
Minh D. Dao
Examiner (ID: 15237)
| Most Active Art Unit | 2618 |
| Art Unit(s) | 2682, 2618, 2648 |
| Total Applications | 943 |
| Issued Applications | 797 |
| Pending Applications | 30 |
| Abandoned Applications | 121 |
Applications
| Application number | Title of the application | Filing Date | Status |
|---|---|---|---|
Array
(
[id] => 8425239
[patent_doc_number] => 20120247114
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2012-10-04
[patent_title] => 'Water Cooling System For Intercooled Turbines'
[patent_app_type] => utility
[patent_app_number] => 13/076200
[patent_app_country] => US
[patent_app_date] => 2011-03-30
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 15
[patent_figures_cnt] => 15
[patent_no_of_words] => 5909
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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] => 13076200
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/076200 | Water Cooling System For Intercooled Turbines | Mar 29, 2011 | Abandoned |
Array
(
[id] => 8414061
[patent_doc_number] => 20120241561
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2012-09-27
[patent_title] => 'METHOD AND APPARATUS FOR PROTECTING AIRCRAFT AND AIRCRAFT ENGINES AGAINST ICING'
[patent_app_type] => utility
[patent_app_number] => 13/076038
[patent_app_country] => US
[patent_app_date] => 2011-03-30
[patent_effective_date] => 0000-00-00
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[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13076038
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/076038 | METHOD AND APPARATUS FOR PROTECTING AIRCRAFT AND AIRCRAFT ENGINES AGAINST ICING | Mar 29, 2011 | Abandoned |
| 13/071060 | APPARATUS FOR PROTECTING AIRCRAFT ENGINES AGAINST ICING | Mar 23, 2011 | Abandoned |
Array
(
[id] => 10868278
[patent_doc_number] => 08893466
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2014-11-25
[patent_title] => 'Dual pump fuel flow system for a gas turbine engine and method of controlling'
[patent_app_type] => utility
[patent_app_number] => 13/051091
[patent_app_country] => US
[patent_app_date] => 2011-03-18
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[patent_drawing_sheets_cnt] => 3
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[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13051091
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/051091 | Dual pump fuel flow system for a gas turbine engine and method of controlling | Mar 17, 2011 | Issued |
Array
(
[id] => 6009345
[patent_doc_number] => 20110219742
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2011-09-15
[patent_title] => 'SUPERSONIC COMBUSTOR ROCKET NOZZLE'
[patent_app_type] => utility
[patent_app_number] => 13/047663
[patent_app_country] => US
[patent_app_date] => 2011-03-14
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 6
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[rel_patent_id] =>[rel_patent_doc_number] =>) 13/047663 | SUPERSONIC COMBUSTOR ROCKET NOZZLE | Mar 13, 2011 | Abandoned |
Array
(
[id] => 9879905
[patent_doc_number] => RE045396
[patent_country] => US
[patent_kind] => E1
[patent_issue_date] => 2015-03-03
[patent_title] => 'Wave rotor apparatus'
[patent_app_type] => reissue
[patent_app_number] => 13/023568
[patent_app_country] => US
[patent_app_date] => 2011-03-01
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[patent_drawing_sheets_cnt] => 26
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[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13023568
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/023568 | Wave rotor apparatus | Feb 28, 2011 | Issued |
Array
(
[id] => 7700642
[patent_doc_number] => 20110225948
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2011-09-22
[patent_title] => 'APPARATUS FOR HIGH-FREQUENCY ELECTROMAGNETIC INITIATION OF A COMBUSTION PROCESS'
[patent_app_type] => utility
[patent_app_number] => 13/036040
[patent_app_country] => US
[patent_app_date] => 2011-02-28
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 6
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[pdf_file] => publications/A1/0225/20110225948.pdf
[firstpage_image] =>[orig_patent_app_number] => 13036040
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/036040 | APPARATUS FOR HIGH-FREQUENCY ELECTROMAGNETIC INITIATION OF A COMBUSTION PROCESS | Feb 27, 2011 | Abandoned |
Array
(
[id] => 8332151
[patent_doc_number] => 20120198854
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2012-08-09
[patent_title] => 'RESONATOR SYSTEM WITH ENHANCED COMBUSTOR LINER COOLING'
[patent_app_type] => utility
[patent_app_number] => 13/023710
[patent_app_country] => US
[patent_app_date] => 2011-02-09
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 8
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[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13023710
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/023710 | Resonator system with enhanced combustor liner cooling | Feb 8, 2011 | Issued |
Array
(
[id] => 6109820
[patent_doc_number] => 20110188989
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2011-08-04
[patent_title] => 'EXHAUST EDUCTOR SYSTEM WITH A RECIRCULATION BAFFLE'
[patent_app_type] => utility
[patent_app_number] => 13/018931
[patent_app_country] => US
[patent_app_date] => 2011-02-01
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
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[patent_no_of_words] => 2039
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[pdf_file] => publications/A1/0188/20110188989.pdf
[firstpage_image] =>[orig_patent_app_number] => 13018931
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/018931 | Exhaust eductor system with a recirculation baffle | Jan 31, 2011 | Issued |
Array
(
[id] => 9975515
[patent_doc_number] => 09021815
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2015-05-05
[patent_title] => 'Gas turbine combustion device'
[patent_app_type] => utility
[patent_app_number] => 13/015910
[patent_app_country] => US
[patent_app_date] => 2011-01-28
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[rel_patent_id] =>[rel_patent_doc_number] =>) 13/015910 | Gas turbine combustion device | Jan 27, 2011 | Issued |
Array
(
[id] => 7582974
[patent_doc_number] => 20110277484
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2011-11-17
[patent_title] => 'SYSTEM AND METHOD FOR VENTILATING A TURBINE'
[patent_app_type] => utility
[patent_app_number] => 13/013172
[patent_app_country] => US
[patent_app_date] => 2011-01-25
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 2
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[firstpage_image] =>[orig_patent_app_number] => 13013172
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/013172 | System and method for ventilating a turbine | Jan 24, 2011 | Issued |
Array
(
[id] => 5953947
[patent_doc_number] => 20110179767
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2011-07-28
[patent_title] => 'COOLING DEVICE FOR AIRCRAFT PROPELLER'
[patent_app_type] => utility
[patent_app_number] => 13/013319
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[rel_patent_id] =>[rel_patent_doc_number] =>) 13/013319 | COOLING DEVICE FOR AIRCRAFT PROPELLER | Jan 24, 2011 | Abandoned |
Array
(
[id] => 8309239
[patent_doc_number] => 20120186262
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[patent_kind] => A1
[patent_issue_date] => 2012-07-26
[patent_title] => 'GAS TURBINE COMBUSTOR AND METHOD FOR OPERATING'
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[rel_patent_id] =>[rel_patent_doc_number] =>) 13/012212 | Axial stage combustor for gas turbine engines | Jan 23, 2011 | Issued |
Array
(
[id] => 10835860
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[patent_issue_date] => 2014-10-21
[patent_title] => 'Combustor with fuel staggering for flame holding mitigation'
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Array
(
[id] => 8273700
[patent_doc_number] => 20120167576
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[patent_kind] => A1
[patent_issue_date] => 2012-07-05
[patent_title] => 'METHOD AND SYSTEM FOR POWERING A VEHICLE'
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[rel_patent_id] =>[rel_patent_doc_number] =>) 12/981044 | System for powering a vehicle | Dec 28, 2010 | Issued |
Array
(
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Array
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Array
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Array
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Array
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