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] => 11922380
[patent_doc_number] => 09789950
[patent_country] => US
[patent_kind] => B1
[patent_issue_date] => 2017-10-17
[patent_title] => 'Unmanned aerial vehicle (UAV) with multi-part foldable wings'
[patent_app_type] => utility
[patent_app_number] => 14/260889
[patent_app_country] => US
[patent_app_date] => 2014-04-24
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 10
[patent_figures_cnt] => 10
[patent_no_of_words] => 3039
[patent_no_of_claims] => 11
[patent_no_of_ind_claims] => 2
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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] => 14260889
[rel_patent_id] =>[rel_patent_doc_number] =>) 14/260889 | Unmanned aerial vehicle (UAV) with multi-part foldable wings | Apr 23, 2014 | Issued |
Array
(
[id] => 10909158
[patent_doc_number] => 20140312173
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2014-10-23
[patent_title] => 'DOUBLE CABIN ATTENDANT SEAT'
[patent_app_type] => utility
[patent_app_number] => 14/258580
[patent_app_country] => US
[patent_app_date] => 2014-04-22
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 7
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[patent_no_of_words] => 3846
[patent_no_of_claims] => 11
[patent_no_of_ind_claims] => 3
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[patent_current_assignee] =>[type] => publication
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14258580
[rel_patent_id] =>[rel_patent_doc_number] =>) 14/258580 | Double cabin attendant seat | Apr 21, 2014 | Issued |
Array
(
[id] => 11357112
[patent_doc_number] => 09533754
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2017-01-03
[patent_title] => 'Wing aerial refueling system'
[patent_app_type] => utility
[patent_app_number] => 14/256935
[patent_app_country] => US
[patent_app_date] => 2014-04-19
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 6
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[patent_no_of_words] => 3002
[patent_no_of_claims] => 26
[patent_no_of_ind_claims] => 2
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[patent_maintenance] => 1
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[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14256935
[rel_patent_id] =>[rel_patent_doc_number] =>) 14/256935 | Wing aerial refueling system | Apr 18, 2014 | Issued |
Array
(
[id] => 10964478
[patent_doc_number] => 20140367509
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2014-12-18
[patent_title] => 'AIRCRAFT WITH FREEWHEELING ENGINE'
[patent_app_type] => utility
[patent_app_number] => 14/251850
[patent_app_country] => US
[patent_app_date] => 2014-04-14
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 10
[patent_figures_cnt] => 10
[patent_no_of_words] => 11372
[patent_no_of_claims] => 21
[patent_no_of_ind_claims] => 2
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[patent_current_assignee] =>[type] => publication
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14251850
[rel_patent_id] =>[rel_patent_doc_number] =>) 14/251850 | AIRCRAFT WITH FREEWHEELING ENGINE | Apr 13, 2014 | Abandoned |
Array
(
[id] => 11304465
[patent_doc_number] => 09511850
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2016-12-06
[patent_title] => 'Wing tip device for an aircraft wing'
[patent_app_type] => utility
[patent_app_number] => 14/251601
[patent_app_country] => US
[patent_app_date] => 2014-04-12
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 10
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[patent_no_of_words] => 8498
[patent_no_of_claims] => 24
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[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14251601
[rel_patent_id] =>[rel_patent_doc_number] =>) 14/251601 | Wing tip device for an aircraft wing | Apr 11, 2014 | Issued |
Array
(
[id] => 10964494
[patent_doc_number] => 20140367525
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2014-12-18
[patent_title] => 'AIRCRAFT USING TURBO-ELECTRIC HYBRID PROPULSION SYSTEM'
[patent_app_type] => utility
[patent_app_number] => 14/247608
[patent_app_country] => US
[patent_app_date] => 2014-04-08
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 9
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[patent_no_of_words] => 5325
[patent_no_of_claims] => 18
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[patent_current_assignee] =>[type] => publication
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14247608
[rel_patent_id] =>[rel_patent_doc_number] =>) 14/247608 | Aircraft using turbo-electric hybrid propulsion system | Apr 7, 2014 | Issued |
Array
(
[id] => 12106035
[patent_doc_number] => 09862505
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2018-01-09
[patent_title] => 'Techniques for emplacing an unmanned aerial vehicle launcher prior to launching an unmanned aerial vehicle'
[patent_app_type] => utility
[patent_app_number] => 14/225751
[patent_app_country] => US
[patent_app_date] => 2014-03-26
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 8
[patent_figures_cnt] => 8
[patent_no_of_words] => 5515
[patent_no_of_claims] => 19
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 288
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14225751
[rel_patent_id] =>[rel_patent_doc_number] =>) 14/225751 | Techniques for emplacing an unmanned aerial vehicle launcher prior to launching an unmanned aerial vehicle | Mar 25, 2014 | Issued |
Array
(
[id] => 13153403
[patent_doc_number] => 10093411
[patent_country] => US
[patent_kind] => B1
[patent_issue_date] => 2018-10-09
[patent_title] => Apparatus and method for reducing a sonic boom signature
[patent_app_type] => utility
[patent_app_number] => 14/217547
[patent_app_country] => US
[patent_app_date] => 2014-03-18
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 9
[patent_figures_cnt] => 12
[patent_no_of_words] => 4529
[patent_no_of_claims] => 11
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 100
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[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14217547
[rel_patent_id] =>[rel_patent_doc_number] =>) 14/217547 | Apparatus and method for reducing a sonic boom signature | Mar 17, 2014 | Issued |
Array
(
[id] => 11736826
[patent_doc_number] => 09701399
[patent_country] => US
[patent_kind] => B1
[patent_issue_date] => 2017-07-11
[patent_title] => 'Parasitic drag induced boundary layer reduction system and method'
[patent_app_type] => utility
[patent_app_number] => 14/218819
[patent_app_country] => US
[patent_app_date] => 2014-03-18
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 10
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[patent_no_of_words] => 8091
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[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14218819
[rel_patent_id] =>[rel_patent_doc_number] =>) 14/218819 | Parasitic drag induced boundary layer reduction system and method | Mar 17, 2014 | Issued |
Array
(
[id] => 13647357
[patent_doc_number] => 09849980
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2017-12-26
[patent_title] => Personal propulsion devices with improved balance
[patent_app_type] => utility
[patent_app_number] => 14/210102
[patent_app_country] => US
[patent_app_date] => 2014-03-13
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 3
[patent_no_of_words] => 2775
[patent_no_of_claims] => 19
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[patent_words_short_claim] => 115
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[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14210102
[rel_patent_id] =>[rel_patent_doc_number] =>) 14/210102 | Personal propulsion devices with improved balance | Mar 12, 2014 | Issued |
Array
(
[id] => 9728142
[patent_doc_number] => 20140263848
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2014-09-18
[patent_title] => 'REVERSIBLE FLIGHT CONTROL SYSTEMS'
[patent_app_type] => utility
[patent_app_number] => 14/195419
[patent_app_country] => US
[patent_app_date] => 2014-03-03
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 9
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[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14195419
[rel_patent_id] =>[rel_patent_doc_number] =>) 14/195419 | Reversible flight control systems | Mar 2, 2014 | Issued |
Array
(
[id] => 9969627
[patent_doc_number] => 09016624
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2015-04-28
[patent_title] => 'Aircraft cabin bin retrofit'
[patent_app_type] => utility
[patent_app_number] => 14/189872
[patent_app_country] => US
[patent_app_date] => 2014-02-25
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
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[patent_no_of_words] => 3883
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[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14189872
[rel_patent_id] =>[rel_patent_doc_number] =>) 14/189872 | Aircraft cabin bin retrofit | Feb 24, 2014 | Issued |
Array
(
[id] => 11763647
[patent_doc_number] => 09372055
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2016-06-21
[patent_title] => 'Passive control fin stops for air launched boosted (two stage) high speed vehicles'
[patent_app_type] => utility
[patent_app_number] => 14/170143
[patent_app_country] => US
[patent_app_date] => 2014-01-31
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 10
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[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14170143
[rel_patent_id] =>[rel_patent_doc_number] =>) 14/170143 | Passive control fin stops for air launched boosted (two stage) high speed vehicles | Jan 30, 2014 | Issued |
Array
(
[id] => 10541036
[patent_doc_number] => 09266143
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2016-02-23
[patent_title] => 'Fireproof bulkhead of a highly porous structure with intumescent coating and method for its production'
[patent_app_type] => utility
[patent_app_number] => 14/163673
[patent_app_country] => US
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[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14163673
[rel_patent_id] =>[rel_patent_doc_number] =>) 14/163673 | Fireproof bulkhead of a highly porous structure with intumescent coating and method for its production | Jan 23, 2014 | Issued |
Array
(
[id] => 9634543
[patent_doc_number] => 20140212652
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2014-07-31
[patent_title] => 'FIREPROOF BULKHEAD OF A HIGHLY POROUS STRUCTURE WITH INTUMESCENT COATING AND METHOD FOR ITS PRODUCTION'
[patent_app_type] => utility
[patent_app_number] => 14/163664
[patent_app_country] => US
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[patent_effective_date] => 0000-00-00
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[rel_patent_id] =>[rel_patent_doc_number] =>) 14/163664 | Fireproof bulkhead of a highly porous structure with intumescent coating and method for its production | Jan 23, 2014 | Issued |
Array
(
[id] => 10929612
[patent_doc_number] => 20140332633
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2014-11-13
[patent_title] => 'EMERGENCY COLLECTIVE ACTUATOR AND METHOD FOR A HELICOPTER'
[patent_app_type] => utility
[patent_app_number] => 14/161877
[patent_app_country] => US
[patent_app_date] => 2014-01-23
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[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14161877
[rel_patent_id] =>[rel_patent_doc_number] =>) 14/161877 | Emergency collective actuator and method for a helicopter | Jan 22, 2014 | Issued |
Array
(
[id] => 10111029
[patent_doc_number] => 09146438
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2015-09-29
[patent_title] => 'Self-powered dimmable windows with integrated controls'
[patent_app_type] => utility
[patent_app_number] => 14/159267
[patent_app_country] => US
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[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14159267
[rel_patent_id] =>[rel_patent_doc_number] =>) 14/159267 | Self-powered dimmable windows with integrated controls | Jan 19, 2014 | Issued |
Array
(
[id] => 10482929
[patent_doc_number] => 20150367947
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2015-12-24
[patent_title] => 'AIRCRAFT PROPULSION ASSEMBLY COMPRISING AT LEAST ONE BRUSH SEAL RESISTANT TO HIGH-TEMPERATURE'
[patent_app_type] => utility
[patent_app_number] => 14/762085
[patent_app_country] => US
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[rel_patent_id] =>[rel_patent_doc_number] =>) 14/762085 | AIRCRAFT PROPULSION ASSEMBLY COMPRISING AT LEAST ONE BRUSH SEAL RESISTANT TO HIGH-TEMPERATURE | Jan 19, 2014 | Abandoned |
Array
(
[id] => 9565587
[patent_doc_number] => 20140183301
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2014-07-03
[patent_title] => 'AIRCRAFT VENTRAL FAIRING WITH AN IMPROVED STORAGE CAPACITY'
[patent_app_type] => utility
[patent_app_number] => 14/140665
[patent_app_country] => US
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[rel_patent_id] =>[rel_patent_doc_number] =>) 14/140665 | Aircraft ventral fairing with an improved storage capacity | Dec 25, 2013 | Issued |
Array
(
[id] => 10298511
[patent_doc_number] => 20150183511
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2015-07-02
[patent_title] => 'CONTROL PANEL INTEGRATION INTO AIRCRAFT THROTTLE CONTROL'
[patent_app_type] => utility
[patent_app_number] => 14/141150
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[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14141150
[rel_patent_id] =>[rel_patent_doc_number] =>) 14/141150 | CONTROL PANEL INTEGRATION INTO AIRCRAFT THROTTLE CONTROL | Dec 25, 2013 | Abandoned |