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] => 5571880 [patent_doc_number] => 20090139239 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2009-06-04 [patent_title] => 'QUENCH JET ARRANGEMENT FOR ANNULAR RICH-QUENCH-LEAN GAS TURBINE COMBUSTORS' [patent_app_type] => utility [patent_app_number] => 11/947337 [patent_app_country] => US [patent_app_date] => 2007-11-29 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 4 [patent_figures_cnt] => 4 [patent_no_of_words] => 3267 [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/A1/0139/20090139239.pdf [firstpage_image] =>[orig_patent_app_number] => 11947337 [rel_patent_id] =>[rel_patent_doc_number] =>)
11/947337
Quench jet arrangement for annular rich-quench-lean gas turbine combustors Nov 28, 2007 Issued
Array ( [id] => 9284121 [patent_doc_number] => 08640439 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2014-02-04 [patent_title] => 'Hybrid drive for an aircraft' [patent_app_type] => utility [patent_app_number] => 11/998437 [patent_app_country] => US [patent_app_date] => 2007-11-29 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 3 [patent_figures_cnt] => 3 [patent_no_of_words] => 3601 [patent_no_of_claims] => 6 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 171 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 11998437 [rel_patent_id] =>[rel_patent_doc_number] =>)
11/998437
Hybrid drive for an aircraft Nov 28, 2007 Issued
Array ( [id] => 4900764 [patent_doc_number] => 20080110175 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2008-05-15 [patent_title] => 'Cowling for connecting a hot gas source to a stirling engine or a turbine' [patent_app_type] => utility [patent_app_number] => 11/983517 [patent_app_country] => US [patent_app_date] => 2007-11-10 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 10 [patent_figures_cnt] => 10 [patent_no_of_words] => 5488 [patent_no_of_claims] => 27 [patent_no_of_ind_claims] => 5 [patent_words_short_claim] => 0 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] => publications/A1/0110/20080110175.pdf [firstpage_image] =>[orig_patent_app_number] => 11983517 [rel_patent_id] =>[rel_patent_doc_number] =>)
11/983517
Cowling for connecting a hot gas source to a stirling engine or a turbine Nov 9, 2007 Abandoned
Array ( [id] => 6548843 [patent_doc_number] => 20100058730 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2010-03-11 [patent_title] => 'GAS TURBINE POWER GENERATION SYSTEM AND METHOD OF DETECTING CALORIFIC ABNORMALITY OF THE SAME' [patent_app_type] => utility [patent_app_number] => 12/306832 [patent_app_country] => US [patent_app_date] => 2007-11-09 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 16 [patent_figures_cnt] => 16 [patent_no_of_words] => 8573 [patent_no_of_claims] => 9 [patent_no_of_ind_claims] => 6 [patent_words_short_claim] => 0 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] => publications/A1/0058/20100058730.pdf [firstpage_image] =>[orig_patent_app_number] => 12306832 [rel_patent_id] =>[rel_patent_doc_number] =>)
12/306832
GAS TURBINE POWER GENERATION SYSTEM AND METHOD OF DETECTING CALORIFIC ABNORMALITY OF THE SAME Nov 8, 2007 Abandoned
Array ( [id] => 5262055 [patent_doc_number] => 20090114740 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2009-05-07 [patent_title] => 'NOZZLE ASSEMBLY WITH FLOW CONDUITS' [patent_app_type] => utility [patent_app_number] => 11/933537 [patent_app_country] => US [patent_app_date] => 2007-11-01 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 3 [patent_figures_cnt] => 3 [patent_no_of_words] => 1283 [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/A1/0114/20090114740.pdf [firstpage_image] =>[orig_patent_app_number] => 11933537 [rel_patent_id] =>[rel_patent_doc_number] =>)
11/933537
Nozzle assembly with flow conduits Oct 31, 2007 Issued
Array ( [id] => 5298834 [patent_doc_number] => 20090293486 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2009-12-03 [patent_title] => 'COMBUSTORS WITH IGNITERS HAVING PROTRUSIONS' [patent_app_type] => utility [patent_app_number] => 11/925347 [patent_app_country] => US [patent_app_date] => 2007-10-26 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 3 [patent_figures_cnt] => 3 [patent_no_of_words] => 2685 [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/A1/0293/20090293486.pdf [firstpage_image] =>[orig_patent_app_number] => 11925347 [rel_patent_id] =>[rel_patent_doc_number] =>)
11/925347
COMBUSTORS WITH IGNITERS HAVING PROTRUSIONS Oct 25, 2007 Abandoned
Array ( [id] => 8338203 [patent_doc_number] => 08240120 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2012-08-14 [patent_title] => 'Vibration management for gas turbine engines' [patent_app_type] => utility [patent_app_number] => 11/923897 [patent_app_country] => US [patent_app_date] => 2007-10-25 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 3 [patent_figures_cnt] => 4 [patent_no_of_words] => 2672 [patent_no_of_claims] => 17 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 132 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 11923897 [rel_patent_id] =>[rel_patent_doc_number] =>)
11/923897
Vibration management for gas turbine engines Oct 24, 2007 Issued
Array ( [id] => 9993811 [patent_doc_number] => 09038392 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2015-05-26 [patent_title] => 'Gas turbine combustor' [patent_app_type] => utility [patent_app_number] => 12/446402 [patent_app_country] => US [patent_app_date] => 2007-10-17 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 11 [patent_figures_cnt] => 18 [patent_no_of_words] => 5067 [patent_no_of_claims] => 9 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 303 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 12446402 [rel_patent_id] =>[rel_patent_doc_number] =>)
12/446402
Gas turbine combustor Oct 16, 2007 Issued
Array ( [id] => 5406197 [patent_doc_number] => 20090120095 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2009-05-14 [patent_title] => 'Combustion liner thimble insert and related method' [patent_app_type] => utility [patent_app_number] => 11/907332 [patent_app_country] => US [patent_app_date] => 2007-10-11 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 5 [patent_figures_cnt] => 5 [patent_no_of_words] => 2268 [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/A1/0120/20090120095.pdf [firstpage_image] =>[orig_patent_app_number] => 11907332 [rel_patent_id] =>[rel_patent_doc_number] =>)
11/907332
Combustion liner thimble insert and related method Oct 10, 2007 Issued
Array ( [id] => 4731473 [patent_doc_number] => 20080048451 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2008-02-28 [patent_title] => 'TURBINE INSTALLATION HAVING A CONNECTABLE AUXILIARY GROUP' [patent_app_type] => utility [patent_app_number] => 11/863617 [patent_app_country] => US [patent_app_date] => 2007-09-28 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 11 [patent_figures_cnt] => 11 [patent_no_of_words] => 10784 [patent_no_of_claims] => 25 [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/A1/0048/20080048451.pdf [firstpage_image] =>[orig_patent_app_number] => 11863617 [rel_patent_id] =>[rel_patent_doc_number] =>)
11/863617
Turbine installation having a connectable auxiliary group Sep 27, 2007 Issued
Array ( [id] => 8537011 [patent_doc_number] => 08312727 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2012-11-20 [patent_title] => 'Vibration damper' [patent_app_type] => utility [patent_app_number] => 11/862163 [patent_app_country] => US [patent_app_date] => 2007-09-26 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 7 [patent_figures_cnt] => 8 [patent_no_of_words] => 4695 [patent_no_of_claims] => 11 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 138 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 11862163 [rel_patent_id] =>[rel_patent_doc_number] =>)
11/862163
Vibration damper Sep 25, 2007 Issued
Array ( [id] => 5504766 [patent_doc_number] => 20090077972 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2009-03-26 [patent_title] => 'TOROIDAL RING MANIFOLD FOR SECONDARY FUEL NOZZLE OF A DLN GAS TURBINE' [patent_app_type] => utility [patent_app_number] => 11/859087 [patent_app_country] => US [patent_app_date] => 2007-09-21 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 11 [patent_figures_cnt] => 11 [patent_no_of_words] => 5646 [patent_no_of_claims] => 20 [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/A1/0077/20090077972.pdf [firstpage_image] =>[orig_patent_app_number] => 11859087 [rel_patent_id] =>[rel_patent_doc_number] =>)
11/859087
TOROIDAL RING MANIFOLD FOR SECONDARY FUEL NOZZLE OF A DLN GAS TURBINE Sep 20, 2007 Abandoned
Array ( [id] => 4935260 [patent_doc_number] => 20080072572 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2008-03-27 [patent_title] => 'TURBOMACHINE FAN DUCT' [patent_app_type] => utility [patent_app_number] => 11/856297 [patent_app_country] => US [patent_app_date] => 2007-09-17 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 6 [patent_figures_cnt] => 6 [patent_no_of_words] => 3409 [patent_no_of_claims] => 14 [patent_no_of_ind_claims] => 7 [patent_words_short_claim] => 0 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] => publications/A1/0072/20080072572.pdf [firstpage_image] =>[orig_patent_app_number] => 11856297 [rel_patent_id] =>[rel_patent_doc_number] =>)
11/856297
Turbomachine fan duct Sep 16, 2007 Issued
Array ( [id] => 5281312 [patent_doc_number] => 20090094985 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2009-04-16 [patent_title] => 'Non-Rectangular Resonator Devices Providing Enhanced Liner Cooling for Combustion Chamber' [patent_app_type] => utility [patent_app_number] => 11/855747 [patent_app_country] => US [patent_app_date] => 2007-09-14 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 6 [patent_figures_cnt] => 6 [patent_no_of_words] => 5912 [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/A1/0094/20090094985.pdf [firstpage_image] =>[orig_patent_app_number] => 11855747 [rel_patent_id] =>[rel_patent_doc_number] =>)
11/855747
Non-rectangular resonator devices providing enhanced liner cooling for combustion chamber Sep 13, 2007 Issued
Array ( [id] => 4929439 [patent_doc_number] => 20080000214 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2008-01-03 [patent_title] => 'METHOD FOR TUNING VALVES FOR PRIMARY AND SECONDARY FUEL CIRCUIT' [patent_app_type] => utility [patent_app_number] => 11/855638 [patent_app_country] => US [patent_app_date] => 2007-09-14 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 6 [patent_figures_cnt] => 6 [patent_no_of_words] => 7369 [patent_no_of_claims] => 23 [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/A1/0000/20080000214.pdf [firstpage_image] =>[orig_patent_app_number] => 11855638 [rel_patent_id] =>[rel_patent_doc_number] =>)
11/855638
Method for tuning valves for primary and secondary fuel circuit Sep 13, 2007 Issued
Array ( [id] => 5448619 [patent_doc_number] => 20090064654 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2009-03-12 [patent_title] => 'Turbine engine with modulated combustion and reheat chambers' [patent_app_type] => utility [patent_app_number] => 11/898257 [patent_app_country] => US [patent_app_date] => 2007-09-11 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 2 [patent_figures_cnt] => 2 [patent_no_of_words] => 1779 [patent_no_of_claims] => 19 [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/A1/0064/20090064654.pdf [firstpage_image] =>[orig_patent_app_number] => 11898257 [rel_patent_id] =>[rel_patent_doc_number] =>)
11/898257
Turbine engine with modulated combustion and reheat chambers Sep 10, 2007 Abandoned
Array ( [id] => 9480735 [patent_doc_number] => 08726675 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2014-05-20 [patent_title] => 'Scalloped flexure ring' [patent_app_type] => utility [patent_app_number] => 11/851667 [patent_app_country] => US [patent_app_date] => 2007-09-07 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 4 [patent_figures_cnt] => 9 [patent_no_of_words] => 2330 [patent_no_of_claims] => 20 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 152 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 11851667 [rel_patent_id] =>[rel_patent_doc_number] =>)
11/851667
Scalloped flexure ring Sep 6, 2007 Issued
Array ( [id] => 4603629 [patent_doc_number] => 07984607 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2011-07-26 [patent_title] => 'Gas turbine engine systems and related methods involving vane-blade count ratios greater than unity' [patent_app_type] => utility [patent_app_number] => 11/850787 [patent_app_country] => US [patent_app_date] => 2007-09-06 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 3 [patent_figures_cnt] => 4 [patent_no_of_words] => 2156 [patent_no_of_claims] => 8 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 81 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/07/984/07984607.pdf [firstpage_image] =>[orig_patent_app_number] => 11850787 [rel_patent_id] =>[rel_patent_doc_number] =>)
11/850787
Gas turbine engine systems and related methods involving vane-blade count ratios greater than unity Sep 5, 2007 Issued
Array ( [id] => 5318352 [patent_doc_number] => 20090056342 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2009-03-05 [patent_title] => 'Methods and Systems for Gas Turbine Part-Load Operating Conditions' [patent_app_type] => utility [patent_app_number] => 11/849383 [patent_app_country] => US [patent_app_date] => 2007-09-04 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 3 [patent_figures_cnt] => 3 [patent_no_of_words] => 2126 [patent_no_of_claims] => 21 [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/A1/0056/20090056342.pdf [firstpage_image] =>[orig_patent_app_number] => 11849383 [rel_patent_id] =>[rel_patent_doc_number] =>)
11/849383
Methods and Systems for Gas Turbine Part-Load Operating Conditions Sep 3, 2007 Abandoned
Array ( [id] => 4632743 [patent_doc_number] => 08011188 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2011-09-06 [patent_title] => 'Augmentor with trapped vortex cavity pilot' [patent_app_type] => utility [patent_app_number] => 11/848587 [patent_app_country] => US [patent_app_date] => 2007-08-31 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 13 [patent_figures_cnt] => 14 [patent_no_of_words] => 5066 [patent_no_of_claims] => 29 [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] => patents/08/011/08011188.pdf [firstpage_image] =>[orig_patent_app_number] => 11848587 [rel_patent_id] =>[rel_patent_doc_number] =>)
11/848587
Augmentor with trapped vortex cavity pilot Aug 30, 2007 Issued
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