
June Hwu
Examiner (ID: 2088, Phone: (571)272-0977 , Office: P/1661 )
| Most Active Art Unit | 1661 |
| Art Unit(s) | 1661, 1649 |
| Total Applications | 4095 |
| Issued Applications | 3836 |
| Pending Applications | 30 |
| Abandoned Applications | 242 |
Applications
| Application number | Title of the application | Filing Date | Status |
|---|---|---|---|
Array
(
[id] => 17688671
[patent_doc_number] => 20220195963
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[patent_kind] => A1
[patent_issue_date] => 2022-06-23
[patent_title] => INJECTION MANIFOLD WITH TESLA VALVES FOR ROTATING DETONATION ENGINES
[patent_app_type] => utility
[patent_app_number] => 17/553550
[patent_app_country] => US
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Array
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[patent_title] => Fuel nozzle, fuel nozzle module having the same, and combustor
[patent_app_type] => utility
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Array
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[patent_title] => NOZZLE ASSEMBLY, COMBUSTOR, AND GAS TURBINE HAVING SAME
[patent_app_type] => utility
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Array
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[patent_title] => COMBUSTION CHAMBER, METHOD OF MANUFACTURING A COMBUSTION CHAMBER AND ENGINE
[patent_app_type] => utility
[patent_app_number] => 17/544032
[patent_app_country] => US
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Array
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[patent_title] => Gas turbine engine combustor with integral fuel conduit(s)
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Array
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[patent_title] => BURNER WITH A BILAMINAR COUNTERDIRECTIONAL VORTEX FLOW
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[rel_patent_id] =>[rel_patent_doc_number] =>) 18/272178 | Burner with two-layer vortex countercurrent flow | Nov 16, 2021 | Issued |
Array
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[patent_issue_date] => 2024-01-23
[patent_title] => System and method for monitoring fuel additives
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[rel_patent_id] =>[rel_patent_doc_number] =>) 17/521024 | System and method for monitoring fuel additives | Nov 7, 2021 | Issued |
Array
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[patent_doc_number] => 20240003316
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[patent_issue_date] => 2024-01-04
[patent_title] => TURBOJET ENGINE REAR PART COMPRISING A NOZZLE HAVING FLAPS COMPRISING LEVERS THAT ARE MOVABLE BY MEANS OF UPSTREAM AND DOWNSTREAM BEARING WALLS
[patent_app_type] => utility
[patent_app_number] => 18/252079
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[rel_patent_id] =>[rel_patent_doc_number] =>) 18/252079 | Turbojet engine rear part comprising a nozzle having flaps comprising levers that are movable by means of upstream and downstream bearing walls | Nov 4, 2021 | Issued |
Array
(
[id] => 18355601
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[patent_title] => Liquid rocket engine injector with variable flow area
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Array
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[patent_title] => COMBUSTOR INCLUDING HEAT EXCHANGE STRUCTURE AND ROCKET COMPRISING SAME
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Array
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[patent_title] => FASTENING OF AN EXHAUST CONE IN A TURBOMACHINE NOZZLE
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Array
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[patent_title] => Methods of operating a turbomachine combustor on hydrogen
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Array
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Array
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Array
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Array
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