
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] => 11537358
[patent_doc_number] => 09611756
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2017-04-04
[patent_title] => 'System and method for protecting components in a gas turbine engine with exhaust gas recirculation'
[patent_app_type] => utility
[patent_app_number] => 14/066488
[patent_app_country] => US
[patent_app_date] => 2013-10-29
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 8
[patent_figures_cnt] => 8
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[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14066488
[rel_patent_id] =>[rel_patent_doc_number] =>) 14/066488 | System and method for protecting components in a gas turbine engine with exhaust gas recirculation | Oct 28, 2013 | Issued |
Array
(
[id] => 9431672
[patent_doc_number] => 20140109578
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2014-04-24
[patent_title] => 'COMBUSTOR TRANSITION'
[patent_app_type] => utility
[patent_app_number] => 14/062001
[patent_app_country] => US
[patent_app_date] => 2013-10-24
[patent_effective_date] => 0000-00-00
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[rel_patent_id] =>[rel_patent_doc_number] =>) 14/062001 | Combustor transition | Oct 23, 2013 | Issued |
Array
(
[id] => 11805587
[patent_doc_number] => 09546618
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2017-01-17
[patent_title] => 'Methods and apparatus for passive thrust vectoring and plume deflection'
[patent_app_type] => utility
[patent_app_number] => 14/062673
[patent_app_country] => US
[patent_app_date] => 2013-10-24
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 17
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[rel_patent_id] =>[rel_patent_doc_number] =>) 14/062673 | Methods and apparatus for passive thrust vectoring and plume deflection | Oct 23, 2013 | Issued |
Array
(
[id] => 10230067
[patent_doc_number] => 20150115061
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2015-04-30
[patent_title] => 'GIMBAL PIN FOR JET PROPULSION SYSTEM'
[patent_app_type] => utility
[patent_app_number] => 14/062733
[patent_app_country] => US
[patent_app_date] => 2013-10-24
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 7
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[rel_patent_id] =>[rel_patent_doc_number] =>) 14/062733 | Gimbal pin for jet propulsion system | Oct 23, 2013 | Issued |
Array
(
[id] => 9431673
[patent_doc_number] => 20140109579
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2014-04-24
[patent_title] => 'COMBUSTOR TRANSITION'
[patent_app_type] => utility
[patent_app_number] => 14/062091
[patent_app_country] => US
[patent_app_date] => 2013-10-24
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[rel_patent_id] =>[rel_patent_doc_number] =>) 14/062091 | Combustor transition | Oct 23, 2013 | Issued |
Array
(
[id] => 16185206
[patent_doc_number] => 10718520
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2020-07-21
[patent_title] => Damper arrangement for reducing combustion-chamber pulsation
[patent_app_type] => utility
[patent_app_number] => 14/061954
[patent_app_country] => US
[patent_app_date] => 2013-10-24
[patent_effective_date] => 0000-00-00
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[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14061954
[rel_patent_id] =>[rel_patent_doc_number] =>) 14/061954 | Damper arrangement for reducing combustion-chamber pulsation | Oct 23, 2013 | Issued |
Array
(
[id] => 11916035
[patent_doc_number] => 09784213
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2017-10-10
[patent_title] => 'Aeroengine thrust reverser arrangement'
[patent_app_type] => utility
[patent_app_number] => 14/060044
[patent_app_country] => US
[patent_app_date] => 2013-10-22
[patent_effective_date] => 0000-00-00
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[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14060044
[rel_patent_id] =>[rel_patent_doc_number] =>) 14/060044 | Aeroengine thrust reverser arrangement | Oct 21, 2013 | Issued |
Array
(
[id] => 11895802
[patent_doc_number] => 09765729
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2017-09-19
[patent_title] => 'Thrust reverser fan ramp with blocker door pocket'
[patent_app_type] => utility
[patent_app_number] => 14/056629
[patent_app_country] => US
[patent_app_date] => 2013-10-17
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 6
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[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14056629
[rel_patent_id] =>[rel_patent_doc_number] =>) 14/056629 | Thrust reverser fan ramp with blocker door pocket | Oct 16, 2013 | Issued |
Array
(
[id] => 9417464
[patent_doc_number] => 20140102114
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2014-04-17
[patent_title] => 'IN-LINE REMOVABLE HEAT SHIELD FOR A TURBOMACHINE SUSPENSION YOKE'
[patent_app_type] => utility
[patent_app_number] => 14/053862
[patent_app_country] => US
[patent_app_date] => 2013-10-15
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
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[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14053862
[rel_patent_id] =>[rel_patent_doc_number] =>) 14/053862 | In-line removable heat shield for a turbomachine suspension yoke | Oct 14, 2013 | Issued |
Array
(
[id] => 9417457
[patent_doc_number] => 20140102107
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2014-04-17
[patent_title] => 'HOUSING STRUCTURE WITH IMPROVED SEAL AND COOLING'
[patent_app_type] => utility
[patent_app_number] => 14/052338
[patent_app_country] => US
[patent_app_date] => 2013-10-11
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 2
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[patent_no_of_words] => 1668
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[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14052338
[rel_patent_id] =>[rel_patent_doc_number] =>) 14/052338 | Housing structure with improved seal and cooling | Oct 10, 2013 | Issued |
Array
(
[id] => 9835020
[patent_doc_number] => 20150027101
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2015-01-29
[patent_title] => 'GEARED GAS TURBINE ENGINE ARCHITECTURE FOR ENHANCED EFFICIENCY'
[patent_app_type] => utility
[patent_app_number] => 14/044971
[patent_app_country] => US
[patent_app_date] => 2013-10-03
[patent_effective_date] => 0000-00-00
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[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14044971
[rel_patent_id] =>[rel_patent_doc_number] =>) 14/044971 | GEARED GAS TURBINE ENGINE ARCHITECTURE FOR ENHANCED EFFICIENCY | Oct 2, 2013 | Abandoned |
Array
(
[id] => 9405280
[patent_doc_number] => 20140096532
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2014-04-10
[patent_title] => 'SYSTEM AND METHOD FOR UREA DECOMPOSITION TO AMMONIA IN A SIDE STREAM FOR SELECTIVE CATALYTIC REDUCTION'
[patent_app_type] => utility
[patent_app_number] => 14/045449
[patent_app_country] => US
[patent_app_date] => 2013-10-03
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[rel_patent_id] =>[rel_patent_doc_number] =>) 14/045449 | System and method for urea decomposition to ammonia in a side stream for selective catalytic reduction | Oct 2, 2013 | Issued |
Array
(
[id] => 17490977
[patent_doc_number] => 11280271
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2022-03-22
[patent_title] => Operability geared turbofan engine including compressor section variable guide vanes
[patent_app_type] => utility
[patent_app_number] => 14/433444
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[rel_patent_id] =>[rel_patent_doc_number] =>) 14/433444 | Operability geared turbofan engine including compressor section variable guide vanes | Oct 2, 2013 | Issued |
Array
(
[id] => 11185267
[patent_doc_number] => 09416662
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2016-08-16
[patent_title] => 'Method and system for providing cooling for turbine components'
[patent_app_type] => utility
[patent_app_number] => 14/016769
[patent_app_country] => US
[patent_app_date] => 2013-09-03
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[rel_patent_id] =>[rel_patent_doc_number] =>) 14/016769 | Method and system for providing cooling for turbine components | Sep 2, 2013 | Issued |
Array
(
[id] => 9853730
[patent_doc_number] => 20150033746
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2015-02-05
[patent_title] => 'HEAT SHIELD WITH STANDOFFS'
[patent_app_type] => utility
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[rel_patent_id] =>[rel_patent_doc_number] =>) 13/957735 | HEAT SHIELD WITH STANDOFFS | Aug 1, 2013 | Abandoned |
Array
(
[id] => 10643099
[patent_doc_number] => 09359959
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2016-06-07
[patent_title] => 'Anti-icing system for a gas turbine'
[patent_app_type] => utility
[patent_app_number] => 13/956201
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[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13956201
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/956201 | Anti-icing system for a gas turbine | Jul 30, 2013 | Issued |
Array
(
[id] => 9291117
[patent_doc_number] => 20140034752
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2014-02-06
[patent_title] => 'Atomizer'
[patent_app_type] => utility
[patent_app_number] => 13/953319
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[rel_patent_id] =>[rel_patent_doc_number] =>) 13/953319 | Atomizer | Jul 28, 2013 | Abandoned |
Array
(
[id] => 10935338
[patent_doc_number] => 20140338358
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2014-11-20
[patent_title] => 'INTERNAL DETONATION ENGINE, HYBRID ENGINES INCLUDING THE SAME, AND METHODS OF MAKING AND USING THE SAME'
[patent_app_type] => utility
[patent_app_number] => 13/946829
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[rel_patent_id] =>[rel_patent_doc_number] =>) 13/946829 | Internal detonation engine, hybrid engines including the same, and methods of making and using the same | Jul 18, 2013 | Issued |
Array
(
[id] => 9405279
[patent_doc_number] => 20140096531
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2014-04-10
[patent_title] => 'COMPRESSED AIR ENERGY SYSTEM INTEGRATED WITH GAS TURBINE'
[patent_app_type] => utility
[patent_app_number] => 13/942609
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[rel_patent_id] =>[rel_patent_doc_number] =>) 13/942609 | Compressed air energy system integrated with gas turbine | Jul 14, 2013 | Issued |
Array
(
[id] => 9117227
[patent_doc_number] => 20130284149
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2013-10-31
[patent_title] => 'INJECTION ELEMENT'
[patent_app_type] => utility
[patent_app_number] => 13/929162
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[rel_patent_id] =>[rel_patent_doc_number] =>) 13/929162 | Injection element | Jun 26, 2013 | Issued |