WO2025096675 - TURBOCHARGER ASSEMBLY
National phase entry is expected:
Publication Number
WO/2025/096675
Publication Date
08.05.2025
International Application No.
PCT/US2024/053744
International Filing Date
30.10.2024
Title **
[English]
TURBOCHARGER ASSEMBLY
[French]
ENSEMBLE TURBOCOMPRESSEUR
Applicants **
OBERMEYER, Henry, K.
Inventors
STURTEVANT, Mark, A.
Priority Data
63/546,730
31.10.2023
US
18/641,130
19.04.2024
US
Application details
| Total Number of Claims/PCT | * |
| Number of Independent Claims | * |
| Number of Priorities | * |
| Number of Multi-Dependent Claims | * |
| Number of Drawings | * |
| Pages for Publication | * |
| Number of Pages with Drawings | * |
| Pages of Specification | * |
| * | |
| Number of Office Actions | * |
| * | |
International Searching Authority |
EPO
* |
| Recordal of a Change of the Applicant's Name/Address |
Change of Applicant's Name and Address
* |
| Type of Assignment |
The Standard Agent's Assignment
* |
| Applicant's Legal Status |
Natural Person
* |
| * | |
| * | |
| * | |
| * | |
| * | |
| Entry into National Phase under |
Chapter I
* |
| Patent Delivery |
Send the Letters Patent by Courier
* |
| Translation |
|
* The data is based on automatic recognition. Please verify and amend if necessary.
** IP-Coster compiles data from publicly available sources. If this data includes your personal information, you can contact us to request its removal.
Quotation for National Phase entry
| Country | Stages | Total | |
|---|---|---|---|
| China | Filing, Examination, Granting | 2306 | |
| EPO | Filing, Examination, Granting | 8242 | |
| Japan | Filing, Examination, Granting | 2326 | |
| South Korea | Filing, Examination, Granting | 2393 | |
| USA | Filing, Examination, Granting | 4740 |
Total:
20,007
The term for entry into the National Phase has expired. This quotation is for informational purposes only
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Abstract[English]
A turbocharger assembly having a turbine assembly and a compressor assembly that are coupled by a rotating shaft. The turbine assembly includes an exhaust incoming-flow duct configured to deliver exhaust gases to a turbine wheel in an annular flow-path. The turbine wheel redirects and discharges the exhaust gases in a direction that is substantially opposite to the incoming exhaust flow direction. The exhaust outgoing flow passes radially inside of the annular flow-path of the exhaust incoming-flow duct. The compressor assembly includes an air incoming-flow duct configured to deliver air to an impeller wheel. The impeller wheel compresses, redirects, and discharges the air in an annular flow-path in a direction that is substantially opposite to the incoming airflow direction. The air incoming flow passes radially inside of the annular flow-path of the air outgoing-flow duct.[French]
Un ensemble turbocompresseur ayant un ensemble turbine et un ensemble compresseur qui sont couplés par un arbre rotatif. L'ensemble turbine comprend un conduit d'écoulement entrant d'échappement conçu pour distribuer des gaz d'échappement à une roue de turbine dans un trajet d'écoulement annulaire. La roue de turbine redirige et évacue les gaz d'échappement dans une direction qui est sensiblement opposée à la direction d'écoulement d'échappement entrante. L'écoulement sortant d'échappement passe radialement à l'intérieur du trajet d'écoulement annulaire du conduit d'écoulement entrant d'échappement. L'ensemble compresseur comprend un conduit d'écoulement entrant d'air conçu pour distribuer de l'air à une roue à aubes. La roue à aubes comprime, redirige et évacue l'air dans un trajet d'écoulement annulaire dans une direction qui est sensiblement opposée à la direction d'écoulement d'air entrant. L'écoulement entrant d'air passe radialement à l'intérieur du trajet d'écoulement annulaire du conduit d'écoulement sortant d'air.