Search

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 numberTitle of the applicationFiling DateStatus
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 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 0 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [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 [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] => 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 [patent_words_short_claim] => 139 [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 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 91 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [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 [patent_no_of_ind_claims] => 2 [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] => 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 [patent_figures_cnt] => 11 [patent_no_of_words] => 5853 [patent_no_of_claims] => 20 [patent_no_of_ind_claims] => 5 [patent_words_short_claim] => 125 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [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 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 265 [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 [patent_no_of_claims] => 17 [patent_no_of_ind_claims] => 2 [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] => 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 [patent_figures_cnt] => 5 [patent_no_of_words] => 2721 [patent_no_of_claims] => 18 [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] => 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 [patent_figures_cnt] => 4 [patent_no_of_words] => 2420 [patent_no_of_claims] => 9 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 127 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [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 [patent_figures_cnt] => 4 [patent_no_of_words] => 1842 [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] => 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 [patent_figures_cnt] => 6 [patent_no_of_words] => 2892 [patent_no_of_claims] => 5 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 235 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [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 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 3 [patent_figures_cnt] => 3 [patent_no_of_words] => 4561 [patent_no_of_claims] => 12 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 244 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [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 [patent_drawing_sheets_cnt] => 3 [patent_figures_cnt] => 3 [patent_no_of_words] => 2603 [patent_no_of_claims] => 19 [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] => 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 [patent_drawing_sheets_cnt] => 8 [patent_figures_cnt] => 8 [patent_no_of_words] => 4963 [patent_no_of_claims] => 20 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 121 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13195629 [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 [patent_app_date] => 2011-07-29 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 6 [patent_figures_cnt] => 6 [patent_no_of_words] => 2854 [patent_no_of_claims] => 11 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 229 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13193865 [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' [patent_app_type] => utility [patent_app_number] => 13/193696 [patent_app_country] => US [patent_app_date] => 2011-07-29 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 10 [patent_figures_cnt] => 15 [patent_no_of_words] => 2456 [patent_no_of_claims] => 9 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 128 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13193696 [rel_patent_id] =>[rel_patent_doc_number] =>)
13/193696
Microcircuit cooling for gas turbine engine combustor Jul 28, 2011 Issued
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