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] => 9303368
[patent_doc_number] => 20140042042
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2014-02-13
[patent_title] => 'Combined Balloon Shipping Container and Deployment System'
[patent_app_type] => utility
[patent_app_number] => 13/570054
[patent_app_country] => US
[patent_app_date] => 2012-08-08
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 11
[patent_figures_cnt] => 11
[patent_no_of_words] => 11089
[patent_no_of_claims] => 22
[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] => 13570054
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/570054 | Combined balloon shipping container and deployment system | Aug 7, 2012 | Issued |
Array
(
[id] => 9624895
[patent_doc_number] => 08794564
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2014-08-05
[patent_title] => 'Vehicle capable of in-air and on-ground mobility'
[patent_app_type] => utility
[patent_app_number] => 13/565656
[patent_app_country] => US
[patent_app_date] => 2012-08-02
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 16
[patent_figures_cnt] => 17
[patent_no_of_words] => 7631
[patent_no_of_claims] => 20
[patent_no_of_ind_claims] => 3
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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] => 13565656
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/565656 | Vehicle capable of in-air and on-ground mobility | Aug 1, 2012 | Issued |
Array
(
[id] => 10829600
[patent_doc_number] => 08857757
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2014-10-14
[patent_title] => 'Independent blade control system with hydraulic pitch link'
[patent_app_type] => utility
[patent_app_number] => 13/565554
[patent_app_country] => US
[patent_app_date] => 2012-08-02
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 56
[patent_figures_cnt] => 82
[patent_no_of_words] => 18531
[patent_no_of_claims] => 21
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 118
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13565554
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/565554 | Independent blade control system with hydraulic pitch link | Aug 1, 2012 | Issued |
Array
(
[id] => 11767642
[patent_doc_number] => 09376205
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2016-06-28
[patent_title] => 'Radial fluid device with variable phase and amplitude'
[patent_app_type] => utility
[patent_app_number] => 13/565496
[patent_app_country] => US
[patent_app_date] => 2012-08-02
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 56
[patent_figures_cnt] => 82
[patent_no_of_words] => 18519
[patent_no_of_claims] => 36
[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] => 13565496
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/565496 | Radial fluid device with variable phase and amplitude | Aug 1, 2012 | Issued |
Array
(
[id] => 9624897
[patent_doc_number] => 08794566
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2014-08-05
[patent_title] => 'Vehicle capable of stabilizing a payload when in motion'
[patent_app_type] => utility
[patent_app_number] => 13/565654
[patent_app_country] => US
[patent_app_date] => 2012-08-02
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 16
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[patent_no_of_words] => 7710
[patent_no_of_claims] => 20
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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] => 13565654
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/565654 | Vehicle capable of stabilizing a payload when in motion | Aug 1, 2012 | Issued |
Array
(
[id] => 8615122
[patent_doc_number] => 20130020434
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2013-01-24
[patent_title] => 'Condensed Water Decreasing Insulation Package For Thermal And Acoustic Insulation Of A Vehicle Cabin'
[patent_app_type] => utility
[patent_app_number] => 13/564870
[patent_app_country] => US
[patent_app_date] => 2012-08-02
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 10
[patent_figures_cnt] => 10
[patent_no_of_words] => 4334
[patent_no_of_claims] => 12
[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] => 13564870
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/564870 | Condensed water decreasing insulation package for thermal and acoustic insulation of a vehicle cabin | Aug 1, 2012 | Issued |
Array
(
[id] => 9830592
[patent_doc_number] => 08939399
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2015-01-27
[patent_title] => 'System and method of augmenting power in a rotorcraft'
[patent_app_type] => utility
[patent_app_number] => 13/563086
[patent_app_country] => US
[patent_app_date] => 2012-07-31
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 6
[patent_figures_cnt] => 7
[patent_no_of_words] => 4307
[patent_no_of_claims] => 16
[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] => 13563086
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/563086 | System and method of augmenting power in a rotorcraft | Jul 30, 2012 | Issued |
Array
(
[id] => 9277609
[patent_doc_number] => 20140027577
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2014-01-30
[patent_title] => 'IMAGING SATELLITE SYSTEM AND METHOD'
[patent_app_type] => utility
[patent_app_number] => 13/559321
[patent_app_country] => US
[patent_app_date] => 2012-07-26
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 6
[patent_figures_cnt] => 6
[patent_no_of_words] => 2175
[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] => 13559321
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/559321 | IMAGING SATELLITE SYSTEM AND METHOD | Jul 25, 2012 | Abandoned |
Array
(
[id] => 10836415
[patent_doc_number] => 08864081
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2014-10-21
[patent_title] => 'Method and device for an optimal management of the slats, the flaps and the landing gear of an aircraft'
[patent_app_type] => utility
[patent_app_number] => 13/557381
[patent_app_country] => US
[patent_app_date] => 2012-07-25
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 2
[patent_figures_cnt] => 4
[patent_no_of_words] => 6651
[patent_no_of_claims] => 15
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 250
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13557381
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/557381 | Method and device for an optimal management of the slats, the flaps and the landing gear of an aircraft | Jul 24, 2012 | Issued |
Array
(
[id] => 10056973
[patent_doc_number] => 09096317
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2015-08-04
[patent_title] => 'Cargo compartment with robot, aircraft, freight storage device'
[patent_app_type] => utility
[patent_app_number] => 13/556356
[patent_app_country] => US
[patent_app_date] => 2012-07-24
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
[patent_figures_cnt] => 10
[patent_no_of_words] => 7593
[patent_no_of_claims] => 12
[patent_no_of_ind_claims] => 4
[patent_words_short_claim] => 77
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13556356
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/556356 | Cargo compartment with robot, aircraft, freight storage device | Jul 23, 2012 | Issued |
Array
(
[id] => 8615117
[patent_doc_number] => 20130020430
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2013-01-24
[patent_title] => 'Method of Extending and Improving Aircraft Life and Efficiency'
[patent_app_type] => utility
[patent_app_number] => 13/555224
[patent_app_country] => US
[patent_app_date] => 2012-07-23
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 2
[patent_figures_cnt] => 2
[patent_no_of_words] => 4565
[patent_no_of_claims] => 18
[patent_no_of_ind_claims] => 3
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[patent_current_assignee] =>[type] => publication
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13555224
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/555224 | Method of Extending and Improving Aircraft Life and Efficiency | Jul 22, 2012 | Pending |
Array
(
[id] => 9266373
[patent_doc_number] => 20140021289
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2014-01-23
[patent_title] => 'RESETTABLE MISSILE CONTROL FIN LOCK ASSEMBLY'
[patent_app_type] => utility
[patent_app_number] => 13/554032
[patent_app_country] => US
[patent_app_date] => 2012-07-20
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 15
[patent_figures_cnt] => 15
[patent_no_of_words] => 5157
[patent_no_of_claims] => 14
[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] => 13554032
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/554032 | Resettable missile control fin lock assembly | Jul 19, 2012 | Issued |
Array
(
[id] => 9873334
[patent_doc_number] => 08960592
[patent_country] => US
[patent_kind] => B1
[patent_issue_date] => 2015-02-24
[patent_title] => 'VTOL propulsion for aircraft'
[patent_app_type] => utility
[patent_app_number] => 13/553080
[patent_app_country] => US
[patent_app_date] => 2012-07-19
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 21
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[patent_no_of_words] => 15029
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[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13553080
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/553080 | VTOL propulsion for aircraft | Jul 18, 2012 | Issued |
Array
(
[id] => 10829599
[patent_doc_number] => 08857756
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2014-10-14
[patent_title] => 'Elastomeric bearing housing and mating grip for helicopter rotor system'
[patent_app_type] => utility
[patent_app_number] => 13/553317
[patent_app_country] => US
[patent_app_date] => 2012-07-19
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
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[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13553317
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/553317 | Elastomeric bearing housing and mating grip for helicopter rotor system | Jul 18, 2012 | Issued |
Array
(
[id] => 9219994
[patent_doc_number] => 20140014769
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2014-01-16
[patent_title] => 'Balloon Altitude Control Using Density Adjustment and/or Volume Adjustment'
[patent_app_type] => utility
[patent_app_number] => 13/546806
[patent_app_country] => US
[patent_app_date] => 2012-07-11
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 10
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[patent_no_of_words] => 14362
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[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13546806
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/546806 | Balloon altitude control using density adjustment and/or volume adjustment | Jul 10, 2012 | Issued |
Array
(
[id] => 9667729
[patent_doc_number] => 20140231592
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2014-08-21
[patent_title] => 'LEADING EDGE RIB ASSEMBLY'
[patent_app_type] => utility
[patent_app_number] => 14/232247
[patent_app_country] => US
[patent_app_date] => 2012-07-06
[patent_effective_date] => 0000-00-00
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[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14232247
[rel_patent_id] =>[rel_patent_doc_number] =>) 14/232247 | Leading edge rib assembly | Jul 5, 2012 | Issued |
Array
(
[id] => 10639593
[patent_doc_number] => 09357111
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2016-05-31
[patent_title] => 'Casing'
[patent_app_type] => utility
[patent_app_number] => 14/129465
[patent_app_country] => US
[patent_app_date] => 2012-06-30
[patent_effective_date] => 0000-00-00
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[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14129465
[rel_patent_id] =>[rel_patent_doc_number] =>) 14/129465 | Casing | Jun 29, 2012 | Issued |
Array
(
[id] => 9310214
[patent_doc_number] => 08651425
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2014-02-18
[patent_title] => 'Emergency collective actuator and method for a helicopter'
[patent_app_type] => utility
[patent_app_number] => 13/479130
[patent_app_country] => US
[patent_app_date] => 2012-05-23
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[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13479130
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/479130 | Emergency collective actuator and method for a helicopter | May 22, 2012 | Issued |
Array
(
[id] => 10649046
[patent_doc_number] => 09365280
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2016-06-14
[patent_title] => 'Gutter profile and aircraft'
[patent_app_type] => utility
[patent_app_number] => 14/116811
[patent_app_country] => US
[patent_app_date] => 2012-05-14
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[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14116811
[rel_patent_id] =>[rel_patent_doc_number] =>) 14/116811 | Gutter profile and aircraft | May 13, 2012 | Issued |
Array
(
[id] => 11319095
[patent_doc_number] => 09517832
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2016-12-13
[patent_title] => 'Aircraft wing with wing tip device'
[patent_app_type] => utility
[patent_app_number] => 14/128234
[patent_app_country] => US
[patent_app_date] => 2012-04-23
[patent_effective_date] => 0000-00-00
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[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14128234
[rel_patent_id] =>[rel_patent_doc_number] =>) 14/128234 | Aircraft wing with wing tip device | Apr 22, 2012 | Issued |