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] => 11004422
[patent_doc_number] => 20160201371
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2016-07-14
[patent_title] => 'QUICK RELEASE HINGE'
[patent_app_type] => utility
[patent_app_number] => 14/592593
[patent_app_country] => US
[patent_app_date] => 2015-01-08
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 9
[patent_figures_cnt] => 9
[patent_no_of_words] => 2138
[patent_no_of_claims] => 15
[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] => 14592593
[rel_patent_id] =>[rel_patent_doc_number] =>) 14/592593 | Quick release hinge | Jan 7, 2015 | Issued |
Array
(
[id] => 11331493
[patent_doc_number] => 09522728
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2016-12-20
[patent_title] => 'Space-maximizing clutch arrangement for vehicle drive wheel'
[patent_app_type] => utility
[patent_app_number] => 14/590898
[patent_app_country] => US
[patent_app_date] => 2015-01-06
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 1
[patent_figures_cnt] => 2
[patent_no_of_words] => 3342
[patent_no_of_claims] => 12
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 133
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14590898
[rel_patent_id] =>[rel_patent_doc_number] =>) 14/590898 | Space-maximizing clutch arrangement for vehicle drive wheel | Jan 5, 2015 | Issued |
Array
(
[id] => 11420996
[patent_doc_number] => 20170029139
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2017-02-02
[patent_title] => 'Attitude Control for Agile Satellite Applications'
[patent_app_type] => utility
[patent_app_number] => 15/107419
[patent_app_country] => US
[patent_app_date] => 2014-12-23
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 12
[patent_figures_cnt] => 12
[patent_no_of_words] => 8229
[patent_no_of_claims] => 12
[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] =>[firstpage_image] =>[orig_patent_app_number] => 15107419
[rel_patent_id] =>[rel_patent_doc_number] =>) 15/107419 | Attitude control for agile satellite applications | Dec 22, 2014 | Issued |
Array
(
[id] => 10399063
[patent_doc_number] => 20150284071
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2015-10-08
[patent_title] => 'CONTRA-ROTATING OPEN ROTOR DISTRIBUTED PROPULSION SYSTEM'
[patent_app_type] => utility
[patent_app_number] => 14/578975
[patent_app_country] => US
[patent_app_date] => 2014-12-22
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 11
[patent_figures_cnt] => 11
[patent_no_of_words] => 4680
[patent_no_of_claims] => 20
[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] =>[firstpage_image] =>[orig_patent_app_number] => 14578975
[rel_patent_id] =>[rel_patent_doc_number] =>) 14/578975 | Contra-rotating open rotor distributed propulsion system | Dec 21, 2014 | Issued |
Array
(
[id] => 11698480
[patent_doc_number] => 09688381
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2017-06-27
[patent_title] => 'Subfloor structure with an integral hull for a rotary wing aircraft'
[patent_app_type] => utility
[patent_app_number] => 14/578653
[patent_app_country] => US
[patent_app_date] => 2014-12-22
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 7
[patent_no_of_words] => 6827
[patent_no_of_claims] => 20
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 393
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14578653
[rel_patent_id] =>[rel_patent_doc_number] =>) 14/578653 | Subfloor structure with an integral hull for a rotary wing aircraft | Dec 21, 2014 | Issued |
Array
(
[id] => 11114557
[patent_doc_number] => 20160311529
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2016-10-27
[patent_title] => 'Modular Electric VTOL Aircraft'
[patent_app_type] => utility
[patent_app_number] => 15/104614
[patent_app_country] => US
[patent_app_date] => 2014-12-17
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 7
[patent_figures_cnt] => 7
[patent_no_of_words] => 8053
[patent_no_of_claims] => 8
[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] =>[firstpage_image] =>[orig_patent_app_number] => 15104614
[rel_patent_id] =>[rel_patent_doc_number] =>) 15/104614 | Modular Electric VTOL Aircraft | Dec 16, 2014 | Abandoned |
Array
(
[id] => 10281194
[patent_doc_number] => 20150166192
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2015-06-18
[patent_title] => 'ASSEMBLY FOR AN AIRCRAFT, COMPRISING AN ENGINE ATTACHMENT BODY PARTIALLY PRODUCED IN ONE PIECE WITH AN INTERNAL STIFFENING RIB OF AN ATTACHMENT PYLON BOX SECTION'
[patent_app_type] => utility
[patent_app_number] => 14/571772
[patent_app_country] => US
[patent_app_date] => 2014-12-16
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 6
[patent_figures_cnt] => 6
[patent_no_of_words] => 4754
[patent_no_of_claims] => 15
[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] =>[firstpage_image] =>[orig_patent_app_number] => 14571772
[rel_patent_id] =>[rel_patent_doc_number] =>) 14/571772 | Assembly for an aircraft, comprising an engine attachment body partially produced in one piece with an internal stiffening rib of an attachment pylon box section | Dec 15, 2014 | Issued |
Array
(
[id] => 15396853
[patent_doc_number] => 10539077
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2020-01-21
[patent_title] => Device for draining liquids for an aircraft engine
[patent_app_type] => utility
[patent_app_number] => 15/104462
[patent_app_country] => US
[patent_app_date] => 2014-12-15
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 10
[patent_no_of_words] => 4660
[patent_no_of_claims] => 19
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 109
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 15104462
[rel_patent_id] =>[rel_patent_doc_number] =>) 15/104462 | Device for draining liquids for an aircraft engine | Dec 14, 2014 | Issued |
Array
(
[id] => 10821634
[patent_doc_number] => 20160167798
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2016-06-16
[patent_title] => 'VARIABLE PITCH MOUNTING FOR AIRCRAFT GAS TURBINE ENGINE'
[patent_app_type] => utility
[patent_app_number] => 14/568555
[patent_app_country] => US
[patent_app_date] => 2014-12-12
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 10
[patent_figures_cnt] => 10
[patent_no_of_words] => 5124
[patent_no_of_claims] => 29
[patent_no_of_ind_claims] => 2
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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] => 14568555
[rel_patent_id] =>[rel_patent_doc_number] =>) 14/568555 | VARIABLE PITCH MOUNTING FOR AIRCRAFT GAS TURBINE ENGINE | Dec 11, 2014 | Abandoned |
Array
(
[id] => 10290253
[patent_doc_number] => 20150175252
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2015-06-25
[patent_title] => 'Method For Producing A Central Wing Box'
[patent_app_type] => utility
[patent_app_number] => 14/566822
[patent_app_country] => US
[patent_app_date] => 2014-12-11
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
[patent_figures_cnt] => 5
[patent_no_of_words] => 2760
[patent_no_of_claims] => 10
[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] => 14566822
[rel_patent_id] =>[rel_patent_doc_number] =>) 14/566822 | Method For Producing A Central Wing Box | Dec 10, 2014 | Abandoned |
Array
(
[id] => 11211706
[patent_doc_number] => 09440732
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2016-09-13
[patent_title] => 'Spring assembly for aircraft components'
[patent_app_type] => utility
[patent_app_number] => 14/568059
[patent_app_country] => US
[patent_app_date] => 2014-12-11
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
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[patent_no_of_words] => 3617
[patent_no_of_claims] => 23
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[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14568059
[rel_patent_id] =>[rel_patent_doc_number] =>) 14/568059 | Spring assembly for aircraft components | Dec 10, 2014 | Issued |
Array
(
[id] => 10649056
[patent_doc_number] => 09365289
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2016-06-14
[patent_title] => 'Rotorcraft fitted with an anti-torque tail rotor that contributes selectively to providing the rotorcraft with lift and with propulsion in translation'
[patent_app_type] => utility
[patent_app_number] => 14/564394
[patent_app_country] => US
[patent_app_date] => 2014-12-09
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
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[patent_no_of_words] => 8999
[patent_no_of_claims] => 11
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[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14564394
[rel_patent_id] =>[rel_patent_doc_number] =>) 14/564394 | Rotorcraft fitted with an anti-torque tail rotor that contributes selectively to providing the rotorcraft with lift and with propulsion in translation | Dec 8, 2014 | Issued |
Array
(
[id] => 11773168
[patent_doc_number] => 09381994
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2016-07-05
[patent_title] => 'Aerofoil portion of an aircraft comprising an attachment support of a connecting device mounted in translation'
[patent_app_type] => utility
[patent_app_number] => 14/565173
[patent_app_country] => US
[patent_app_date] => 2014-12-09
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
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[patent_no_of_words] => 4379
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[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14565173
[rel_patent_id] =>[rel_patent_doc_number] =>) 14/565173 | Aerofoil portion of an aircraft comprising an attachment support of a connecting device mounted in translation | Dec 8, 2014 | Issued |
Array
(
[id] => 10281195
[patent_doc_number] => 20150166191
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2015-06-18
[patent_title] => 'ASSEMBLY COMPRISING AN ARTICULATION SPINDLE SUPPORTED BY A CLEVIS AND IMMOBILIZED IN TRANSLATION BY A BLOCKING DEVICE INTEGRATING A DOUBLE ANTI-ROTATION SYSTEM'
[patent_app_type] => utility
[patent_app_number] => 14/563040
[patent_app_country] => US
[patent_app_date] => 2014-12-08
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 6
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[patent_no_of_words] => 4639
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[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14563040
[rel_patent_id] =>[rel_patent_doc_number] =>) 14/563040 | Assembly comprising an articulation spindle supported by a clevis and immobilized in translation by a blocking device integrating a double anti-rotation system | Dec 7, 2014 | Issued |
Array
(
[id] => 11634786
[patent_doc_number] => 09656742
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2017-05-23
[patent_title] => 'Air ejection device comprising an aerodynamic profile provided with a slot obturating flexible tongue'
[patent_app_type] => utility
[patent_app_number] => 14/561488
[patent_app_country] => US
[patent_app_date] => 2014-12-05
[patent_effective_date] => 0000-00-00
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[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14561488
[rel_patent_id] =>[rel_patent_doc_number] =>) 14/561488 | Air ejection device comprising an aerodynamic profile provided with a slot obturating flexible tongue | Dec 4, 2014 | Issued |
Array
(
[id] => 10273583
[patent_doc_number] => 20150158581
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2015-06-11
[patent_title] => 'FLYING MACHINE'
[patent_app_type] => utility
[patent_app_number] => 14/562155
[patent_app_country] => US
[patent_app_date] => 2014-12-05
[patent_effective_date] => 0000-00-00
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[patent_no_of_words] => 4653
[patent_no_of_claims] => 13
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[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14562155
[rel_patent_id] =>[rel_patent_doc_number] =>) 14/562155 | Flying machine | Dec 4, 2014 | Issued |
Array
(
[id] => 11304470
[patent_doc_number] => 09511856
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2016-12-06
[patent_title] => 'Emergency collective actuator and method for a helicopter'
[patent_app_type] => utility
[patent_app_number] => 14/562479
[patent_app_country] => US
[patent_app_date] => 2014-12-05
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[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14562479
[rel_patent_id] =>[rel_patent_doc_number] =>) 14/562479 | Emergency collective actuator and method for a helicopter | Dec 4, 2014 | Issued |
Array
(
[id] => 11450065
[patent_doc_number] => 09573697
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2017-02-21
[patent_title] => 'Energy recovery of an aircraft'
[patent_app_type] => utility
[patent_app_number] => 14/562244
[patent_app_country] => US
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[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14562244
[rel_patent_id] =>[rel_patent_doc_number] =>) 14/562244 | Energy recovery of an aircraft | Dec 4, 2014 | Issued |
Array
(
[id] => 10614619
[patent_doc_number] => 09334049
[patent_country] => US
[patent_kind] => B1
[patent_issue_date] => 2016-05-10
[patent_title] => 'Single blade rotor system for use in a vertical takeoff and landing (VTOL) aircraft'
[patent_app_type] => utility
[patent_app_number] => 14/559529
[patent_app_country] => US
[patent_app_date] => 2014-12-03
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[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14559529
[rel_patent_id] =>[rel_patent_doc_number] =>) 14/559529 | Single blade rotor system for use in a vertical takeoff and landing (VTOL) aircraft | Dec 2, 2014 | Issued |
Array
(
[id] => 11480142
[patent_doc_number] => 09586667
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2017-03-07
[patent_title] => 'Splice assembly for joining structural components'
[patent_app_type] => utility
[patent_app_number] => 14/557812
[patent_app_country] => US
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[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14557812
[rel_patent_id] =>[rel_patent_doc_number] =>) 14/557812 | Splice assembly for joining structural components | Dec 1, 2014 | Issued |