FLOW DIVERTER ELEMENT AND ASSEMBLY

摘要

An assembly for a gas turbine engine, comprises a fairing assembly extending generally axially through a portion of the gas turbine engine, a first component disposed radially inward of the fairing assembly, a second component disposed axially adjacent to the first component, a flow diverter, and a finger seal. The flow diverter includes a mounting portion securing the flow diverter to the first component, and an arm extending in an axial direction from the mounting portion toward the second component. The finger seal includes a fixed end secured between the flow diverter mounting portion and the first component.

主权项

1. An assembly for a gas turbine engine, comprising:
a fairing assembly extending generally axially through a portion of the gas turbine engine; a first component disposed radially inward of the fairing assembly; a second component, disposed axially adjacent to the first component; a flow diverter including a mounting portion securing the flow diverter to the first component, and an arm extending in an axial direction from the mounting portion toward the second component; and a finger seal including a fixed end secured between the flow diverter mounting portion and the first component.