Highly integrated engine component and engine assembly

The invention discloses a highly integrated engine component which comprises a transition section, a power turbine guider, a bearing seat mounting seat, a gas turbine bearing seat and a power turbine bearing seat, and the transition section, the power turbine guider, the bearing seat mounting seat,...

Ausführliche Beschreibung

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Bibliographische Detailangaben
Hauptverfasser: WANG XU, JIANG KANGHE, ZHANG RUOYUN, GAO JIE, CAO JUN
Format: Patent
Sprache:chi ; eng
Schlagworte:
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Beschreibung
Zusammenfassung:The invention discloses a highly integrated engine component which comprises a transition section, a power turbine guider, a bearing seat mounting seat, a gas turbine bearing seat and a power turbine bearing seat, and the transition section, the power turbine guider, the bearing seat mounting seat, the gas turbine bearing seat and the power turbine bearing seat are integrally formed. The invention further provides an engine assembly. The engine assembly comprises the highly-integrated engine component, a power turbine rotor elastic support, a heat shield, a gas turbine rotor elastic support, a tight sealing ring, a gas turbine bearing seat front section, an oil conveying pipe and an oil spraying nozzle. According to the highly integrated engine component provided by the invention, an original transition section assembly component structure is structurally simplified, so that the assembly process is simplified; the number of parts of an original transition section assembly component is reduced to the maximum e