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] => 4684582 [patent_doc_number] => 20080028763 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2008-02-07 [patent_title] => 'Thermal management system with thrust recovery for a gas turbine engine fan nacelle assembly' [patent_app_type] => utility [patent_app_number] => 11/498848 [patent_app_country] => US [patent_app_date] => 2006-08-03 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 9 [patent_figures_cnt] => 9 [patent_no_of_words] => 2527 [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] => publications/A1/0028/20080028763.pdf [firstpage_image] =>[orig_patent_app_number] => 11498848 [rel_patent_id] =>[rel_patent_doc_number] =>)
11/498848
Thermal management system with thrust recovery for a gas turbine engine fan nacelle assembly Aug 2, 2006 Abandoned
Array ( [id] => 78082 [patent_doc_number] => 07743598 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2010-06-29 [patent_title] => 'Sealing system for the rear lubricating chamber of a jet engine' [patent_app_type] => utility [patent_app_number] => 11/461614 [patent_app_country] => US [patent_app_date] => 2006-08-01 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 1 [patent_figures_cnt] => 1 [patent_no_of_words] => 1482 [patent_no_of_claims] => 6 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 152 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/07/743/07743598.pdf [firstpage_image] =>[orig_patent_app_number] => 11461614 [rel_patent_id] =>[rel_patent_doc_number] =>)
11/461614
Sealing system for the rear lubricating chamber of a jet engine Jul 31, 2006 Issued
Array ( [id] => 5566416 [patent_doc_number] => 20090249793 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2009-10-08 [patent_title] => 'Apparatus for Modifying the Content of a Gaseous Fuel' [patent_app_type] => utility [patent_app_number] => 11/990467 [patent_app_country] => US [patent_app_date] => 2006-07-31 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 7 [patent_figures_cnt] => 7 [patent_no_of_words] => 2849 [patent_no_of_claims] => 21 [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/A1/0249/20090249793.pdf [firstpage_image] =>[orig_patent_app_number] => 11990467 [rel_patent_id] =>[rel_patent_doc_number] =>)
11/990467
Apparatus for Modifying the Content of a Gaseous Fuel Jul 30, 2006 Abandoned
Array ( [id] => 10835863 [patent_doc_number] => 08863528 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2014-10-21 [patent_title] => 'Ceramic combustor can for a gas turbine engine' [patent_app_type] => utility [patent_app_number] => 11/494083 [patent_app_country] => US [patent_app_date] => 2006-07-27 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 24 [patent_figures_cnt] => 24 [patent_no_of_words] => 3488 [patent_no_of_claims] => 13 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 123 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 11494083 [rel_patent_id] =>[rel_patent_doc_number] =>)
11/494083
Ceramic combustor can for a gas turbine engine Jul 26, 2006 Issued
Array ( [id] => 4906103 [patent_doc_number] => 20080016869 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2008-01-24 [patent_title] => 'Gas turbine internal manifold mounting arrangement' [patent_app_type] => utility [patent_app_number] => 11/488801 [patent_app_country] => US [patent_app_date] => 2006-07-19 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 6 [patent_figures_cnt] => 6 [patent_no_of_words] => 2902 [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] => publications/A1/0016/20080016869.pdf [firstpage_image] =>[orig_patent_app_number] => 11488801 [rel_patent_id] =>[rel_patent_doc_number] =>)
11/488801
Gas turbine internal manifold mounting arrangement Jul 18, 2006 Issued
Array ( [id] => 4428307 [patent_doc_number] => 07966804 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2011-06-28 [patent_title] => 'Method and apparatus for testing gas turbine engines' [patent_app_type] => utility [patent_app_number] => 11/485493 [patent_app_country] => US [patent_app_date] => 2006-07-12 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 4 [patent_figures_cnt] => 4 [patent_no_of_words] => 3225 [patent_no_of_claims] => 12 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 190 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/07/966/07966804.pdf [firstpage_image] =>[orig_patent_app_number] => 11485493 [rel_patent_id] =>[rel_patent_doc_number] =>)
11/485493
Method and apparatus for testing gas turbine engines Jul 11, 2006 Issued
Array ( [id] => 159395 [patent_doc_number] => 07669420 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2010-03-02 [patent_title] => 'Fuel injector having an annular prefilmer' [patent_app_type] => utility [patent_app_number] => 11/482718 [patent_app_country] => US [patent_app_date] => 2006-07-10 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 7 [patent_figures_cnt] => 9 [patent_no_of_words] => 4165 [patent_no_of_claims] => 11 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 168 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/07/669/07669420.pdf [firstpage_image] =>[orig_patent_app_number] => 11482718 [rel_patent_id] =>[rel_patent_doc_number] =>)
11/482718
Fuel injector having an annular prefilmer Jul 9, 2006 Issued
Array ( [id] => 4929441 [patent_doc_number] => 20080000216 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2008-01-03 [patent_title] => 'TURBOFAN ENGINE' [patent_app_type] => utility [patent_app_number] => 11/427107 [patent_app_country] => US [patent_app_date] => 2006-06-28 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 8 [patent_figures_cnt] => 8 [patent_no_of_words] => 5731 [patent_no_of_claims] => 7 [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/A1/0000/20080000216.pdf [firstpage_image] =>[orig_patent_app_number] => 11427107 [rel_patent_id] =>[rel_patent_doc_number] =>)
11/427107
Turbofan engine Jun 27, 2006 Issued
Array ( [id] => 128198 [patent_doc_number] => 07698885 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2010-04-20 [patent_title] => 'Closure and locking detection system for turbojet thrust reverser' [patent_app_type] => utility [patent_app_number] => 11/426480 [patent_app_country] => US [patent_app_date] => 2006-06-26 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 6 [patent_figures_cnt] => 11 [patent_no_of_words] => 4361 [patent_no_of_claims] => 6 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 171 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/07/698/07698885.pdf [firstpage_image] =>[orig_patent_app_number] => 11426480 [rel_patent_id] =>[rel_patent_doc_number] =>)
11/426480
Closure and locking detection system for turbojet thrust reverser Jun 25, 2006 Issued
Array ( [id] => 5227205 [patent_doc_number] => 20070289311 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2007-12-20 [patent_title] => 'Combustion apparatus using pilot fuel selected for reduced emissions' [patent_app_type] => utility [patent_app_number] => 11/454698 [patent_app_country] => US [patent_app_date] => 2006-06-16 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 2 [patent_figures_cnt] => 2 [patent_no_of_words] => 1364 [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/A1/0289/20070289311.pdf [firstpage_image] =>[orig_patent_app_number] => 11454698 [rel_patent_id] =>[rel_patent_doc_number] =>)
11/454698
Combustion apparatus using pilot fuel selected for reduced emissions Jun 15, 2006 Issued
Array ( [id] => 249623 [patent_doc_number] => 07581377 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2009-09-01 [patent_title] => 'Low-cost frangible cable for gas turbine engine' [patent_app_type] => utility [patent_app_number] => 11/452297 [patent_app_country] => US [patent_app_date] => 2006-06-14 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 3 [patent_figures_cnt] => 4 [patent_no_of_words] => 3192 [patent_no_of_claims] => 10 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 142 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/07/581/07581377.pdf [firstpage_image] =>[orig_patent_app_number] => 11452297 [rel_patent_id] =>[rel_patent_doc_number] =>)
11/452297
Low-cost frangible cable for gas turbine engine Jun 13, 2006 Issued
Array ( [id] => 5091926 [patent_doc_number] => 20070113535 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2007-05-24 [patent_title] => 'Dual-plasma-fusion jet thrusters using DC turbo-contacting generator as its electrical power source' [patent_app_type] => utility [patent_app_number] => 11/472517 [patent_app_country] => US [patent_app_date] => 2006-06-12 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 9 [patent_figures_cnt] => 9 [patent_no_of_words] => 4247 [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] => publications/A1/0113/20070113535.pdf [firstpage_image] =>[orig_patent_app_number] => 11472517 [rel_patent_id] =>[rel_patent_doc_number] =>)
11/472517
Dual-plasma-fusion jet thrusters using DC turbo-contacting generator as its electrical power source Jun 11, 2006 Abandoned
Array ( [id] => 5243404 [patent_doc_number] => 20070021899 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2007-01-25 [patent_title] => 'Method and system for operating a multi-stage combustor' [patent_app_type] => utility [patent_app_number] => 11/447893 [patent_app_country] => US [patent_app_date] => 2006-06-07 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 5 [patent_figures_cnt] => 5 [patent_no_of_words] => 4556 [patent_no_of_claims] => 11 [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/A1/0021/20070021899.pdf [firstpage_image] =>[orig_patent_app_number] => 11447893 [rel_patent_id] =>[rel_patent_doc_number] =>)
11/447893
Method and system for operating a multi-stage combustor Jun 6, 2006 Abandoned
Array ( [id] => 5081878 [patent_doc_number] => 20070271928 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2007-11-29 [patent_title] => 'Fuel heating system for turbine engines' [patent_app_type] => utility [patent_app_number] => 11/440821 [patent_app_country] => US [patent_app_date] => 2006-05-25 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 4 [patent_figures_cnt] => 4 [patent_no_of_words] => 2310 [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/A1/0271/20070271928.pdf [firstpage_image] =>[orig_patent_app_number] => 11440821 [rel_patent_id] =>[rel_patent_doc_number] =>)
11/440821
Fuel heating system for turbine engines May 24, 2006 Issued
Array ( [id] => 5167706 [patent_doc_number] => 20070068137 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2007-03-29 [patent_title] => 'Injection device for combustion chambers of liquid-fueled rocket engines' [patent_app_type] => utility [patent_app_number] => 11/438335 [patent_app_country] => US [patent_app_date] => 2006-05-23 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 2 [patent_figures_cnt] => 2 [patent_no_of_words] => 3987 [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/A1/0068/20070068137.pdf [firstpage_image] =>[orig_patent_app_number] => 11438335 [rel_patent_id] =>[rel_patent_doc_number] =>)
11/438335
Injection device for combustion chambers of liquid-fueled rocket engines May 22, 2006 Issued
Array ( [id] => 5167707 [patent_doc_number] => 20070068138 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2007-03-29 [patent_title] => 'Rocket vehicle and engine' [patent_app_type] => utility [patent_app_number] => 11/436138 [patent_app_country] => US [patent_app_date] => 2006-05-17 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 15 [patent_figures_cnt] => 15 [patent_no_of_words] => 5569 [patent_no_of_claims] => 11 [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/A1/0068/20070068138.pdf [firstpage_image] =>[orig_patent_app_number] => 11436138 [rel_patent_id] =>[rel_patent_doc_number] =>)
11/436138
Rocket vehicle and engine May 16, 2006 Abandoned
Array ( [id] => 5281313 [patent_doc_number] => 20090094986 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2009-04-16 [patent_title] => 'Combustion Chamber Wall, Gas Turbine Installation and Process for Starting or Shutting Down a Gas Turbine Installation' [patent_app_type] => utility [patent_app_number] => 11/920397 [patent_app_country] => US [patent_app_date] => 2006-05-10 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 5 [patent_figures_cnt] => 5 [patent_no_of_words] => 5109 [patent_no_of_claims] => 11 [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/A1/0094/20090094986.pdf [firstpage_image] =>[orig_patent_app_number] => 11920397 [rel_patent_id] =>[rel_patent_doc_number] =>)
11/920397
Combustion chamber wall, gas turbine installation and process for starting or shutting down a gas turbine installation May 9, 2006 Issued
Array ( [id] => 5144396 [patent_doc_number] => 20070044450 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2007-03-01 [patent_title] => 'Powder propellant-based space propulsion device' [patent_app_type] => utility [patent_app_number] => 11/431452 [patent_app_country] => US [patent_app_date] => 2006-05-09 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 10 [patent_figures_cnt] => 10 [patent_no_of_words] => 22835 [patent_no_of_claims] => 26 [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/A1/0044/20070044450.pdf [firstpage_image] =>[orig_patent_app_number] => 11431452 [rel_patent_id] =>[rel_patent_doc_number] =>)
11/431452
Powder propellant-based space propulsion device May 8, 2006 Abandoned
Array ( [id] => 5443308 [patent_doc_number] => 20090044534 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2009-02-19 [patent_title] => 'Scheme of power enhancement for combined cycle plants through steam injection' [patent_app_type] => utility [patent_app_number] => 11/920631 [patent_app_country] => US [patent_app_date] => 2006-05-09 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 4 [patent_figures_cnt] => 4 [patent_no_of_words] => 1680 [patent_no_of_claims] => 15 [patent_no_of_ind_claims] => 14 [patent_words_short_claim] => 0 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] => publications/A1/0044/20090044534.pdf [firstpage_image] =>[orig_patent_app_number] => 11920631 [rel_patent_id] =>[rel_patent_doc_number] =>)
11/920631
Scheme of power enhancement for combined cycle plants through steam injection May 8, 2006 Abandoned
Array ( [id] => 9230771 [patent_doc_number] => 08596071 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2013-12-03 [patent_title] => 'Method and apparatus for assembling a gas turbine engine' [patent_app_type] => utility [patent_app_number] => 11/418613 [patent_app_country] => US [patent_app_date] => 2006-05-05 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 4 [patent_figures_cnt] => 4 [patent_no_of_words] => 3098 [patent_no_of_claims] => 19 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 136 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 11418613 [rel_patent_id] =>[rel_patent_doc_number] =>)
11/418613
Method and apparatus for assembling a gas turbine engine May 4, 2006 Issued
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