Search

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 numberTitle of the applicationFiling DateStatus
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 [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] => 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 [patent_figures_cnt] => 10 [patent_no_of_words] => 3617 [patent_no_of_claims] => 23 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 156 [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 [patent_figures_cnt] => 9 [patent_no_of_words] => 8999 [patent_no_of_claims] => 11 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 590 [patent_maintenance] => 1 [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 [patent_figures_cnt] => 5 [patent_no_of_words] => 4379 [patent_no_of_claims] => 11 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 143 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [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 [patent_figures_cnt] => 6 [patent_no_of_words] => 4639 [patent_no_of_claims] => 9 [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] => 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 [patent_drawing_sheets_cnt] => 4 [patent_figures_cnt] => 9 [patent_no_of_words] => 4781 [patent_no_of_claims] => 19 [patent_no_of_ind_claims] => 2 [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] => 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 [patent_drawing_sheets_cnt] => 5 [patent_figures_cnt] => 5 [patent_no_of_words] => 4653 [patent_no_of_claims] => 13 [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] => 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 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 14 [patent_figures_cnt] => 28 [patent_no_of_words] => 10389 [patent_no_of_claims] => 18 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 134 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [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 [patent_app_date] => 2014-12-05 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 9 [patent_figures_cnt] => 18 [patent_no_of_words] => 6243 [patent_no_of_claims] => 18 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 145 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [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 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 7 [patent_figures_cnt] => 9 [patent_no_of_words] => 6431 [patent_no_of_claims] => 19 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 93 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [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 [patent_app_date] => 2014-12-02 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 25 [patent_figures_cnt] => 37 [patent_no_of_words] => 17604 [patent_no_of_claims] => 21 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 262 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [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
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