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] => 8425239 [patent_doc_number] => 20120247114 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2012-10-04 [patent_title] => 'Water Cooling System For Intercooled Turbines' [patent_app_type] => utility [patent_app_number] => 13/076200 [patent_app_country] => US [patent_app_date] => 2011-03-30 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 15 [patent_figures_cnt] => 15 [patent_no_of_words] => 5909 [patent_no_of_claims] => 36 [patent_no_of_ind_claims] => 10 [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] => 13076200 [rel_patent_id] =>[rel_patent_doc_number] =>)
13/076200
Water Cooling System For Intercooled Turbines Mar 29, 2011 Abandoned
Array ( [id] => 8414061 [patent_doc_number] => 20120241561 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2012-09-27 [patent_title] => 'METHOD AND APPARATUS FOR PROTECTING AIRCRAFT AND AIRCRAFT ENGINES AGAINST ICING' [patent_app_type] => utility [patent_app_number] => 13/076038 [patent_app_country] => US [patent_app_date] => 2011-03-30 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 7 [patent_figures_cnt] => 7 [patent_no_of_words] => 3754 [patent_no_of_claims] => 19 [patent_no_of_ind_claims] => 15 [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] => 13076038 [rel_patent_id] =>[rel_patent_doc_number] =>)
13/076038
METHOD AND APPARATUS FOR PROTECTING AIRCRAFT AND AIRCRAFT ENGINES AGAINST ICING Mar 29, 2011 Abandoned
13/071060 APPARATUS FOR PROTECTING AIRCRAFT ENGINES AGAINST ICING Mar 23, 2011 Abandoned
Array ( [id] => 10868278 [patent_doc_number] => 08893466 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2014-11-25 [patent_title] => 'Dual pump fuel flow system for a gas turbine engine and method of controlling' [patent_app_type] => utility [patent_app_number] => 13/051091 [patent_app_country] => US [patent_app_date] => 2011-03-18 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 3 [patent_figures_cnt] => 3 [patent_no_of_words] => 4625 [patent_no_of_claims] => 9 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 347 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13051091 [rel_patent_id] =>[rel_patent_doc_number] =>)
13/051091
Dual pump fuel flow system for a gas turbine engine and method of controlling Mar 17, 2011 Issued
Array ( [id] => 6009345 [patent_doc_number] => 20110219742 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2011-09-15 [patent_title] => 'SUPERSONIC COMBUSTOR ROCKET NOZZLE' [patent_app_type] => utility [patent_app_number] => 13/047663 [patent_app_country] => US [patent_app_date] => 2011-03-14 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 6 [patent_figures_cnt] => 6 [patent_no_of_words] => 5625 [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/A1/0219/20110219742.pdf [firstpage_image] =>[orig_patent_app_number] => 13047663 [rel_patent_id] =>[rel_patent_doc_number] =>)
13/047663
SUPERSONIC COMBUSTOR ROCKET NOZZLE Mar 13, 2011 Abandoned
Array ( [id] => 9879905 [patent_doc_number] => RE045396 [patent_country] => US [patent_kind] => E1 [patent_issue_date] => 2015-03-03 [patent_title] => 'Wave rotor apparatus' [patent_app_type] => reissue [patent_app_number] => 13/023568 [patent_app_country] => US [patent_app_date] => 2011-03-01 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 26 [patent_figures_cnt] => 29 [patent_no_of_words] => 7503 [patent_no_of_claims] => 121 [patent_no_of_ind_claims] => 16 [patent_words_short_claim] => 44 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13023568 [rel_patent_id] =>[rel_patent_doc_number] =>)
13/023568
Wave rotor apparatus Feb 28, 2011 Issued
Array ( [id] => 7700642 [patent_doc_number] => 20110225948 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2011-09-22 [patent_title] => 'APPARATUS FOR HIGH-FREQUENCY ELECTROMAGNETIC INITIATION OF A COMBUSTION PROCESS' [patent_app_type] => utility [patent_app_number] => 13/036040 [patent_app_country] => US [patent_app_date] => 2011-02-28 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 6 [patent_figures_cnt] => 6 [patent_no_of_words] => 5007 [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/A1/0225/20110225948.pdf [firstpage_image] =>[orig_patent_app_number] => 13036040 [rel_patent_id] =>[rel_patent_doc_number] =>)
13/036040
APPARATUS FOR HIGH-FREQUENCY ELECTROMAGNETIC INITIATION OF A COMBUSTION PROCESS Feb 27, 2011 Abandoned
Array ( [id] => 8332151 [patent_doc_number] => 20120198854 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2012-08-09 [patent_title] => 'RESONATOR SYSTEM WITH ENHANCED COMBUSTOR LINER COOLING' [patent_app_type] => utility [patent_app_number] => 13/023710 [patent_app_country] => US [patent_app_date] => 2011-02-09 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 8 [patent_figures_cnt] => 8 [patent_no_of_words] => 6537 [patent_no_of_claims] => 20 [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] => 13023710 [rel_patent_id] =>[rel_patent_doc_number] =>)
13/023710
Resonator system with enhanced combustor liner cooling Feb 8, 2011 Issued
Array ( [id] => 6109820 [patent_doc_number] => 20110188989 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2011-08-04 [patent_title] => 'EXHAUST EDUCTOR SYSTEM WITH A RECIRCULATION BAFFLE' [patent_app_type] => utility [patent_app_number] => 13/018931 [patent_app_country] => US [patent_app_date] => 2011-02-01 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 3 [patent_figures_cnt] => 3 [patent_no_of_words] => 2039 [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/A1/0188/20110188989.pdf [firstpage_image] =>[orig_patent_app_number] => 13018931 [rel_patent_id] =>[rel_patent_doc_number] =>)
13/018931
Exhaust eductor system with a recirculation baffle Jan 31, 2011 Issued
Array ( [id] => 9975515 [patent_doc_number] => 09021815 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2015-05-05 [patent_title] => 'Gas turbine combustion device' [patent_app_type] => utility [patent_app_number] => 13/015910 [patent_app_country] => US [patent_app_date] => 2011-01-28 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 3 [patent_figures_cnt] => 11 [patent_no_of_words] => 1883 [patent_no_of_claims] => 16 [patent_no_of_ind_claims] => 1 [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] => 13015910 [rel_patent_id] =>[rel_patent_doc_number] =>)
13/015910
Gas turbine combustion device Jan 27, 2011 Issued
Array ( [id] => 7582974 [patent_doc_number] => 20110277484 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2011-11-17 [patent_title] => 'SYSTEM AND METHOD FOR VENTILATING A TURBINE' [patent_app_type] => utility [patent_app_number] => 13/013172 [patent_app_country] => US [patent_app_date] => 2011-01-25 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 2 [patent_figures_cnt] => 2 [patent_no_of_words] => 2547 [patent_no_of_claims] => 10 [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/A1/0277/20110277484.pdf [firstpage_image] =>[orig_patent_app_number] => 13013172 [rel_patent_id] =>[rel_patent_doc_number] =>)
13/013172
System and method for ventilating a turbine Jan 24, 2011 Issued
Array ( [id] => 5953947 [patent_doc_number] => 20110179767 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2011-07-28 [patent_title] => 'COOLING DEVICE FOR AIRCRAFT PROPELLER' [patent_app_type] => utility [patent_app_number] => 13/013319 [patent_app_country] => US [patent_app_date] => 2011-01-25 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 9 [patent_figures_cnt] => 9 [patent_no_of_words] => 6427 [patent_no_of_claims] => 9 [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/A1/0179/20110179767.pdf [firstpage_image] =>[orig_patent_app_number] => 13013319 [rel_patent_id] =>[rel_patent_doc_number] =>)
13/013319
COOLING DEVICE FOR AIRCRAFT PROPELLER Jan 24, 2011 Abandoned
Array ( [id] => 8309239 [patent_doc_number] => 20120186262 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2012-07-26 [patent_title] => 'GAS TURBINE COMBUSTOR AND METHOD FOR OPERATING' [patent_app_type] => utility [patent_app_number] => 13/012212 [patent_app_country] => US [patent_app_date] => 2011-01-24 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 4 [patent_figures_cnt] => 4 [patent_no_of_words] => 4581 [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] => 13012212 [rel_patent_id] =>[rel_patent_doc_number] =>)
13/012212
Axial stage combustor for gas turbine engines Jan 23, 2011 Issued
Array ( [id] => 10835860 [patent_doc_number] => 08863525 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2014-10-21 [patent_title] => 'Combustor with fuel staggering for flame holding mitigation' [patent_app_type] => utility [patent_app_number] => 12/983342 [patent_app_country] => US [patent_app_date] => 2011-01-03 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 4 [patent_figures_cnt] => 6 [patent_no_of_words] => 2635 [patent_no_of_claims] => 10 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 175 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 12983342 [rel_patent_id] =>[rel_patent_doc_number] =>)
12/983342
Combustor with fuel staggering for flame holding mitigation Jan 2, 2011 Issued
Array ( [id] => 8273700 [patent_doc_number] => 20120167576 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2012-07-05 [patent_title] => 'METHOD AND SYSTEM FOR POWERING A VEHICLE' [patent_app_type] => utility [patent_app_number] => 12/981044 [patent_app_country] => US [patent_app_date] => 2010-12-29 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 3 [patent_figures_cnt] => 3 [patent_no_of_words] => 1858 [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] => 12981044 [rel_patent_id] =>[rel_patent_doc_number] =>)
12/981044
System for powering a vehicle Dec 28, 2010 Issued
Array ( [id] => 11613113 [patent_doc_number] => 09650964 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2017-05-16 [patent_title] => 'Accessory gearbox with a starter/generator' [patent_app_type] => utility [patent_app_number] => 12/979579 [patent_app_country] => US [patent_app_date] => 2010-12-28 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 4 [patent_figures_cnt] => 4 [patent_no_of_words] => 3947 [patent_no_of_claims] => 13 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 256 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 12979579 [rel_patent_id] =>[rel_patent_doc_number] =>)
12/979579
Accessory gearbox with a starter/generator Dec 27, 2010 Issued
Array ( [id] => 9646290 [patent_doc_number] => 08800294 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2014-08-12 [patent_title] => 'Integrated aero-engine flowpath structure' [patent_app_type] => utility [patent_app_number] => 12/978954 [patent_app_country] => US [patent_app_date] => 2010-12-27 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 2 [patent_figures_cnt] => 5 [patent_no_of_words] => 4175 [patent_no_of_claims] => 14 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 147 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 12978954 [rel_patent_id] =>[rel_patent_doc_number] =>)
12/978954
Integrated aero-engine flowpath structure Dec 26, 2010 Issued
Array ( [id] => 9646290 [patent_doc_number] => 08800294 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2014-08-12 [patent_title] => 'Integrated aero-engine flowpath structure' [patent_app_type] => utility [patent_app_number] => 12/978954 [patent_app_country] => US [patent_app_date] => 2010-12-27 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 2 [patent_figures_cnt] => 5 [patent_no_of_words] => 4175 [patent_no_of_claims] => 14 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 147 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 12978954 [rel_patent_id] =>[rel_patent_doc_number] =>)
12/978954
Integrated aero-engine flowpath structure Dec 26, 2010 Issued
Array ( [id] => 9646290 [patent_doc_number] => 08800294 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2014-08-12 [patent_title] => 'Integrated aero-engine flowpath structure' [patent_app_type] => utility [patent_app_number] => 12/978954 [patent_app_country] => US [patent_app_date] => 2010-12-27 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 2 [patent_figures_cnt] => 5 [patent_no_of_words] => 4175 [patent_no_of_claims] => 14 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 147 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 12978954 [rel_patent_id] =>[rel_patent_doc_number] =>)
12/978954
Integrated aero-engine flowpath structure Dec 26, 2010 Issued
Array ( [id] => 9646290 [patent_doc_number] => 08800294 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2014-08-12 [patent_title] => 'Integrated aero-engine flowpath structure' [patent_app_type] => utility [patent_app_number] => 12/978954 [patent_app_country] => US [patent_app_date] => 2010-12-27 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 2 [patent_figures_cnt] => 5 [patent_no_of_words] => 4175 [patent_no_of_claims] => 14 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 147 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 12978954 [rel_patent_id] =>[rel_patent_doc_number] =>)
12/978954
Integrated aero-engine flowpath structure Dec 26, 2010 Issued
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