
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] => 4647823
[patent_doc_number] => 20080035078
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2008-02-14
[patent_title] => 'Method and device of turbine submerged combustion boiler'
[patent_app_type] => utility
[patent_app_number] => 11/881420
[patent_app_country] => US
[patent_app_date] => 2007-07-28
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 2
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[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0035/20080035078.pdf
[firstpage_image] =>[orig_patent_app_number] => 11881420
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/881420 | Method and device of turbine submerged combustion boiler | Jul 27, 2007 | Issued |
Array
(
[id] => 5381810
[patent_doc_number] => 20090223054
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2009-09-10
[patent_title] => 'FUEL NOZZLE FOR A GAS TURBINE ENGINE AND METHOD OF FABRICATING THE SAME'
[patent_app_type] => utility
[patent_app_number] => 11/828447
[patent_app_country] => US
[patent_app_date] => 2007-07-26
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
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[pdf_file] => publications/A1/0223/20090223054.pdf
[firstpage_image] =>[orig_patent_app_number] => 11828447
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/828447 | Fuel nozzle assembly for a gas turbine engine | Jul 25, 2007 | Issued |
Array
(
[id] => 4736105
[patent_doc_number] => 20080229757
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2008-09-25
[patent_title] => 'Methods and systems for output variance and facilitation of maintenance of multiple gas turbine plants'
[patent_app_type] => utility
[patent_app_number] => 11/879317
[patent_app_country] => US
[patent_app_date] => 2007-07-17
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 2
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[pdf_file] => publications/A1/0229/20080229757.pdf
[firstpage_image] =>[orig_patent_app_number] => 11879317
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/879317 | Methods and systems for output variance and facilitation of maintenance of multiple gas turbine plants | Jul 16, 2007 | Issued |
Array
(
[id] => 78083
[patent_doc_number] => 07743599
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2010-06-29
[patent_title] => 'System and apparatus for gas turbine engine lean blowout avoidance'
[patent_app_type] => utility
[patent_app_number] => 11/779127
[patent_app_country] => US
[patent_app_date] => 2007-07-17
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 8
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[pdf_file] => patents/07/743/07743599.pdf
[firstpage_image] =>[orig_patent_app_number] => 11779127
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/779127 | System and apparatus for gas turbine engine lean blowout avoidance | Jul 16, 2007 | Issued |
Array
(
[id] => 5293582
[patent_doc_number] => 20090008508
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2009-01-08
[patent_title] => 'VARIABLE CONTOUR NACELLE ASSEMBLY FOR A GAS TURBINE ENGINE'
[patent_app_type] => utility
[patent_app_number] => 11/772287
[patent_app_country] => US
[patent_app_date] => 2007-07-02
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 6
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[pdf_file] => publications/A1/0008/20090008508.pdf
[firstpage_image] =>[orig_patent_app_number] => 11772287
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/772287 | Variable contour nacelle assembly for a gas turbine engine | Jul 1, 2007 | Issued |
Array
(
[id] => 5348637
[patent_doc_number] => 20090003998
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2009-01-01
[patent_title] => 'COMBUSTORS FOR USE IN TURBINE ENGINE ASSEMBLIES'
[patent_app_type] => utility
[patent_app_number] => 11/769077
[patent_app_country] => US
[patent_app_date] => 2007-06-27
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 7
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[pdf_file] => publications/A1/0003/20090003998.pdf
[firstpage_image] =>[orig_patent_app_number] => 11769077
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/769077 | Combustors for use in turbine engine assemblies | Jun 26, 2007 | Issued |
Array
(
[id] => 4665999
[patent_doc_number] => 20080041059
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2008-02-21
[patent_title] => 'Radially staged RQL combustor with tangential fuel premixers'
[patent_app_type] => utility
[patent_app_number] => 11/820427
[patent_app_country] => US
[patent_app_date] => 2007-06-19
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
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[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0041/20080041059.pdf
[firstpage_image] =>[orig_patent_app_number] => 11820427
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/820427 | Radially staged RQL combustor with tangential fuel-air premixers | Jun 18, 2007 | Issued |
Array
(
[id] => 9045205
[patent_doc_number] => 08539753
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2013-09-24
[patent_title] => 'Hybrid rocket motor with annular, concentric solid fuel elements'
[patent_app_type] => utility
[patent_app_number] => 11/764677
[patent_app_country] => US
[patent_app_date] => 2007-06-18
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
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[patent_no_of_words] => 2134
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[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 11764677
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/764677 | Hybrid rocket motor with annular, concentric solid fuel elements | Jun 17, 2007 | Issued |
Array
(
[id] => 4957808
[patent_doc_number] => 20080272232
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2008-11-06
[patent_title] => 'Jet Engine Exhaust Nozzle Flow Effector'
[patent_app_type] => utility
[patent_app_number] => 11/762827
[patent_app_country] => US
[patent_app_date] => 2007-06-14
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 8
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[pdf_file] => publications/A1/0272/20080272232.pdf
[firstpage_image] =>[orig_patent_app_number] => 11762827
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/762827 | Jet engine exhaust nozzle flow effector | Jun 13, 2007 | Issued |
Array
(
[id] => 5448624
[patent_doc_number] => 20090064659
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2009-03-12
[patent_title] => 'GAS TURBINE ENGINE WITH FAN VARIABLE AREA NOZZLE HAVING A ROTATIONAL VALVE SYSTEM'
[patent_app_type] => utility
[patent_app_number] => 11/755757
[patent_app_country] => US
[patent_app_date] => 2007-05-31
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
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[patent_no_of_words] => 2205
[patent_no_of_claims] => 18
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[pdf_file] => publications/A1/0064/20090064659.pdf
[firstpage_image] =>[orig_patent_app_number] => 11755757
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/755757 | Gas turbine engine with fan variable area nozzle having a rotational valve system | May 30, 2007 | Issued |
Array
(
[id] => 4706955
[patent_doc_number] => 20080295481
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2008-12-04
[patent_title] => 'Fluidic vectoring for exhaust nozzle'
[patent_app_type] => utility
[patent_app_number] => 11/809297
[patent_app_country] => US
[patent_app_date] => 2007-05-31
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[pdf_file] => publications/A1/0295/20080295481.pdf
[firstpage_image] =>[orig_patent_app_number] => 11809297
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/809297 | Fluidic vectoring for exhaust nozzle | May 30, 2007 | Issued |
Array
(
[id] => 4525671
[patent_doc_number] => 07870741
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2011-01-18
[patent_title] => 'Turbine engine valve assembly and method of assembling the same'
[patent_app_type] => utility
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[patent_app_country] => US
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[pdf_file] => patents/07/870/07870741.pdf
[firstpage_image] =>[orig_patent_app_number] => 11753907
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/753907 | Turbine engine valve assembly and method of assembling the same | May 24, 2007 | Issued |
Array
(
[id] => 5274236
[patent_doc_number] => 20090126368
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2009-05-21
[patent_title] => 'FUEL INJECTION SYSTEM FOR A GAS TURBINE ENGINE'
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[patent_app_number] => 11/748675
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[firstpage_image] =>[orig_patent_app_number] => 11748675
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/748675 | Fuel injection system for a gas turbine engine | May 14, 2007 | Issued |
Array
(
[id] => 6534611
[patent_doc_number] => 20100126140
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2010-05-27
[patent_title] => 'MILLIMETRE-SCALE ENGINE'
[patent_app_type] => utility
[patent_app_number] => 11/814927
[patent_app_country] => US
[patent_app_date] => 2007-05-09
[patent_effective_date] => 0000-00-00
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[firstpage_image] =>[orig_patent_app_number] => 11814927
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/814927 | Millimetre-scale engine | May 8, 2007 | Issued |
Array
(
[id] => 5267388
[patent_doc_number] => 20090071163
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2009-03-19
[patent_title] => 'SYSTEMS AND METHODS FOR INSTALLING COOLING HOLES IN A COMBUSTION LINER'
[patent_app_type] => utility
[patent_app_number] => 11/742197
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[firstpage_image] =>[orig_patent_app_number] => 11742197
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/742197 | SYSTEMS AND METHODS FOR INSTALLING COOLING HOLES IN A COMBUSTION LINER | Apr 29, 2007 | Abandoned |
Array
(
[id] => 5448626
[patent_doc_number] => 20090064661
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2009-03-12
[patent_title] => 'ELECTRO-DYNAMIC SWIRLER, COMBUSTION APPARATUS AND METHODS USING THE SAME'
[patent_app_type] => utility
[patent_app_number] => 11/734370
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[rel_patent_id] =>[rel_patent_doc_number] =>) 11/734370 | Electro-dynamic swirler, combustion apparatus and methods using the same | Apr 11, 2007 | Issued |
Array
(
[id] => 8355530
[patent_doc_number] => 20120210694
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[patent_kind] => A1
[patent_issue_date] => 2012-08-23
[patent_title] => 'TURBO MACHINE SPOOL PARAMETER DETECTION'
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[rel_patent_id] =>[rel_patent_doc_number] =>) 11/733874 | TURBO MACHINE SPOOL PARAMETER DETECTION | Apr 10, 2007 | Abandoned |
Array
(
[id] => 6260325
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[patent_title] => 'Stacked laminate gas turbine component'
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[rel_patent_id] =>[rel_patent_doc_number] =>) 11/784154 | Stacked laminate gas turbine component | Apr 4, 2007 | Issued |
Array
(
[id] => 4464133
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[rel_patent_id] =>[rel_patent_doc_number] =>) 11/691337 | Combustors and combustion systems for gas turbine engines | Mar 25, 2007 | Issued |
Array
(
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[patent_title] => 'Gas turbine engine starting method and control device'
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[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 12227470
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/227470 | Gas turbine engine starting method and control device | Feb 26, 2007 | Issued |