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] => 6096619 [patent_doc_number] => 20110162387 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2011-07-07 [patent_title] => 'TURBINE COOLING SYSTEM' [patent_app_type] => utility [patent_app_number] => 13/119291 [patent_app_country] => US [patent_app_date] => 2009-08-19 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 7 [patent_figures_cnt] => 7 [patent_no_of_words] => 5021 [patent_no_of_claims] => 16 [patent_no_of_ind_claims] => 4 [patent_words_short_claim] => 0 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] => publications/A1/0162/20110162387.pdf [firstpage_image] =>[orig_patent_app_number] => 13119291 [rel_patent_id] =>[rel_patent_doc_number] =>)
13/119291
Turbine cooling system Aug 18, 2009 Issued
Array ( [id] => 6445002 [patent_doc_number] => 20100038455 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2010-02-18 [patent_title] => 'LIQUID EJECTOR' [patent_app_type] => utility [patent_app_number] => 12/508160 [patent_app_country] => US [patent_app_date] => 2009-07-23 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 4 [patent_figures_cnt] => 4 [patent_no_of_words] => 1559 [patent_no_of_claims] => 12 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 0 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] => publications/A1/0038/20100038455.pdf [firstpage_image] =>[orig_patent_app_number] => 12508160 [rel_patent_id] =>[rel_patent_doc_number] =>)
12/508160
LIQUID EJECTOR Jul 22, 2009 Abandoned
Array ( [id] => 9373506 [patent_doc_number] => 08677754 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2014-03-25 [patent_title] => 'Fuel supply system for a gas-turbine engine' [patent_app_type] => utility [patent_app_number] => 12/501602 [patent_app_country] => US [patent_app_date] => 2009-07-13 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 5 [patent_figures_cnt] => 10 [patent_no_of_words] => 3112 [patent_no_of_claims] => 15 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 286 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 12501602 [rel_patent_id] =>[rel_patent_doc_number] =>)
12/501602
Fuel supply system for a gas-turbine engine Jul 12, 2009 Issued
Array ( [id] => 9243294 [patent_doc_number] => 08607569 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2013-12-17 [patent_title] => 'Methods and systems to thermally protect fuel nozzles in combustion systems' [patent_app_type] => utility [patent_app_number] => 12/495918 [patent_app_country] => US [patent_app_date] => 2009-07-01 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 4 [patent_figures_cnt] => 5 [patent_no_of_words] => 4130 [patent_no_of_claims] => 17 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 200 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 12495918 [rel_patent_id] =>[rel_patent_doc_number] =>)
12/495918
Methods and systems to thermally protect fuel nozzles in combustion systems Jun 30, 2009 Issued
Array ( [id] => 6322200 [patent_doc_number] => 20100326047 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2010-12-30 [patent_title] => 'SYSTEM AND METHOD FOR ASSEMBLING A THRUST REVERSER FOR A GAS TURBINE PROPULSION SYSTEM' [patent_app_type] => utility [patent_app_number] => 12/495248 [patent_app_country] => US [patent_app_date] => 2009-06-30 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 8 [patent_figures_cnt] => 8 [patent_no_of_words] => 4422 [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] => publications/A1/0326/20100326047.pdf [firstpage_image] =>[orig_patent_app_number] => 12495248 [rel_patent_id] =>[rel_patent_doc_number] =>)
12/495248
System and method for assembling a thrust reverser for a gas turbine propulsion system Jun 29, 2009 Issued
Array ( [id] => 5460293 [patent_doc_number] => 20090320493 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2009-12-31 [patent_title] => 'METHOD FOR PRIMARY CONTROL OF A COMBINED GAS AND STEAM TURBINE ARRANGEMENT' [patent_app_type] => utility [patent_app_number] => 12/492959 [patent_app_country] => US [patent_app_date] => 2009-06-26 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 5 [patent_figures_cnt] => 5 [patent_no_of_words] => 4632 [patent_no_of_claims] => 10 [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/A1/0320/20090320493.pdf [firstpage_image] =>[orig_patent_app_number] => 12492959 [rel_patent_id] =>[rel_patent_doc_number] =>)
12/492959
Method for primary control of a combined gas and steam turbine arrangement Jun 25, 2009 Issued
Array ( [id] => 9689505 [patent_doc_number] => 08820085 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2014-09-02 [patent_title] => 'Lean fuel intake gas turbine system' [patent_app_type] => utility [patent_app_number] => 12/993398 [patent_app_country] => US [patent_app_date] => 2009-06-10 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 3 [patent_figures_cnt] => 3 [patent_no_of_words] => 5476 [patent_no_of_claims] => 7 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 195 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 12993398 [rel_patent_id] =>[rel_patent_doc_number] =>)
12/993398
Lean fuel intake gas turbine system Jun 9, 2009 Issued
Array ( [id] => 6345843 [patent_doc_number] => 20100071377 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2010-03-25 [patent_title] => 'Combustor Apparatus for Use in a Gas Turbine Engine' [patent_app_type] => utility [patent_app_number] => 12/477397 [patent_app_country] => US [patent_app_date] => 2009-06-03 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 12 [patent_figures_cnt] => 12 [patent_no_of_words] => 10127 [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] => publications/A1/0071/20100071377.pdf [firstpage_image] =>[orig_patent_app_number] => 12477397 [rel_patent_id] =>[rel_patent_doc_number] =>)
12/477397
Combustor Apparatus for Use in a Gas Turbine Engine Jun 2, 2009 Abandoned
Array ( [id] => 8627762 [patent_doc_number] => 08359825 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2013-01-29 [patent_title] => 'Microjet creation and control of shock waves' [patent_app_type] => utility [patent_app_number] => 12/454587 [patent_app_country] => US [patent_app_date] => 2009-05-20 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 11 [patent_figures_cnt] => 11 [patent_no_of_words] => 4541 [patent_no_of_claims] => 2 [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] => 12454587 [rel_patent_id] =>[rel_patent_doc_number] =>)
12/454587
Microjet creation and control of shock waves May 19, 2009 Issued
Array ( [id] => 9955630 [patent_doc_number] => 09003812 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2015-04-14 [patent_title] => 'Supporting structure for a gas turbine engine' [patent_app_type] => utility [patent_app_number] => 13/319114 [patent_app_country] => US [patent_app_date] => 2009-05-08 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 5 [patent_figures_cnt] => 11 [patent_no_of_words] => 5577 [patent_no_of_claims] => 11 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 202 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13319114 [rel_patent_id] =>[rel_patent_doc_number] =>)
13/319114
Supporting structure for a gas turbine engine May 7, 2009 Issued
Array ( [id] => 8662272 [patent_doc_number] => 08375726 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2013-02-19 [patent_title] => 'Combustor assembly in a gas turbine engine' [patent_app_type] => utility [patent_app_number] => 12/431302 [patent_app_country] => US [patent_app_date] => 2009-04-28 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 3 [patent_figures_cnt] => 4 [patent_no_of_words] => 7539 [patent_no_of_claims] => 16 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 196 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 12431302 [rel_patent_id] =>[rel_patent_doc_number] =>)
12/431302
Combustor assembly in a gas turbine engine Apr 27, 2009 Issued
Array ( [id] => 9748341 [patent_doc_number] => 08839805 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2014-09-23 [patent_title] => 'Passive boundary layer bleed system for nacelle inlet airflow control' [patent_app_type] => utility [patent_app_number] => 12/428582 [patent_app_country] => US [patent_app_date] => 2009-04-23 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 2 [patent_figures_cnt] => 4 [patent_no_of_words] => 2508 [patent_no_of_claims] => 25 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 153 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 12428582 [rel_patent_id] =>[rel_patent_doc_number] =>)
12/428582
Passive boundary layer bleed system for nacelle inlet airflow control Apr 22, 2009 Issued
Array ( [id] => 6229541 [patent_doc_number] => 20100263382 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2010-10-21 [patent_title] => 'DUAL ORIFICE PILOT FUEL INJECTOR' [patent_app_type] => utility [patent_app_number] => 12/424612 [patent_app_country] => US [patent_app_date] => 2009-04-16 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 10 [patent_figures_cnt] => 10 [patent_no_of_words] => 4932 [patent_no_of_claims] => 39 [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] => publications/A1/0263/20100263382.pdf [firstpage_image] =>[orig_patent_app_number] => 12424612 [rel_patent_id] =>[rel_patent_doc_number] =>)
12/424612
DUAL ORIFICE PILOT FUEL INJECTOR Apr 15, 2009 Abandoned
Array ( [id] => 5312584 [patent_doc_number] => 20090277182 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2009-11-12 [patent_title] => 'FUEL LANCE' [patent_app_type] => utility [patent_app_number] => 12/422497 [patent_app_country] => US [patent_app_date] => 2009-04-13 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 7 [patent_figures_cnt] => 7 [patent_no_of_words] => 6430 [patent_no_of_claims] => 21 [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/A1/0277/20090277182.pdf [firstpage_image] =>[orig_patent_app_number] => 12422497 [rel_patent_id] =>[rel_patent_doc_number] =>)
12/422497
Burner and fuel lance for a gas turbine installation Apr 12, 2009 Issued
Array ( [id] => 9689512 [patent_doc_number] => 08820092 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2014-09-02 [patent_title] => 'Gas turbine engine cooling system and method' [patent_app_type] => utility [patent_app_number] => 12/937213 [patent_app_country] => US [patent_app_date] => 2009-04-09 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 12 [patent_figures_cnt] => 20 [patent_no_of_words] => 12156 [patent_no_of_claims] => 24 [patent_no_of_ind_claims] => 10 [patent_words_short_claim] => 200 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 12937213 [rel_patent_id] =>[rel_patent_doc_number] =>)
12/937213
Gas turbine engine cooling system and method Apr 8, 2009 Issued
Array ( [id] => 5468385 [patent_doc_number] => 20090241551 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2009-10-01 [patent_title] => 'Cogeneration of Hydrogen and Power' [patent_app_type] => utility [patent_app_number] => 12/410487 [patent_app_country] => US [patent_app_date] => 2009-03-25 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 6 [patent_figures_cnt] => 6 [patent_no_of_words] => 3178 [patent_no_of_claims] => 14 [patent_no_of_ind_claims] => 4 [patent_words_short_claim] => 0 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] => publications/A1/0241/20090241551.pdf [firstpage_image] =>[orig_patent_app_number] => 12410487 [rel_patent_id] =>[rel_patent_doc_number] =>)
12/410487
Cogeneration of Hydrogen and Power Mar 24, 2009 Abandoned
Array ( [id] => 9572998 [patent_doc_number] => 08763406 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2014-07-01 [patent_title] => 'Turbomachine combustion chamber' [patent_app_type] => utility [patent_app_number] => 12/918946 [patent_app_country] => US [patent_app_date] => 2009-03-06 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 2 [patent_figures_cnt] => 4 [patent_no_of_words] => 2278 [patent_no_of_claims] => 12 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 197 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 12918946 [rel_patent_id] =>[rel_patent_doc_number] =>)
12/918946
Turbomachine combustion chamber Mar 5, 2009 Issued
Array ( [id] => 5545177 [patent_doc_number] => 20090155054 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2009-06-18 [patent_title] => 'WALL STRUCTURE FOR LIMITING A HOT GAS PATH' [patent_app_type] => utility [patent_app_number] => 12/390901 [patent_app_country] => US [patent_app_date] => 2009-02-23 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 3 [patent_figures_cnt] => 3 [patent_no_of_words] => 3615 [patent_no_of_claims] => 5 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 0 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] => publications/A1/0155/20090155054.pdf [firstpage_image] =>[orig_patent_app_number] => 12390901 [rel_patent_id] =>[rel_patent_doc_number] =>)
12/390901
Wall structure for limiting a hot gas path Feb 22, 2009 Issued
Array ( [id] => 6459711 [patent_doc_number] => 20100205967 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2010-08-19 [patent_title] => 'PRE-HEATING GAS TURBINE INLET AIR USING AN EXTERNAL FIRED HEATER AND REDUCING OVERBOARD BLEED IN LOW-BTU APPLICATIONS' [patent_app_type] => utility [patent_app_number] => 12/371883 [patent_app_country] => US [patent_app_date] => 2009-02-16 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 7 [patent_figures_cnt] => 7 [patent_no_of_words] => 7391 [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] => publications/A1/0205/20100205967.pdf [firstpage_image] =>[orig_patent_app_number] => 12371883 [rel_patent_id] =>[rel_patent_doc_number] =>)
12/371883
PRE-HEATING GAS TURBINE INLET AIR USING AN EXTERNAL FIRED HEATER AND REDUCING OVERBOARD BLEED IN LOW-BTU APPLICATIONS Feb 15, 2009 Abandoned
Array ( [id] => 7794022 [patent_doc_number] => 08122726 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2012-02-28 [patent_title] => 'Combustion chamber of a combustion system' [patent_app_type] => utility [patent_app_number] => 12/367997 [patent_app_country] => US [patent_app_date] => 2009-02-09 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 2 [patent_figures_cnt] => 3 [patent_no_of_words] => 2742 [patent_no_of_claims] => 11 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 163 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/08/122/08122726.pdf [firstpage_image] =>[orig_patent_app_number] => 12367997 [rel_patent_id] =>[rel_patent_doc_number] =>)
12/367997
Combustion chamber of a combustion system Feb 8, 2009 Issued
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