WO2024069540 - STRUCTURAL ARRANGEMENT IN A LOW-TEMPERATURE TURBOCOMPRESSOR USING OTHER POWER CONNECTIONS

National phase entry is expected:
Publication Number WO/2024/069540
Publication Date 04.04.2024
International Application No. PCT/IB2023/059724
International Filing Date 28.09.2023
Title **
[English] STRUCTURAL ARRANGEMENT IN A LOW-TEMPERATURE TURBOCOMPRESSOR USING OTHER POWER CONNECTIONS
[French] AGENCEMENT STRUCTURAL DANS UN TURBOCOMPRESSEUR À BASSE TEMPÉRATURE UTILISANT D'AUTRES CONNEXIONS D'ALIMENTATION
Applicants **
DUO ENGENHARIA CRIATIVA LTDA
Inventors
DE AVILA ANTONINI, Natal
SCHAAN CASAGRANDE, Andre
HARTMANN DA SILVA, Bruno
DONADEL BASSO, Eduardo
TUMELERO VALENTE, Vitor
Priority Data
17/957,754   30.09.2022   US
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Quotation for National Phase entry

Country StagesTotal
China Filing, Examination, Granting2308
EPO Filing, Examination, Granting14249
Japan Filing, Examination, Granting2307
South Korea Filing, Examination, Granting2463
USA Filing, Examination, Granting4310
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Total: 25,637

The term for entry into the National Phase has expired. This quotation is for informational purposes only

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Abstract[English] A low-temperature turbocompressor structural arrangement for an internal combustion engine for using energy that is available but unused during operation to cool the air supplied to the engine by supercharging. The temperature of the air compressed by the compressor is reduced by a cooling system and the air is then conveyed to a further turbine actuated by the intake air flow of the engine. The structural arrangement may be mounted in full or in part, and also each component may be fitted into existing systems.[French] L'invention concerne un agencement structural de turbocompresseur à basse température pour un moteur à combustion interne pour utiliser l'énergie qui est disponible mais non utilisée pendant le fonctionnement pour refroidir l'air fourni au moteur par suralimentation. La température de l'air comprimé par le compresseur est réduite par un système de refroidissement et l'air est ensuite transporté vers une autre turbine actionnée par le flux d'air d'admission du moteur. L'agencement structural peut être monté en totalité ou en partie, et chaque composant peut également être ajusté dans des systèmes existants.