
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] => 9993786
[patent_doc_number] => 09038367
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2015-05-26
[patent_title] => 'Fan case thrust reverser'
[patent_app_type] => utility
[patent_app_number] => 13/234213
[patent_app_country] => US
[patent_app_date] => 2011-09-16
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 8
[patent_figures_cnt] => 9
[patent_no_of_words] => 2644
[patent_no_of_claims] => 20
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 87
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13234213
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/234213 | Fan case thrust reverser | Sep 15, 2011 | Issued |
Array
(
[id] => 8047145
[patent_doc_number] => 20120073305
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2012-03-29
[patent_title] => 'COMBUSTION CHAMBER AND METHOD FOR OPERATING A COMBUSTION CHAMBER'
[patent_app_type] => utility
[patent_app_number] => 13/233369
[patent_app_country] => US
[patent_app_date] => 2011-09-15
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 7
[patent_figures_cnt] => 7
[patent_no_of_words] => 3875
[patent_no_of_claims] => 14
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[patent_maintenance] => 1
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[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0073/20120073305.pdf
[firstpage_image] =>[orig_patent_app_number] => 13233369
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/233369 | Combustion chamber and method for operating a combustion chamber | Sep 14, 2011 | Issued |
Array
(
[id] => 8704308
[patent_doc_number] => 20130061597
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2013-03-14
[patent_title] => 'Systems and Methods for Inlet Fogging Control'
[patent_app_type] => utility
[patent_app_number] => 13/232002
[patent_app_country] => US
[patent_app_date] => 2011-09-14
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 6
[patent_figures_cnt] => 6
[patent_no_of_words] => 3613
[patent_no_of_claims] => 20
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[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13232002
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/232002 | Systems and methods for inlet fogging control | Sep 13, 2011 | Issued |
Array
(
[id] => 9007267
[patent_doc_number] => 08522553
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2013-09-03
[patent_title] => 'System and method for conditioning a working fluid in a combustor'
[patent_app_type] => utility
[patent_app_number] => 13/232191
[patent_app_country] => US
[patent_app_date] => 2011-09-14
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 4
[patent_no_of_words] => 3856
[patent_no_of_claims] => 16
[patent_no_of_ind_claims] => 3
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[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13232191
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/232191 | System and method for conditioning a working fluid in a combustor | Sep 13, 2011 | Issued |
Array
(
[id] => 10045642
[patent_doc_number] => 09086033
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2015-07-21
[patent_title] => 'Additive manufactured propulsion system'
[patent_app_type] => utility
[patent_app_number] => 13/231603
[patent_app_country] => US
[patent_app_date] => 2011-09-13
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 10
[patent_figures_cnt] => 10
[patent_no_of_words] => 8298
[patent_no_of_claims] => 9
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[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13231603
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/231603 | Additive manufactured propulsion system | Sep 12, 2011 | Issued |
Array
(
[id] => 8704306
[patent_doc_number] => 20130061595
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2013-03-14
[patent_title] => 'Speed Card-Controlled Override Fuel Pump Assist'
[patent_app_type] => utility
[patent_app_number] => 13/229751
[patent_app_country] => US
[patent_app_date] => 2011-09-11
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 18
[patent_figures_cnt] => 18
[patent_no_of_words] => 4486
[patent_no_of_claims] => 16
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[patent_current_assignee] =>[type] => publication
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13229751
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/229751 | Speed card-controlled override fuel pump assist | Sep 10, 2011 | Issued |
Array
(
[id] => 8704305
[patent_doc_number] => 20130061594
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2013-03-14
[patent_title] => 'TURNING GUIDE FOR COMBUSTION FUEL NOZZLE IN GAS TURBINE AND METHOD TO TURN FUEL FLOW ENTERING COMBUSTION CHAMBER'
[patent_app_type] => utility
[patent_app_number] => 13/229115
[patent_app_country] => US
[patent_app_date] => 2011-09-09
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 10
[patent_figures_cnt] => 10
[patent_no_of_words] => 3638
[patent_no_of_claims] => 20
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 0
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13229115
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/229115 | Turning guide for combustion fuel nozzle in gas turbine and method to turn fuel flow entering combustion chamber | Sep 8, 2011 | Issued |
Array
(
[id] => 10891455
[patent_doc_number] => 08915059
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2014-12-23
[patent_title] => 'Fuel gas pressure control system and method for reducing gas turbine fuel supply pressure requirements'
[patent_app_type] => utility
[patent_app_number] => 13/229202
[patent_app_country] => US
[patent_app_date] => 2011-09-09
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
[patent_figures_cnt] => 5
[patent_no_of_words] => 5313
[patent_no_of_claims] => 12
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 146
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13229202
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/229202 | Fuel gas pressure control system and method for reducing gas turbine fuel supply pressure requirements | Sep 8, 2011 | Issued |
Array
(
[id] => 9975513
[patent_doc_number] => 09021813
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2015-05-05
[patent_title] => 'Cable-actuated variable area fan nozzle with elastomeric seals'
[patent_app_type] => utility
[patent_app_number] => 13/225803
[patent_app_country] => US
[patent_app_date] => 2011-09-06
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 10
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[patent_no_of_words] => 5853
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[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13225803
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/225803 | Cable-actuated variable area fan nozzle with elastomeric seals | Sep 5, 2011 | Issued |
Array
(
[id] => 10057769
[patent_doc_number] => 09097118
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2015-08-04
[patent_title] => 'Transitional region for a combustion chamber of a gas turbine'
[patent_app_type] => utility
[patent_app_number] => 13/226020
[patent_app_country] => US
[patent_app_date] => 2011-09-06
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 2
[patent_figures_cnt] => 4
[patent_no_of_words] => 5157
[patent_no_of_claims] => 18
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[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13226020
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/226020 | Transitional region for a combustion chamber of a gas turbine | Sep 5, 2011 | Issued |
Array
(
[id] => 8693712
[patent_doc_number] => 20130055721
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2013-03-07
[patent_title] => 'METHOD AND APPARATUS FOR SEGREGATED OIL SUPPLY AND SCAVENGE IN A GAS TURBINE ENGINE'
[patent_app_type] => utility
[patent_app_number] => 13/225510
[patent_app_country] => US
[patent_app_date] => 2011-09-05
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 3
[patent_no_of_words] => 2410
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[patent_current_assignee] =>[type] => publication
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13225510
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/225510 | Method and apparatus for segregated oil supply and scavenge in a gas turbine engine | Sep 4, 2011 | Issued |
Array
(
[id] => 8693715
[patent_doc_number] => 20130055724
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2013-03-07
[patent_title] => 'GAS TURBINE ENGINE AIR CYCLE SYSTEM'
[patent_app_type] => utility
[patent_app_number] => 13/223578
[patent_app_country] => US
[patent_app_date] => 2011-09-01
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
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[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13223578
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/223578 | GAS TURBINE ENGINE AIR CYCLE SYSTEM | Aug 31, 2011 | Abandoned |
Array
(
[id] => 10071116
[patent_doc_number] => 09109464
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2015-08-18
[patent_title] => 'Distributed lubrication system'
[patent_app_type] => utility
[patent_app_number] => 13/222183
[patent_app_country] => US
[patent_app_date] => 2011-08-31
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
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[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13222183
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/222183 | Distributed lubrication system | Aug 30, 2011 | Issued |
Array
(
[id] => 8679335
[patent_doc_number] => 20130047619
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2013-02-28
[patent_title] => 'INJECTION NOZZLE ASSEMBLY FOR A GAS TURBOMACHINE'
[patent_app_type] => utility
[patent_app_number] => 13/221027
[patent_app_country] => US
[patent_app_date] => 2011-08-30
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
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[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13221027
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/221027 | INJECTION NOZZLE ASSEMBLY FOR A GAS TURBOMACHINE | Aug 29, 2011 | Abandoned |
Array
(
[id] => 9880156
[patent_doc_number] => 08966905
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2015-03-03
[patent_title] => 'Combustion device'
[patent_app_type] => utility
[patent_app_number] => 13/217979
[patent_app_country] => US
[patent_app_date] => 2011-08-25
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
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[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13217979
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/217979 | Combustion device | Aug 24, 2011 | Issued |
Array
(
[id] => 8894760
[patent_doc_number] => 08474271
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2013-07-02
[patent_title] => 'System and method for hot ambient and grid frequency compensation for a gas turbine'
[patent_app_type] => utility
[patent_app_number] => 13/205006
[patent_app_country] => US
[patent_app_date] => 2011-08-08
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[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13205006
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/205006 | System and method for hot ambient and grid frequency compensation for a gas turbine | Aug 7, 2011 | Issued |
Array
(
[id] => 8646182
[patent_doc_number] => 20130031912
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2013-02-07
[patent_title] => 'GAS TURBINE START ARCHITECTURE'
[patent_app_type] => utility
[patent_app_number] => 13/195223
[patent_app_country] => US
[patent_app_date] => 2011-08-01
[patent_effective_date] => 0000-00-00
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[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13195223
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/195223 | GAS TURBINE START ARCHITECTURE | Jul 31, 2011 | Abandoned |
Array
(
[id] => 9993787
[patent_doc_number] => 09038368
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2015-05-26
[patent_title] => 'Systems, methods, and apparatus for providing a multi-fuel hybrid rocket motor'
[patent_app_type] => utility
[patent_app_number] => 13/195629
[patent_app_country] => US
[patent_app_date] => 2011-08-01
[patent_effective_date] => 0000-00-00
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[rel_patent_id] =>[rel_patent_doc_number] =>) 13/195629 | Systems, methods, and apparatus for providing a multi-fuel hybrid rocket motor | Jul 31, 2011 | Issued |
Array
(
[id] => 10574903
[patent_doc_number] => 09297534
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2016-03-29
[patent_title] => 'Combustor portion for a turbomachine and method of operating a turbomachine'
[patent_app_type] => utility
[patent_app_number] => 13/193865
[patent_app_country] => US
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[rel_patent_id] =>[rel_patent_doc_number] =>) 13/193865 | Combustor portion for a turbomachine and method of operating a turbomachine | Jul 28, 2011 | Issued |
Array
(
[id] => 10014512
[patent_doc_number] => 09057523
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2015-06-16
[patent_title] => 'Microcircuit cooling for gas turbine engine combustor'
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[rel_patent_id] =>[rel_patent_doc_number] =>) 13/193696 | Microcircuit cooling for gas turbine engine combustor | Jul 28, 2011 | Issued |