
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] => 10822991
[patent_doc_number] => 20160169156
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2016-06-16
[patent_title] => 'THRUST REVERSER SYSTEM WITH TRANSLATING-ROTATING HINGE ASSEMBLY'
[patent_app_type] => utility
[patent_app_number] => 14/908557
[patent_app_country] => US
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[patent_effective_date] => 0000-00-00
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[rel_patent_id] =>[rel_patent_doc_number] =>) 14/908557 | Thrust reverser system with translating-rotating hinge assembly | Jul 29, 2014 | Issued |
Array
(
[id] => 12369852
[patent_doc_number] => 09958162
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2018-05-01
[patent_title] => Combustor assembly for a turbine engine
[patent_app_type] => utility
[patent_app_number] => 14/335334
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[patent_app_date] => 2014-07-18
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Array
(
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[patent_doc_number] => 20140325989
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2014-11-06
[patent_title] => 'Combustor with Fuel Staggering for Flame Holding Mitigation'
[patent_app_type] => utility
[patent_app_number] => 14/333603
[patent_app_country] => US
[patent_app_date] => 2014-07-17
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Array
(
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[patent_doc_number] => 20140360158
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[patent_kind] => A1
[patent_issue_date] => 2014-12-11
[patent_title] => 'TWIN-DOOR THRUST REVERSER'
[patent_app_type] => utility
[patent_app_number] => 14/328967
[patent_app_country] => US
[patent_app_date] => 2014-07-11
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Array
(
[id] => 12080354
[patent_doc_number] => 20170342941
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2017-11-30
[patent_title] => 'INTEGRATED THRUST REVERSER ACTUATION SYSTEM'
[patent_app_type] => utility
[patent_app_number] => 15/510513
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Array
(
[id] => 10918952
[patent_doc_number] => 20140321970
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2014-10-30
[patent_title] => 'PASSIVE BOUNDARY LAYER BLEED SYSTEM FOR NACELLE INLET AIRFLOW CONTROL'
[patent_app_type] => utility
[patent_app_number] => 14/325583
[patent_app_country] => US
[patent_app_date] => 2014-07-08
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[rel_patent_id] =>[rel_patent_doc_number] =>) 14/325583 | Passive boundary layer bleed system for nacelle inlet airflow control | Jul 7, 2014 | Issued |
Array
(
[id] => 11902387
[patent_doc_number] => 09771813
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[patent_kind] => B2
[patent_issue_date] => 2017-09-26
[patent_title] => 'Converging flow joint insert system at an intersection between adjacent transitions extending between a combustor and a turbine assembly in a gas turbine engine'
[patent_app_type] => utility
[patent_app_number] => 15/318781
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[rel_patent_id] =>[rel_patent_doc_number] =>) 15/318781 | Converging flow joint insert system at an intersection between adjacent transitions extending between a combustor and a turbine assembly in a gas turbine engine | Jun 25, 2014 | Issued |
Array
(
[id] => 10460380
[patent_doc_number] => 20150345395
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2015-12-03
[patent_title] => 'TURBOFAN ENGINE WITH VARIABLE EXHAUST COOLING'
[patent_app_type] => utility
[patent_app_number] => 14/293963
[patent_app_country] => US
[patent_app_date] => 2014-06-02
[patent_effective_date] => 0000-00-00
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[rel_patent_id] =>[rel_patent_doc_number] =>) 14/293963 | Turbofan engine with variable exhaust cooling | Jun 1, 2014 | Issued |
Array
(
[id] => 10915123
[patent_doc_number] => 20140318143
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2014-10-30
[patent_title] => 'MULTI-CIRCUIT BUFFER SYSTEM FOR A GAS TURBINE ENGINE'
[patent_app_type] => utility
[patent_app_number] => 14/283610
[patent_app_country] => US
[patent_app_date] => 2014-05-21
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[rel_patent_id] =>[rel_patent_doc_number] =>) 14/283610 | Multi-circuit buffer system for a gas turbine engine | May 20, 2014 | Issued |
Array
(
[id] => 9752825
[patent_doc_number] => 20140283525
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2014-09-25
[patent_title] => 'TWO-BRANCH MIXING PASSAGE AND METHOD TO CONTROL COMBUSTOR PULSATIONS'
[patent_app_type] => utility
[patent_app_number] => 14/274647
[patent_app_country] => US
[patent_app_date] => 2014-05-09
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[rel_patent_id] =>[rel_patent_doc_number] =>) 14/274647 | Two-branch mixing passage and method to control combustor pulsations | May 8, 2014 | Issued |
Array
(
[id] => 9652914
[patent_doc_number] => 20140223918
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2014-08-14
[patent_title] => 'COMPRESSED AIR ENERGY SYSTEM INTEGRATED WITH GAS TURBINE'
[patent_app_type] => utility
[patent_app_number] => 14/259071
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[rel_patent_id] =>[rel_patent_doc_number] =>) 14/259071 | COMPRESSED AIR ENERGY SYSTEM INTEGRATED WITH GAS TURBINE | Apr 21, 2014 | Abandoned |
Array
(
[id] => 12212701
[patent_doc_number] => 09909499
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[patent_issue_date] => 2018-03-06
[patent_title] => 'Fuel drainage and purge system and method'
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Array
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[patent_title] => 'Engine systems and methods for removing particles from turbine air'
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Array
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Array
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Array
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Array
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Array
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