK'
[patent_app_type] => utility
[patent_app_number] => 13/657294
[patent_app_country] => US
[patent_app_date] => 2012-10-22
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 6
[patent_figures_cnt] => 6
[patent_no_of_words] => 5300
[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] =>[firstpage_image] =>[orig_patent_app_number] => 13657294
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/657294 | Compact two axis gimbal for control stick | Oct 21, 2012 | Issued |
Array
(
[id] => 8788656
[patent_doc_number] => 20130105625
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2013-05-02
[patent_title] => 'AIRCRAFT PROVIDED WITH A BUOYANCY SYSTEM FOR A ROTARY ELEMENT'
[patent_app_type] => utility
[patent_app_number] => 13/654576
[patent_app_country] => US
[patent_app_date] => 2012-10-18
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
[patent_figures_cnt] => 5
[patent_no_of_words] => 2785
[patent_no_of_claims] => 6
[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] =>[firstpage_image] =>[orig_patent_app_number] => 13654576
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/654576 | Aircraft provided with a buoyancy system for a rotary element | Oct 17, 2012 | Issued |
Array
(
[id] => 9418509
[patent_doc_number] => 20140103159
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2014-04-17
[patent_title] => 'Tunnel wing system for lift, altitude flight, and ground effect flight'
[patent_app_type] => utility
[patent_app_number] => 13/654371
[patent_app_country] => US
[patent_app_date] => 2012-10-17
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
[patent_figures_cnt] => 5
[patent_no_of_words] => 443
[patent_no_of_claims] => 11
[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] =>[firstpage_image] =>[orig_patent_app_number] => 13654371
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/654371 | Tunnel wing system for lift, altitude flight, and ground effect flight | Oct 16, 2012 | Abandoned |
Array
(
[id] => 8850730
[patent_doc_number] => 20130140405
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2013-06-06
[patent_title] => 'Integral Powered Wing Aircraft Utilizing Full Rotary Disc Stacking With Aeronautical Enhancements'
[patent_app_type] => utility
[patent_app_number] => 13/650576
[patent_app_country] => US
[patent_app_date] => 2012-10-12
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 11
[patent_figures_cnt] => 11
[patent_no_of_words] => 4665
[patent_no_of_claims] => 10
[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] =>[firstpage_image] =>[orig_patent_app_number] => 13650576
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/650576 | Integral Powered Wing Aircraft Utilizing Full Rotary Disc Stacking With Aeronautical Enhancements | Oct 11, 2012 | Abandoned |
Array
(
[id] => 9406041
[patent_doc_number] => 20140097293
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2014-04-10
[patent_title] => 'Airplane Shock Absorbing Suspension'
[patent_app_type] => utility
[patent_app_number] => 13/649086
[patent_app_country] => US
[patent_app_date] => 2012-10-10
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 16
[patent_figures_cnt] => 16
[patent_no_of_words] => 1390
[patent_no_of_claims] => 7
[patent_no_of_ind_claims] => 1
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[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13649086
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/649086 | Airplane Shock Absorbing Suspension | Oct 9, 2012 | Abandoned |
Array
(
[id] => 9188581
[patent_doc_number] => 20130327896
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2013-12-12
[patent_title] => 'ROTORCRAFT YAW PILOTING SYSTEM MAKING USE OF A MEMBER OF THE HUMAN-OPERATED TYPE AND OF A FLIGHT CONTROL GENERATOR FO THE OBJECTIVE TYPE'
[patent_app_type] => utility
[patent_app_number] => 13/647508
[patent_app_country] => US
[patent_app_date] => 2012-10-09
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 2
[patent_figures_cnt] => 2
[patent_no_of_words] => 6580
[patent_no_of_claims] => 12
[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] =>[firstpage_image] =>[orig_patent_app_number] => 13647508
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/647508 | Rotorcraft yaw piloting system making use of a member of the human-operated type and of a flight control generator of the objective type | Oct 8, 2012 | Issued |
Array
(
[id] => 10499331
[patent_doc_number] => 09227721
[patent_country] => US
[patent_kind] => B1
[patent_issue_date] => 2016-01-05
[patent_title] => 'Variable camber continuous aerodynamic control surfaces and methods for active wing shaping control'
[patent_app_type] => utility
[patent_app_number] => 13/648197
[patent_app_country] => US
[patent_app_date] => 2012-10-09
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 39
[patent_figures_cnt] => 40
[patent_no_of_words] => 21908
[patent_no_of_claims] => 18
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 179
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13648197
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/648197 | Variable camber continuous aerodynamic control surfaces and methods for active wing shaping control | Oct 8, 2012 | Issued |
Array
(
[id] => 9709139
[patent_doc_number] => 08833696
[patent_country] => US
[patent_kind] => B1
[patent_issue_date] => 2014-09-16
[patent_title] => 'Balloon envelope adapted to direct sunlight towards payload'
[patent_app_type] => utility
[patent_app_number] => 13/631057
[patent_app_country] => US
[patent_app_date] => 2012-09-28
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 9
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[patent_no_of_words] => 11967
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[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13631057
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/631057 | Balloon envelope adapted to direct sunlight towards payload | Sep 27, 2012 | Issued |
Array
(
[id] => 10083235
[patent_doc_number] => 09120573
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2015-09-01
[patent_title] => 'Sanitary module arrangement for installation in an aircraft cabin'
[patent_app_type] => utility
[patent_app_number] => 13/627759
[patent_app_country] => US
[patent_app_date] => 2012-09-26
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 7
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[patent_no_of_words] => 8224
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[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13627759
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/627759 | Sanitary module arrangement for installation in an aircraft cabin | Sep 25, 2012 | Issued |
Array
(
[id] => 10614616
[patent_doc_number] => 09334046
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2016-05-10
[patent_title] => 'Device for maneuvering, on the ground, a door of an aircraft landing gear'
[patent_app_type] => utility
[patent_app_number] => 13/624181
[patent_app_country] => US
[patent_app_date] => 2012-09-21
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[patent_drawing_sheets_cnt] => 3
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[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13624181
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/624181 | Device for maneuvering, on the ground, a door of an aircraft landing gear | Sep 20, 2012 | Issued |
Array
(
[id] => 9025034
[patent_doc_number] => 08534608
[patent_country] => US
[patent_kind] => B1
[patent_issue_date] => 2013-09-17
[patent_title] => 'Aerial emergency load release mechanism'
[patent_app_type] => utility
[patent_app_number] => 13/602748
[patent_app_country] => US
[patent_app_date] => 2012-09-04
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[rel_patent_id] =>[rel_patent_doc_number] =>) 13/602748 | Aerial emergency load release mechanism | Sep 3, 2012 | Issued |
Array
(
[id] => 9982189
[patent_doc_number] => 09027886
[patent_country] => US
[patent_kind] => B1
[patent_issue_date] => 2015-05-12
[patent_title] => 'High altitude escape pod'
[patent_app_type] => utility
[patent_app_number] => 13/595373
[patent_app_country] => US
[patent_app_date] => 2012-08-27
[patent_effective_date] => 0000-00-00
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[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13595373
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/595373 | High altitude escape pod | Aug 26, 2012 | Issued |
Array
(
[id] => 10573867
[patent_doc_number] => 09296494
[patent_country] => US
[patent_kind] => B1
[patent_issue_date] => 2016-03-29
[patent_title] => 'Thruster orbit control method and configuration'
[patent_app_type] => utility
[patent_app_number] => 13/572586
[patent_app_country] => US
[patent_app_date] => 2012-08-10
[patent_effective_date] => 0000-00-00
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[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13572586
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/572586 | Thruster orbit control method and configuration | Aug 9, 2012 | Issued |
Array
(
[id] => 10115435
[patent_doc_number] => 09150303
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2015-10-06
[patent_title] => 'Control quadrant'
[patent_app_type] => utility
[patent_app_number] => 13/571573
[patent_app_country] => US
[patent_app_date] => 2012-08-10
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[rel_patent_id] =>[rel_patent_doc_number] =>) 13/571573 | Control quadrant | Aug 9, 2012 | Issued |
Array
(
[id] => 8680505
[patent_doc_number] => 20130048789
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2013-02-28
[patent_title] => 'AIRCRAFT STORE EJECTOR SYSTEM'
[patent_app_type] => utility
[patent_app_number] => 13/572504
[patent_app_country] => US
[patent_app_date] => 2012-08-10
[patent_effective_date] => 0000-00-00
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[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13572504
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/572504 | Pitch control valve in an aircraft store ejector system | Aug 9, 2012 | Issued |
Array
(
[id] => 9303596
[patent_doc_number] => 20140042270
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2014-02-13
[patent_title] => 'STORAGE SYSTEM FOR STORING STATIC ELECTRICAL ENERGY IN ATMOSPHERE'
[patent_app_type] => utility
[patent_app_number] => 13/571105
[patent_app_country] => US
[patent_app_date] => 2012-08-09
[patent_effective_date] => 0000-00-00
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[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13571105
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/571105 | STORAGE SYSTEM FOR STORING STATIC ELECTRICAL ENERGY IN ATMOSPHERE | Aug 8, 2012 | Abandoned |