
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 number | Title of the application | Filing Date | Status |
|---|---|---|---|
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
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[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
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[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
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[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
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[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
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[patent_no_of_words] => 4556
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[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
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[patent_no_of_words] => 2310
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[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
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[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
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[patent_no_of_words] => 5569
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[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
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[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
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[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
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[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
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[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 |