
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] => 4678845
[patent_doc_number] => 20080245071
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2008-10-09
[patent_title] => 'THERMAL POWER PLANT'
[patent_app_type] => utility
[patent_app_number] => 12/056805
[patent_app_country] => US
[patent_app_date] => 2008-03-27
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 10
[patent_figures_cnt] => 10
[patent_no_of_words] => 10993
[patent_no_of_claims] => 10
[patent_no_of_ind_claims] => 1
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[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0245/20080245071.pdf
[firstpage_image] =>[orig_patent_app_number] => 12056805
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/056805 | THERMAL POWER PLANT | Mar 26, 2008 | Abandoned |
Array
(
[id] => 4678848
[patent_doc_number] => 20080245074
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2008-10-09
[patent_title] => 'Combustor of a gas turbine engine'
[patent_app_type] => utility
[patent_app_number] => 12/076087
[patent_app_country] => US
[patent_app_date] => 2008-03-13
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 11
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[patent_no_of_words] => 6281
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[pdf_file] => publications/A1/0245/20080245074.pdf
[firstpage_image] =>[orig_patent_app_number] => 12076087
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/076087 | Combustor of a gas turbine engine | Mar 12, 2008 | Issued |
Array
(
[id] => 5381957
[patent_doc_number] => 20090223201
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2009-09-10
[patent_title] => 'Methods of Injecting Diluent Into A Gas Turbine Assembly'
[patent_app_type] => utility
[patent_app_number] => 12/045497
[patent_app_country] => US
[patent_app_date] => 2008-03-10
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
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[patent_no_of_words] => 3322
[patent_no_of_claims] => 16
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[pdf_file] => publications/A1/0223/20090223201.pdf
[firstpage_image] =>[orig_patent_app_number] => 12045497
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/045497 | Methods of Injecting Diluent Into A Gas Turbine Assembly | Mar 9, 2008 | Abandoned |
Array
(
[id] => 7769866
[patent_doc_number] => 08117847
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2012-02-21
[patent_title] => 'Hybrid missile propulsion system with reconfigurable multinozzle grid'
[patent_app_type] => utility
[patent_app_number] => 12/044227
[patent_app_country] => US
[patent_app_date] => 2008-03-07
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 9
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[patent_no_of_words] => 4388
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[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/08/117/08117847.pdf
[firstpage_image] =>[orig_patent_app_number] => 12044227
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/044227 | Hybrid missile propulsion system with reconfigurable multinozzle grid | Mar 6, 2008 | Issued |
Array
(
[id] => 5381983
[patent_doc_number] => 20090223227
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2009-09-10
[patent_title] => 'Combustion cap with crown mixing holes'
[patent_app_type] => utility
[patent_app_number] => 12/073407
[patent_app_country] => US
[patent_app_date] => 2008-03-05
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 9
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[patent_no_of_words] => 2346
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[pdf_file] => publications/A1/0223/20090223227.pdf
[firstpage_image] =>[orig_patent_app_number] => 12073407
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/073407 | Combustion cap with crown mixing holes | Mar 4, 2008 | Abandoned |
Array
(
[id] => 6181448
[patent_doc_number] => 20110167794
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2011-07-14
[patent_title] => 'Multi-Functional Pulse-Divided Rocket'
[patent_app_type] => utility
[patent_app_number] => 12/041797
[patent_app_country] => US
[patent_app_date] => 2008-03-04
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 8
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[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0167/20110167794.pdf
[firstpage_image] =>[orig_patent_app_number] => 12041797
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/041797 | Multi-functional pulse-divided rocket | Mar 3, 2008 | Issued |
Array
(
[id] => 8196828
[patent_doc_number] => 08186145
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2012-05-29
[patent_title] => 'Rocket nozzles for unconventional vehicles'
[patent_app_type] => utility
[patent_app_number] => 12/072487
[patent_app_country] => US
[patent_app_date] => 2008-02-26
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 13
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[patent_no_of_words] => 3321
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[patent_words_short_claim] => 160
[patent_maintenance] => 1
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[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/08/186/08186145.pdf
[firstpage_image] =>[orig_patent_app_number] => 12072487
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/072487 | Rocket nozzles for unconventional vehicles | Feb 25, 2008 | Issued |
Array
(
[id] => 5388029
[patent_doc_number] => 20090205341
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2009-08-20
[patent_title] => 'GAS TURBINE ENGINE WITH TWIN TOWERSHAFT ACCESSORY GEARBOX'
[patent_app_type] => utility
[patent_app_number] => 12/033902
[patent_app_country] => US
[patent_app_date] => 2008-02-20
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 7
[patent_figures_cnt] => 7
[patent_no_of_words] => 1516
[patent_no_of_claims] => 20
[patent_no_of_ind_claims] => 3
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[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0205/20090205341.pdf
[firstpage_image] =>[orig_patent_app_number] => 12033902
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/033902 | GAS TURBINE ENGINE WITH TWIN TOWERSHAFT ACCESSORY GEARBOX | Feb 19, 2008 | Abandoned |
Array
(
[id] => 5476582
[patent_doc_number] => 20090199563
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2009-08-13
[patent_title] => 'Scalable pyrospin combustor'
[patent_app_type] => utility
[patent_app_number] => 12/069107
[patent_app_country] => US
[patent_app_date] => 2008-02-07
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
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[patent_no_of_words] => 5556
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[pdf_file] => publications/A1/0199/20090199563.pdf
[firstpage_image] =>[orig_patent_app_number] => 12069107
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/069107 | Scalable pyrospin combustor | Feb 6, 2008 | Abandoned |
Array
(
[id] => 6213638
[patent_doc_number] => 20100050591
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2010-03-04
[patent_title] => 'Method for automatic closed-loop control of one or more combustion temperatures in a gas turbine installation and method for determination of the water content in the working fluid of a gas turbine instalation'
[patent_app_type] => utility
[patent_app_number] => 12/068337
[patent_app_country] => US
[patent_app_date] => 2008-02-05
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 2
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[patent_no_of_words] => 4377
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[pdf_file] => publications/A1/0050/20100050591.pdf
[firstpage_image] =>[orig_patent_app_number] => 12068337
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/068337 | Method for automatic closed-loop control of one or more combustion temperatures in a gas turbine installation and method for determination of the water content in the working fluid of a gas turbine installation | Feb 4, 2008 | Issued |
Array
(
[id] => 5523733
[patent_doc_number] => 20090193809
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2009-08-06
[patent_title] => 'METHOD AND SYSTEM TO FACILITATE COMBINED CYCLE WORKING FLUID MODIFICATION AND COMBUSTION THEREOF'
[patent_app_type] => utility
[patent_app_number] => 12/025437
[patent_app_country] => US
[patent_app_date] => 2008-02-04
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[pdf_file] => publications/A1/0193/20090193809.pdf
[firstpage_image] =>[orig_patent_app_number] => 12025437
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/025437 | METHOD AND SYSTEM TO FACILITATE COMBINED CYCLE WORKING FLUID MODIFICATION AND COMBUSTION THEREOF | Feb 3, 2008 | Abandoned |
Array
(
[id] => 6578109
[patent_doc_number] => 20100000221
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2010-01-07
[patent_title] => 'Method for producing fuel and power from a methane hydrate bed using a gas turbine engine'
[patent_app_type] => utility
[patent_app_number] => 12/012397
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[patent_app_date] => 2008-01-31
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[rel_patent_id] =>[rel_patent_doc_number] =>) 12/012397 | Method for producing fuel and power from a methane hydrate bed using a gas turbine engine | Jan 30, 2008 | Abandoned |
Array
(
[id] => 6244683
[patent_doc_number] => 20100024431
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2010-02-04
[patent_title] => 'METHOD OF DETECTING A PARTIAL FLAME FAILURE IN A GAS TURBINE ENGINE AND A GAS TURBINE ENGINE'
[patent_app_type] => utility
[patent_app_number] => 12/524788
[patent_app_country] => US
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[firstpage_image] =>[orig_patent_app_number] => 12524788
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/524788 | Method of detecting a partial flame failure in a gas turbine engine and a gas turbine engine | Jan 27, 2008 | Issued |
Array
(
[id] => 7794016
[patent_doc_number] => 08122720
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2012-02-28
[patent_title] => 'Fuel nozzle apparatus, gas turbine, and method of controlling fuel nozzle apparatus'
[patent_app_type] => utility
[patent_app_number] => 12/010393
[patent_app_country] => US
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[firstpage_image] =>[orig_patent_app_number] => 12010393
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/010393 | Fuel nozzle apparatus, gas turbine, and method of controlling fuel nozzle apparatus | Jan 23, 2008 | Issued |
Array
(
[id] => 5352148
[patent_doc_number] => 20090183492
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2009-07-23
[patent_title] => 'COMBUSTION LEAN-BLOWOUT PROTECTION VIA NOZZLE EQUIVALENCE RATIO CONTROL'
[patent_app_type] => utility
[patent_app_number] => 12/017507
[patent_app_country] => US
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[rel_patent_id] =>[rel_patent_doc_number] =>) 12/017507 | COMBUSTION LEAN-BLOWOUT PROTECTION VIA NOZZLE EQUIVALENCE RATIO CONTROL | Jan 21, 2008 | Abandoned |
Array
(
[id] => 8824503
[patent_doc_number] => 20130125548
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2013-05-23
[patent_title] => 'FLOW CONDITIONER FOR FUEL INJECTOR FOR COMBUSTOR AND METHOD FOR LOW-NOx COMBUSTOR'
[patent_app_type] => utility
[patent_app_number] => 12/015366
[patent_app_country] => US
[patent_app_date] => 2008-01-16
[patent_effective_date] => 0000-00-00
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[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 12015366
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/015366 | Flow conditioner for fuel injector for combustor and method for low-NOx combustor | Jan 15, 2008 | Issued |
Array
(
[id] => 5430851
[patent_doc_number] => 20090165436
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2009-07-02
[patent_title] => 'Premixed, preswirled plasma-assisted pilot'
[patent_app_type] => utility
[patent_app_number] => 12/005807
[patent_app_country] => US
[patent_app_date] => 2007-12-28
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Array
(
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[patent_issue_date] => 2010-02-25
[patent_title] => 'GAS TURBINE ENGINE COMBUSTOR AND METHOD FOR DELIVERING PURGE GAS INTO A COMBUSTION CHAMBER OF THE COMBUSTOR'
[patent_app_type] => utility
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[rel_patent_id] =>[rel_patent_doc_number] =>) 11/965397 | Gas turbine engine combustor and method for delivering purge gas into a combustion chamber of the combustor | Dec 26, 2007 | Issued |
Array
(
[id] => 7499740
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[patent_issue_date] => 2011-10-11
[patent_title] => 'Drive device on the basis of a gel-type propellant and method for conveying propellant'
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[rel_patent_id] =>[rel_patent_doc_number] =>) 12/005651 | Drive device on the basis of a gel-type propellant and method for conveying propellant | Dec 26, 2007 | Issued |
Array
(
[id] => 6315056
[patent_doc_number] => 20100242488
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2010-09-30
[patent_title] => ' GAS TURBINE ENGINE AND METHOD OF OPERATION'
[patent_app_type] => utility
[patent_app_number] => 12/742031
[patent_app_country] => US
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[rel_patent_id] =>[rel_patent_doc_number] =>) 12/742031 | GAS TURBINE ENGINE AND METHOD OF OPERATION | Nov 28, 2007 | Abandoned |