
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] => 6499612
[patent_doc_number] => 20100012750
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2010-01-21
[patent_title] => 'FUEL NOZZLE CENTERBODY AND METHOD OF ASSEMBLING THE SAME'
[patent_app_type] => utility
[patent_app_number] => 12/176898
[patent_app_country] => US
[patent_app_date] => 2008-07-21
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 10
[patent_figures_cnt] => 10
[patent_no_of_words] => 4715
[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/A1/0012/20100012750.pdf
[firstpage_image] =>[orig_patent_app_number] => 12176898
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/176898 | Fuel nozzle centerbody and method of assembling the same | Jul 20, 2008 | Issued |
Array
(
[id] => 6490044
[patent_doc_number] => 20100011742
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2010-01-21
[patent_title] => 'Rocket Motor Containing Multiple Pellet Cells'
[patent_app_type] => utility
[patent_app_number] => 12/175303
[patent_app_country] => US
[patent_app_date] => 2008-07-17
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 11
[patent_figures_cnt] => 11
[patent_no_of_words] => 5275
[patent_no_of_claims] => 22
[patent_no_of_ind_claims] => 4
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[patent_maintenance] => 1
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[pdf_file] => publications/A1/0011/20100011742.pdf
[firstpage_image] =>[orig_patent_app_number] => 12175303
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/175303 | Rocket Motor Containing Multiple Pellet Cells | Jul 16, 2008 | Abandoned |
Array
(
[id] => 6490277
[patent_doc_number] => 20100011769
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2010-01-21
[patent_title] => 'FORWARD-SECTION RESONATOR FOR HIGH FREQUENCY DYNAMIC DAMPING'
[patent_app_type] => utility
[patent_app_number] => 12/174187
[patent_app_country] => US
[patent_app_date] => 2008-07-16
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 8
[patent_figures_cnt] => 8
[patent_no_of_words] => 3758
[patent_no_of_claims] => 15
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[pdf_file] => publications/A1/0011/20100011769.pdf
[firstpage_image] =>[orig_patent_app_number] => 12174187
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/174187 | Forward-section resonator for high frequency dynamic damping | Jul 15, 2008 | Issued |
Array
(
[id] => 6423122
[patent_doc_number] => 20100186417
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2010-07-29
[patent_title] => 'USE OF INERT GASES FOR SHIELDING OXIDIZER AND FUEL'
[patent_app_type] => utility
[patent_app_number] => 12/665970
[patent_app_country] => US
[patent_app_date] => 2008-07-03
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 2
[patent_figures_cnt] => 2
[patent_no_of_words] => 2032
[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/A1/0186/20100186417.pdf
[firstpage_image] =>[orig_patent_app_number] => 12665970
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/665970 | USE OF INERT GASES FOR SHIELDING OXIDIZER AND FUEL | Jul 2, 2008 | Abandoned |
Array
(
[id] => 9243267
[patent_doc_number] => 08607542
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2013-12-17
[patent_title] => 'Valveless pulse combustor'
[patent_app_type] => utility
[patent_app_number] => 12/143907
[patent_app_country] => US
[patent_app_date] => 2008-06-23
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 7
[patent_no_of_words] => 3948
[patent_no_of_claims] => 28
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[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 12143907
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/143907 | Valveless pulse combustor | Jun 22, 2008 | Issued |
Array
(
[id] => 8992916
[patent_doc_number] => 08516788
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2013-08-27
[patent_title] => 'Pulse detonation engine operating with an air-fuel mixture'
[patent_app_type] => utility
[patent_app_number] => 12/667486
[patent_app_country] => US
[patent_app_date] => 2008-06-19
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 2
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[patent_no_of_words] => 2784
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[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 12667486
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/667486 | Pulse detonation engine operating with an air-fuel mixture | Jun 18, 2008 | Issued |
Array
(
[id] => 9586996
[patent_doc_number] => 08776527
[patent_country] => US
[patent_kind] => B1
[patent_issue_date] => 2014-07-15
[patent_title] => 'Techniques to reduce infrared detection of a gas turbine engine'
[patent_app_type] => utility
[patent_app_number] => 12/214269
[patent_app_country] => US
[patent_app_date] => 2008-06-17
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 6
[patent_figures_cnt] => 6
[patent_no_of_words] => 6086
[patent_no_of_claims] => 28
[patent_no_of_ind_claims] => 4
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[patent_maintenance] => 1
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[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 12214269
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/214269 | Techniques to reduce infrared detection of a gas turbine engine | Jun 16, 2008 | Issued |
Array
(
[id] => 5370492
[patent_doc_number] => 20090308051
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2009-12-17
[patent_title] => 'HEAT EXCHANGER TUBE AND AIR-TO-AIR INTERCOOLER'
[patent_app_type] => utility
[patent_app_number] => 12/137037
[patent_app_country] => US
[patent_app_date] => 2008-06-11
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 6
[patent_figures_cnt] => 6
[patent_no_of_words] => 1845
[patent_no_of_claims] => 15
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 0
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[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0308/20090308051.pdf
[firstpage_image] =>[orig_patent_app_number] => 12137037
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/137037 | HEAT EXCHANGER TUBE AND AIR-TO-AIR INTERCOOLER | Jun 10, 2008 | Abandoned |
Array
(
[id] => 5363519
[patent_doc_number] => 20090301078
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2009-12-10
[patent_title] => 'SYSTEM FOR RECOVERING THE WASTE HEAT GENERATED BY AN AUXILIARY SYSTEM OF A TURBOMACHINE'
[patent_app_type] => utility
[patent_app_number] => 12/136337
[patent_app_country] => US
[patent_app_date] => 2008-06-10
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 3
[patent_no_of_words] => 2749
[patent_no_of_claims] => 19
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[pdf_file] => publications/A1/0301/20090301078.pdf
[firstpage_image] =>[orig_patent_app_number] => 12136337
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/136337 | SYSTEM FOR RECOVERING THE WASTE HEAT GENERATED BY AN AUXILIARY SYSTEM OF A TURBOMACHINE | Jun 9, 2008 | Abandoned |
Array
(
[id] => 8304066
[patent_doc_number] => 08225592
[patent_country] => US
[patent_kind] => B1
[patent_issue_date] => 2012-07-24
[patent_title] => 'Microjet noise suppression system for jet engines'
[patent_app_type] => utility
[patent_app_number] => 12/157332
[patent_app_country] => US
[patent_app_date] => 2008-06-09
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 6
[patent_figures_cnt] => 6
[patent_no_of_words] => 2879
[patent_no_of_claims] => 10
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 277
[patent_maintenance] => 1
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[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 12157332
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/157332 | Microjet noise suppression system for jet engines | Jun 8, 2008 | Issued |
Array
(
[id] => 5407597
[patent_doc_number] => 20090121495
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2009-05-14
[patent_title] => 'Combined cycle power plant'
[patent_app_type] => utility
[patent_app_number] => 12/157067
[patent_app_country] => US
[patent_app_date] => 2008-06-06
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
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[patent_no_of_words] => 12690
[patent_no_of_claims] => 48
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[pdf_file] => publications/A1/0121/20090121495.pdf
[firstpage_image] =>[orig_patent_app_number] => 12157067
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/157067 | Combined cycle power plant | Jun 5, 2008 | Issued |
Array
(
[id] => 5363496
[patent_doc_number] => 20090301055
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2009-12-10
[patent_title] => 'Gas Turbine Engine Systems and Methods Involving Vibration Monitoring'
[patent_app_type] => utility
[patent_app_number] => 12/132847
[patent_app_country] => US
[patent_app_date] => 2008-06-04
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 6
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[pdf_file] => publications/A1/0301/20090301055.pdf
[firstpage_image] =>[orig_patent_app_number] => 12132847
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/132847 | Gas Turbine Engine Systems and Methods Involving Vibration Monitoring | Jun 3, 2008 | Abandoned |
Array
(
[id] => 7799260
[patent_doc_number] => 08127525
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2012-03-06
[patent_title] => 'System for dissipating energy in the event of a turbine shaft breaking in a gas turbine engine'
[patent_app_type] => utility
[patent_app_number] => 12/126407
[patent_app_country] => US
[patent_app_date] => 2008-05-23
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[pdf_file] => patents/08/127/08127525.pdf
[firstpage_image] =>[orig_patent_app_number] => 12126407
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/126407 | System for dissipating energy in the event of a turbine shaft breaking in a gas turbine engine | May 22, 2008 | Issued |
Array
(
[id] => 6482682
[patent_doc_number] => 20100199627
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2010-08-12
[patent_title] => 'Gas Turbo Set and Method for Controlling a Gas Turbo Set'
[patent_app_type] => utility
[patent_app_number] => 12/601055
[patent_app_country] => US
[patent_app_date] => 2008-05-16
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 2
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[pdf_file] => publications/A1/0199/20100199627.pdf
[firstpage_image] =>[orig_patent_app_number] => 12601055
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/601055 | Gas turbo set and method for controlling a gas turbo set | May 15, 2008 | Issued |
Array
(
[id] => 6497009
[patent_doc_number] => 20100218481
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2010-09-02
[patent_title] => 'TWO-PULSE ROCKET MOTOR'
[patent_app_type] => utility
[patent_app_number] => 12/599874
[patent_app_country] => US
[patent_app_date] => 2008-05-09
[patent_effective_date] => 0000-00-00
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[pdf_file] => publications/A1/0218/20100218481.pdf
[firstpage_image] =>[orig_patent_app_number] => 12599874
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/599874 | Two-pulse rocket motor | May 8, 2008 | Issued |
Array
(
[id] => 6236873
[patent_doc_number] => 20100132330
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2010-06-03
[patent_title] => 'METHOD AND APPARATUS FOR SUPPRESSING AEROENGINE CONTRAILS'
[patent_app_type] => utility
[patent_app_number] => 12/451503
[patent_app_country] => US
[patent_app_date] => 2008-04-28
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
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[patent_no_of_words] => 3002
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[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0132/20100132330.pdf
[firstpage_image] =>[orig_patent_app_number] => 12451503
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/451503 | Method and apparatus for suppressing aeroengine contrails | Apr 27, 2008 | Issued |
Array
(
[id] => 5455116
[patent_doc_number] => 20090255268
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2009-10-15
[patent_title] => 'Divergent cooling thimbles for combustor liners and related method'
[patent_app_type] => utility
[patent_app_number] => 12/081167
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[patent_app_date] => 2008-04-11
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[rel_patent_id] =>[rel_patent_doc_number] =>) 12/081167 | Divergent cooling thimbles for combustor liners and related method | Apr 10, 2008 | Abandoned |
Array
(
[id] => 9164646
[patent_doc_number] => 08590316
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[patent_kind] => B2
[patent_issue_date] => 2013-11-26
[patent_title] => 'CMC mixer with structural outer cowling'
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[patent_app_number] => 12/594874
[patent_app_country] => US
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[rel_patent_id] =>[rel_patent_doc_number] =>) 12/594874 | CMC mixer with structural outer cowling | Apr 7, 2008 | Issued |
Array
(
[id] => 5468381
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[patent_kind] => A1
[patent_issue_date] => 2009-10-01
[patent_title] => 'Gas turbine fuel injector for lower heating capacity fuels'
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[patent_app_number] => 12/078407
[patent_app_country] => US
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[pdf_file] => publications/A1/0241/20090241547.pdf
[firstpage_image] =>[orig_patent_app_number] => 12078407
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/078407 | Gas turbine fuel injector for lower heating capacity fuels | Mar 30, 2008 | Abandoned |
Array
(
[id] => 5306368
[patent_doc_number] => 20090013664
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2009-01-15
[patent_title] => 'Actuator Arrangement'
[patent_app_type] => utility
[patent_app_number] => 12/057497
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[patent_effective_date] => 0000-00-00
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[pdf_file] => publications/A1/0013/20090013664.pdf
[firstpage_image] =>[orig_patent_app_number] => 12057497
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/057497 | Thrust reverser and VAFN arrangement | Mar 27, 2008 | Issued |