
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] => 5212640
[patent_doc_number] => 20070101720
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2007-05-10
[patent_title] => 'Methods and apparatus for a combustion turbine fuel recirculation system and nitrogen purge system'
[patent_app_type] => utility
[patent_app_number] => 11/268247
[patent_app_country] => US
[patent_app_date] => 2005-11-07
[patent_effective_date] => 0000-00-00
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[pdf_file] => publications/A1/0101/20070101720.pdf
[firstpage_image] =>[orig_patent_app_number] => 11268247
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/268247 | Methods and apparatus for a combustion turbine fuel recirculation system and nitrogen purge system | Nov 6, 2005 | Issued |
Array
(
[id] => 5212643
[patent_doc_number] => 20070101723
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2007-05-10
[patent_title] => 'Methods and apparatus for a combustion turbine nitrogen purge system'
[patent_app_type] => utility
[patent_app_number] => 11/268041
[patent_app_country] => US
[patent_app_date] => 2005-11-07
[patent_effective_date] => 0000-00-00
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[firstpage_image] =>[orig_patent_app_number] => 11268041
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/268041 | Methods and apparatus for a combustion turbine nitrogen purge system | Nov 6, 2005 | Issued |
Array
(
[id] => 5571879
[patent_doc_number] => 20090139238
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2009-06-04
[patent_title] => 'AIRFLOW DISTRIBUTION TO A LOW EMISSIONS COMBUSTOR'
[patent_app_type] => utility
[patent_app_number] => 11/262447
[patent_app_country] => US
[patent_app_date] => 2005-10-28
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
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[patent_no_of_words] => 2000
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[pdf_file] => publications/A1/0139/20090139238.pdf
[firstpage_image] =>[orig_patent_app_number] => 11262447
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/262447 | Airflow distribution to a low emissions combustor | Oct 27, 2005 | Issued |
Array
(
[id] => 5037139
[patent_doc_number] => 20070089421
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2007-04-26
[patent_title] => 'Assembly and method for cooling rear bearing and exhaust frame of gas turbine'
[patent_app_type] => utility
[patent_app_number] => 11/257153
[patent_app_country] => US
[patent_app_date] => 2005-10-25
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 7
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[patent_no_of_words] => 1854
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[firstpage_image] =>[orig_patent_app_number] => 11257153
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/257153 | Assembly and method for cooling rear bearing and exhaust frame of gas turbine | Oct 24, 2005 | Issued |
Array
(
[id] => 5037145
[patent_doc_number] => 20070089427
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2007-04-26
[patent_title] => 'Two-branch mixing passage and method to control combustor pulsations'
[patent_app_type] => utility
[patent_app_number] => 11/257264
[patent_app_country] => US
[patent_app_date] => 2005-10-24
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 7
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[pdf_file] => publications/A1/0089/20070089427.pdf
[firstpage_image] =>[orig_patent_app_number] => 11257264
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/257264 | Two-branch mixing passage and method to control combustor pulsations | Oct 23, 2005 | Abandoned |
Array
(
[id] => 5037146
[patent_doc_number] => 20070089428
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2007-04-26
[patent_title] => 'Gas turbine engine mixing duct and method to start the engine'
[patent_app_type] => utility
[patent_app_number] => 11/255339
[patent_app_country] => US
[patent_app_date] => 2005-10-21
[patent_effective_date] => 0000-00-00
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[firstpage_image] =>[orig_patent_app_number] => 11255339
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/255339 | Gas turbine engine mixing duct and method to start the engine | Oct 20, 2005 | Issued |
Array
(
[id] => 59912
[patent_doc_number] => 07762076
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2010-07-27
[patent_title] => 'Attachment of a ceramic combustor can'
[patent_app_type] => utility
[patent_app_number] => 11/254876
[patent_app_country] => US
[patent_app_date] => 2005-10-20
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 2
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[patent_no_of_words] => 2200
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[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/07/762/07762076.pdf
[firstpage_image] =>[orig_patent_app_number] => 11254876
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/254876 | Attachment of a ceramic combustor can | Oct 19, 2005 | Issued |
Array
(
[id] => 5740356
[patent_doc_number] => 20060086078
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2006-04-27
[patent_title] => 'Universal Carnot propulsion systems for turbo rocketry'
[patent_app_type] => utility
[patent_app_number] => 11/254421
[patent_app_country] => US
[patent_app_date] => 2005-10-20
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 16
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[patent_no_of_words] => 4223
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[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0086/20060086078.pdf
[firstpage_image] =>[orig_patent_app_number] => 11254421
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/254421 | Universal Carnot propulsion systems for turbo rocketry | Oct 19, 2005 | Abandoned |
Array
(
[id] => 4541183
[patent_doc_number] => 07836698
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2010-11-23
[patent_title] => 'Combustor with staged fuel premixer'
[patent_app_type] => utility
[patent_app_number] => 11/163483
[patent_app_country] => US
[patent_app_date] => 2005-10-20
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 1
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[pdf_file] => patents/07/836/07836698.pdf
[firstpage_image] =>[orig_patent_app_number] => 11163483
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/163483 | Combustor with staged fuel premixer | Oct 19, 2005 | Issued |
Array
(
[id] => 4983333
[patent_doc_number] => 20070087892
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2007-04-19
[patent_title] => 'Gas turbine engine assembly and methods of assembling same'
[patent_app_type] => utility
[patent_app_number] => 11/253495
[patent_app_country] => US
[patent_app_date] => 2005-10-19
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 8
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[pdf_file] => publications/A1/0087/20070087892.pdf
[firstpage_image] =>[orig_patent_app_number] => 11253495
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/253495 | Gas turbine assembly and methods of assembling same | Oct 18, 2005 | Issued |
Array
(
[id] => 5072071
[patent_doc_number] => 20070012046
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2007-01-18
[patent_title] => 'GAS TURBINE INTERMEDIATE STRUCTURE AND A GAS TURBINE ENGINE COMPRISING THE INTERMEDIATE STRUCTURE'
[patent_app_type] => utility
[patent_app_number] => 11/163172
[patent_app_country] => US
[patent_app_date] => 2005-10-07
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[pdf_file] => publications/A1/0012/20070012046.pdf
[firstpage_image] =>[orig_patent_app_number] => 11163172
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/163172 | GAS TURBINE INTERMEDIATE STRUCTURE AND A GAS TURBINE ENGINE COMPRISING THE INTERMEDIATE STRUCTURE | Oct 6, 2005 | Abandoned |
Array
(
[id] => 207831
[patent_doc_number] => 07624578
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2009-12-01
[patent_title] => 'Method and apparatus for generating combustion products within a gas turbine engine'
[patent_app_type] => utility
[patent_app_number] => 11/241391
[patent_app_country] => US
[patent_app_date] => 2005-09-30
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[pdf_file] => patents/07/624/07624578.pdf
[firstpage_image] =>[orig_patent_app_number] => 11241391
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/241391 | Method and apparatus for generating combustion products within a gas turbine engine | Sep 29, 2005 | Issued |
Array
(
[id] => 302400
[patent_doc_number] => 07533533
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2009-05-19
[patent_title] => 'Jet engine with a variable section nozzle of which at least one flap pivots about a pin, pins for flaps'
[patent_app_type] => utility
[patent_app_number] => 11/236576
[patent_app_country] => US
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[firstpage_image] =>[orig_patent_app_number] => 11236576
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/236576 | Jet engine with a variable section nozzle of which at least one flap pivots about a pin, pins for flaps | Sep 27, 2005 | Issued |
Array
(
[id] => 5013196
[patent_doc_number] => 20070256404
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2007-11-08
[patent_title] => 'Method of adjusting a triggering clearance and a trigger'
[patent_app_type] => utility
[patent_app_number] => 11/234180
[patent_app_country] => US
[patent_app_date] => 2005-09-26
[patent_effective_date] => 0000-00-00
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[firstpage_image] =>[orig_patent_app_number] => 11234180
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/234180 | Method of adjusting a triggering clearance and a trigger | Sep 25, 2005 | Issued |
Array
(
[id] => 273040
[patent_doc_number] => 07559203
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[patent_kind] => B2
[patent_issue_date] => 2009-07-14
[patent_title] => 'Cooled support boss for a combustor in a gas turbine engine'
[patent_app_type] => utility
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[rel_patent_id] =>[rel_patent_doc_number] =>) 11/227285 | Cooled support boss for a combustor in a gas turbine engine | Sep 15, 2005 | Issued |
Array
(
[id] => 5897026
[patent_doc_number] => 20060042259
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2006-03-02
[patent_title] => 'Combined-cycle power plant and steam thermal power plant'
[patent_app_type] => utility
[patent_app_number] => 11/213724
[patent_app_country] => US
[patent_app_date] => 2005-08-30
[patent_effective_date] => 0000-00-00
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[firstpage_image] =>[orig_patent_app_number] => 11213724
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/213724 | Combined-cycle power plant and steam thermal power plant | Aug 29, 2005 | Abandoned |
Array
(
[id] => 5151040
[patent_doc_number] => 20070033921
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[patent_kind] => A1
[patent_issue_date] => 2007-02-15
[patent_title] => 'Aircraft engine exhaust flap curved strut slot'
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[firstpage_image] =>[orig_patent_app_number] => 11200895
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/200895 | Aircraft engine exhaust flap curved strut slot | Aug 9, 2005 | Issued |
Array
(
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Array
(
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[patent_title] => 'Helicopter defense system and method'
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[firstpage_image] =>[orig_patent_app_number] => 11199267
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/199267 | Helicopter defense system and method | Aug 8, 2005 | Abandoned |
Array
(
[id] => 5049259
[patent_doc_number] => 20070029803
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[patent_kind] => A1
[patent_issue_date] => 2007-02-08
[patent_title] => 'Machine for transferring power and producing electricity in a jet engine'
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[patent_app_country] => US
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[pdf_file] => publications/A1/0029/20070029803.pdf
[firstpage_image] =>[orig_patent_app_number] => 11197689
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/197689 | Machine for transferring power and producing electricity in a jet engine | Aug 3, 2005 | Abandoned |