Buffer effect of turbine rim cavity on hot gas ingestion

Author:

Jia Xingyun1ORCID,He Lidong1,Liu Chunrui1,Zhang Le1

Affiliation:

1. College of Mechanical and Electrical Engineering, Beijing University of Chemical Technology, China

Abstract

The rotor disc in the gas turbine creates a pump effect that entrains the fluid near it to radially outward. The hot gas in the mainstream enters the stator–rotor wheel space to maintain mass balance, leading to gas ingestion. The mechanism of the gas ingestion, and the spoiling effect of purge flow on mainstream, and the formation and transform mechanism of the source and core fluid regions in rotor–stator system are revealed in this research. In addition, a radial–radial–axial clearance rim seal (RRACS) is proposed to form a new stator–stator cavity to buff the ingestion flow. Numerical results show that the minimum mass flow rate for seal of the RRACS is 15.76% of the standard axial clearance rim seal.

Funder

China Postdoctoral Science Foundation funded project

The National Science and Technology Major Project

Fundamental Research Funds for the Central Universities

Publisher

SAGE Publications

Subject

Mechanical Engineering,Energy Engineering and Power Technology

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