
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] => 8992917
[patent_doc_number] => 08516789
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2013-08-27
[patent_title] => 'Gas turbine engine with aft core driven fan section'
[patent_app_type] => utility
[patent_app_number] => 13/190595
[patent_app_country] => US
[patent_app_date] => 2011-07-26
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 6
[patent_no_of_words] => 2571
[patent_no_of_claims] => 17
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 117
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13190595
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/190595 | Gas turbine engine with aft core driven fan section | Jul 25, 2011 | Issued |
Array
(
[id] => 8413094
[patent_doc_number] => 20120240594
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2012-09-27
[patent_title] => 'METHOD AND APPARATUS FOR PROTECTING AIRCRAFT ENGINES AGAINST ICING'
[patent_app_type] => utility
[patent_app_number] => 13/190965
[patent_app_country] => US
[patent_app_date] => 2011-07-26
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 7
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[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13190965
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/190965 | METHOD AND APPARATUS FOR PROTECTING AIRCRAFT ENGINES AGAINST ICING | Jul 25, 2011 | Abandoned |
Array
(
[id] => 8614275
[patent_doc_number] => 20130019587
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2013-01-24
[patent_title] => 'THRUSTER DEVICES AND METHODS OF MAKING THRUSTER DEVICES FOR USE WITH THRUST VECTOR CONTROL SYSTEMS'
[patent_app_type] => utility
[patent_app_number] => 13/187752
[patent_app_country] => US
[patent_app_date] => 2011-07-21
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
[patent_figures_cnt] => 5
[patent_no_of_words] => 3989
[patent_no_of_claims] => 21
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[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13187752
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/187752 | THRUSTER DEVICES AND METHODS OF MAKING THRUSTER DEVICES FOR USE WITH THRUST VECTOR CONTROL SYSTEMS | Jul 20, 2011 | Abandoned |
Array
(
[id] => 9993780
[patent_doc_number] => 09038361
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2015-05-26
[patent_title] => 'Combustion controller'
[patent_app_type] => utility
[patent_app_number] => 13/180920
[patent_app_country] => US
[patent_app_date] => 2011-07-12
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 20
[patent_figures_cnt] => 20
[patent_no_of_words] => 6059
[patent_no_of_claims] => 21
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[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13180920
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/180920 | Combustion controller | Jul 11, 2011 | Issued |
Array
(
[id] => 9759948
[patent_doc_number] => 08844259
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2014-09-30
[patent_title] => 'Flashback protector'
[patent_app_type] => utility
[patent_app_number] => 13/181061
[patent_app_country] => US
[patent_app_date] => 2011-07-12
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 10
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[patent_no_of_words] => 3487
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[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13181061
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/181061 | Flashback protector | Jul 11, 2011 | Issued |
Array
(
[id] => 9935103
[patent_doc_number] => 08984895
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2015-03-24
[patent_title] => 'Metallic ceramic spool for a gas turbine engine'
[patent_app_type] => utility
[patent_app_number] => 13/180275
[patent_app_country] => US
[patent_app_date] => 2011-07-11
[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] => 13180275
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/180275 | Metallic ceramic spool for a gas turbine engine | Jul 10, 2011 | Issued |
Array
(
[id] => 8602862
[patent_doc_number] => 20130008174
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2013-01-10
[patent_title] => 'METHOD AND CONTROLLER FOR DETECTING ICE'
[patent_app_type] => utility
[patent_app_number] => 13/178818
[patent_app_country] => US
[patent_app_date] => 2011-07-08
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
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[patent_no_of_words] => 2390
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[patent_current_assignee] =>[type] => publication
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13178818
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/178818 | Method and controller for detecting ice | Jul 7, 2011 | Issued |
Array
(
[id] => 10895925
[patent_doc_number] => 08919125
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2014-12-30
[patent_title] => 'Apparatus and systems relating to fuel injectors and fuel passages in gas turbine engines'
[patent_app_type] => utility
[patent_app_number] => 13/176784
[patent_app_country] => US
[patent_app_date] => 2011-07-06
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 4
[patent_no_of_words] => 4619
[patent_no_of_claims] => 19
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[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13176784
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/176784 | Apparatus and systems relating to fuel injectors and fuel passages in gas turbine engines | Jul 5, 2011 | Issued |
Array
(
[id] => 8581499
[patent_doc_number] => 20130000321
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2013-01-03
[patent_title] => 'GAS TURBINE INLET HEATING SYSTEM'
[patent_app_type] => utility
[patent_app_number] => 13/175006
[patent_app_country] => US
[patent_app_date] => 2011-07-01
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 2
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[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13175006
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/175006 | Gas turbine inlet heating system | Jun 30, 2011 | Issued |
Array
(
[id] => 9975478
[patent_doc_number] => 09021778
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2015-05-05
[patent_title] => 'Differential gear system with carrier drive'
[patent_app_type] => utility
[patent_app_number] => 13/170574
[patent_app_country] => US
[patent_app_date] => 2011-06-28
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
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[patent_no_of_words] => 3357
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[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13170574
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/170574 | Differential gear system with carrier drive | Jun 27, 2011 | Issued |
Array
(
[id] => 8992921
[patent_doc_number] => 08516793
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2013-08-27
[patent_title] => 'Gas turbine engine systems and related methods involving vane-blade count ratios greater than unity'
[patent_app_type] => utility
[patent_app_number] => 13/163304
[patent_app_country] => US
[patent_app_date] => 2011-06-17
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
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[patent_no_of_words] => 2182
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[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13163304
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/163304 | Gas turbine engine systems and related methods involving vane-blade count ratios greater than unity | Jun 16, 2011 | Issued |
Array
(
[id] => 10622203
[patent_doc_number] => 09341141
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2016-05-17
[patent_title] => 'Variable jet engine outlet with a mainly circle sector-formed cross section'
[patent_app_type] => utility
[patent_app_number] => 14/123379
[patent_app_country] => US
[patent_app_date] => 2011-06-17
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 14
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[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14123379
[rel_patent_id] =>[rel_patent_doc_number] =>) 14/123379 | Variable jet engine outlet with a mainly circle sector-formed cross section | Jun 16, 2011 | Issued |
Array
(
[id] => 10842339
[patent_doc_number] => 08869501
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2014-10-28
[patent_title] => 'Clamping assembly'
[patent_app_type] => utility
[patent_app_number] => 13/159932
[patent_app_country] => US
[patent_app_date] => 2011-06-14
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 1
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[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13159932
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/159932 | Clamping assembly | Jun 13, 2011 | Issued |
Array
(
[id] => 9619215
[patent_doc_number] => 08789376
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2014-07-29
[patent_title] => 'Flade duct turbine cooling and power and thermal management'
[patent_app_type] => utility
[patent_app_number] => 13/117607
[patent_app_country] => US
[patent_app_date] => 2011-05-27
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[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13117607
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/117607 | Flade duct turbine cooling and power and thermal management | May 26, 2011 | Issued |
Array
(
[id] => 8498364
[patent_doc_number] => 20120297773
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2012-11-29
[patent_title] => 'GASIFIER POWER PLANT AND MANAGEMENT OF WASTES'
[patent_app_type] => utility
[patent_app_number] => 13/115902
[patent_app_country] => US
[patent_app_date] => 2011-05-25
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[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13115902
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/115902 | Gasifier power plant and management of wastes | May 24, 2011 | Issued |
Array
(
[id] => 8844260
[patent_doc_number] => 08453428
[patent_country] => US
[patent_kind] => B1
[patent_issue_date] => 2013-06-04
[patent_title] => 'Modular engine units including turbine engine with combustion mediating hub'
[patent_app_type] => utility
[patent_app_number] => 13/102355
[patent_app_country] => US
[patent_app_date] => 2011-05-06
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[rel_patent_id] =>[rel_patent_doc_number] =>) 13/102355 | Modular engine units including turbine engine with combustion mediating hub | May 5, 2011 | Issued |
Array
(
[id] => 6041211
[patent_doc_number] => 20110203288
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2011-08-25
[patent_title] => 'Jet Engine Exhaust Nozzle Flow Effector'
[patent_app_type] => utility
[patent_app_number] => 13/096305
[patent_app_country] => US
[patent_app_date] => 2011-04-28
[patent_effective_date] => 0000-00-00
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[pdf_file] => publications/A1/0203/20110203288.pdf
[firstpage_image] =>[orig_patent_app_number] => 13096305
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/096305 | Jet engine exhaust nozzle flow effector | Apr 27, 2011 | Issued |
Array
(
[id] => 6158969
[patent_doc_number] => 20110192171
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2011-08-11
[patent_title] => 'TRANSITION SUPPORT SYSTEM FOR COMBUSTION TRANSITION DUCTS FOR TURBINE ENGINES'
[patent_app_type] => utility
[patent_app_number] => 13/087534
[patent_app_country] => US
[patent_app_date] => 2011-04-15
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[rel_patent_id] =>[rel_patent_doc_number] =>) 13/087534 | TRANSITION SUPPORT SYSTEM FOR COMBUSTION TRANSITION DUCTS FOR TURBINE ENGINES | Apr 14, 2011 | Abandoned |
Array
(
[id] => 9987547
[patent_doc_number] => 09032739
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[patent_issue_date] => 2015-05-19
[patent_title] => 'Load limited actuator'
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[rel_patent_id] =>[rel_patent_doc_number] =>) 13/083820 | Load limited actuator | Apr 10, 2011 | Issued |
Array
(
[id] => 10848811
[patent_doc_number] => 08875485
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[patent_kind] => B2
[patent_issue_date] => 2014-11-04
[patent_title] => 'Micro-cathode thruster and a method of increasing thrust output for a micro-cathode thruster'
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[rel_patent_id] =>[rel_patent_doc_number] =>) 13/081106 | Micro-cathode thruster and a method of increasing thrust output for a micro-cathode thruster | Apr 5, 2011 | Issued |