
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] => 6096619
[patent_doc_number] => 20110162387
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2011-07-07
[patent_title] => 'TURBINE COOLING SYSTEM'
[patent_app_type] => utility
[patent_app_number] => 13/119291
[patent_app_country] => US
[patent_app_date] => 2009-08-19
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 7
[patent_figures_cnt] => 7
[patent_no_of_words] => 5021
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[pdf_file] => publications/A1/0162/20110162387.pdf
[firstpage_image] =>[orig_patent_app_number] => 13119291
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/119291 | Turbine cooling system | Aug 18, 2009 | Issued |
Array
(
[id] => 6445002
[patent_doc_number] => 20100038455
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2010-02-18
[patent_title] => 'LIQUID EJECTOR'
[patent_app_type] => utility
[patent_app_number] => 12/508160
[patent_app_country] => US
[patent_app_date] => 2009-07-23
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
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[pdf_file] => publications/A1/0038/20100038455.pdf
[firstpage_image] =>[orig_patent_app_number] => 12508160
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/508160 | LIQUID EJECTOR | Jul 22, 2009 | Abandoned |
Array
(
[id] => 9373506
[patent_doc_number] => 08677754
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2014-03-25
[patent_title] => 'Fuel supply system for a gas-turbine engine'
[patent_app_type] => utility
[patent_app_number] => 12/501602
[patent_app_country] => US
[patent_app_date] => 2009-07-13
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[rel_patent_id] =>[rel_patent_doc_number] =>) 12/501602 | Fuel supply system for a gas-turbine engine | Jul 12, 2009 | Issued |
Array
(
[id] => 9243294
[patent_doc_number] => 08607569
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2013-12-17
[patent_title] => 'Methods and systems to thermally protect fuel nozzles in combustion systems'
[patent_app_type] => utility
[patent_app_number] => 12/495918
[patent_app_country] => US
[patent_app_date] => 2009-07-01
[patent_effective_date] => 0000-00-00
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[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 12495918
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/495918 | Methods and systems to thermally protect fuel nozzles in combustion systems | Jun 30, 2009 | Issued |
Array
(
[id] => 6322200
[patent_doc_number] => 20100326047
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2010-12-30
[patent_title] => 'SYSTEM AND METHOD FOR ASSEMBLING A THRUST REVERSER FOR A GAS TURBINE PROPULSION SYSTEM'
[patent_app_type] => utility
[patent_app_number] => 12/495248
[patent_app_country] => US
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[pdf_file] => publications/A1/0326/20100326047.pdf
[firstpage_image] =>[orig_patent_app_number] => 12495248
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/495248 | System and method for assembling a thrust reverser for a gas turbine propulsion system | Jun 29, 2009 | Issued |
Array
(
[id] => 5460293
[patent_doc_number] => 20090320493
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2009-12-31
[patent_title] => 'METHOD FOR PRIMARY CONTROL OF A COMBINED GAS AND STEAM TURBINE ARRANGEMENT'
[patent_app_type] => utility
[patent_app_number] => 12/492959
[patent_app_country] => US
[patent_app_date] => 2009-06-26
[patent_effective_date] => 0000-00-00
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[pdf_file] => publications/A1/0320/20090320493.pdf
[firstpage_image] =>[orig_patent_app_number] => 12492959
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/492959 | Method for primary control of a combined gas and steam turbine arrangement | Jun 25, 2009 | Issued |
Array
(
[id] => 9689505
[patent_doc_number] => 08820085
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2014-09-02
[patent_title] => 'Lean fuel intake gas turbine system'
[patent_app_type] => utility
[patent_app_number] => 12/993398
[patent_app_country] => US
[patent_app_date] => 2009-06-10
[patent_effective_date] => 0000-00-00
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[rel_patent_id] =>[rel_patent_doc_number] =>) 12/993398 | Lean fuel intake gas turbine system | Jun 9, 2009 | Issued |
Array
(
[id] => 6345843
[patent_doc_number] => 20100071377
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2010-03-25
[patent_title] => 'Combustor Apparatus for Use in a Gas Turbine Engine'
[patent_app_type] => utility
[patent_app_number] => 12/477397
[patent_app_country] => US
[patent_app_date] => 2009-06-03
[patent_effective_date] => 0000-00-00
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[pdf_file] => publications/A1/0071/20100071377.pdf
[firstpage_image] =>[orig_patent_app_number] => 12477397
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/477397 | Combustor Apparatus for Use in a Gas Turbine Engine | Jun 2, 2009 | Abandoned |
Array
(
[id] => 8627762
[patent_doc_number] => 08359825
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2013-01-29
[patent_title] => 'Microjet creation and control of shock waves'
[patent_app_type] => utility
[patent_app_number] => 12/454587
[patent_app_country] => US
[patent_app_date] => 2009-05-20
[patent_effective_date] => 0000-00-00
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[rel_patent_id] =>[rel_patent_doc_number] =>) 12/454587 | Microjet creation and control of shock waves | May 19, 2009 | Issued |
Array
(
[id] => 9955630
[patent_doc_number] => 09003812
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2015-04-14
[patent_title] => 'Supporting structure for a gas turbine engine'
[patent_app_type] => utility
[patent_app_number] => 13/319114
[patent_app_country] => US
[patent_app_date] => 2009-05-08
[patent_effective_date] => 0000-00-00
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[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13319114
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/319114 | Supporting structure for a gas turbine engine | May 7, 2009 | Issued |
Array
(
[id] => 8662272
[patent_doc_number] => 08375726
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2013-02-19
[patent_title] => 'Combustor assembly in a gas turbine engine'
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[rel_patent_id] =>[rel_patent_doc_number] =>) 12/431302 | Combustor assembly in a gas turbine engine | Apr 27, 2009 | Issued |
Array
(
[id] => 9748341
[patent_doc_number] => 08839805
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2014-09-23
[patent_title] => 'Passive boundary layer bleed system for nacelle inlet airflow control'
[patent_app_type] => utility
[patent_app_number] => 12/428582
[patent_app_country] => US
[patent_app_date] => 2009-04-23
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[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 12428582
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/428582 | Passive boundary layer bleed system for nacelle inlet airflow control | Apr 22, 2009 | Issued |
Array
(
[id] => 6229541
[patent_doc_number] => 20100263382
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2010-10-21
[patent_title] => 'DUAL ORIFICE PILOT FUEL INJECTOR'
[patent_app_type] => utility
[patent_app_number] => 12/424612
[patent_app_country] => US
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[rel_patent_id] =>[rel_patent_doc_number] =>) 12/424612 | DUAL ORIFICE PILOT FUEL INJECTOR | Apr 15, 2009 | Abandoned |
Array
(
[id] => 5312584
[patent_doc_number] => 20090277182
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2009-11-12
[patent_title] => 'FUEL LANCE'
[patent_app_type] => utility
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[pdf_file] => publications/A1/0277/20090277182.pdf
[firstpage_image] =>[orig_patent_app_number] => 12422497
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/422497 | Burner and fuel lance for a gas turbine installation | Apr 12, 2009 | Issued |
Array
(
[id] => 9689512
[patent_doc_number] => 08820092
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[patent_kind] => B2
[patent_issue_date] => 2014-09-02
[patent_title] => 'Gas turbine engine cooling system and method'
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[rel_patent_id] =>[rel_patent_doc_number] =>) 12/937213 | Gas turbine engine cooling system and method | Apr 8, 2009 | Issued |
Array
(
[id] => 5468385
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[patent_issue_date] => 2009-10-01
[patent_title] => 'Cogeneration of Hydrogen and Power'
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[firstpage_image] =>[orig_patent_app_number] => 12410487
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/410487 | Cogeneration of Hydrogen and Power | Mar 24, 2009 | Abandoned |
Array
(
[id] => 9572998
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[patent_issue_date] => 2014-07-01
[patent_title] => 'Turbomachine combustion chamber'
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[rel_patent_id] =>[rel_patent_doc_number] =>) 12/918946 | Turbomachine combustion chamber | Mar 5, 2009 | Issued |
Array
(
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[patent_title] => 'WALL STRUCTURE FOR LIMITING A HOT GAS PATH'
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[rel_patent_id] =>[rel_patent_doc_number] =>) 12/390901 | Wall structure for limiting a hot gas path | Feb 22, 2009 | Issued |
Array
(
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[patent_title] => 'PRE-HEATING GAS TURBINE INLET AIR USING AN EXTERNAL FIRED HEATER AND REDUCING OVERBOARD BLEED IN LOW-BTU APPLICATIONS'
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Array
(
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[rel_patent_id] =>[rel_patent_doc_number] =>) 12/367997 | Combustion chamber of a combustion system | Feb 8, 2009 | Issued |