Kompressionswerkzeug und Verfahren zur Herstellung von Gasturbinenmotorkomponenten

Details

Veröffentlichungs-Nr.

EP3900918

Aktenzeichen

EP21170290

Anmeldetag

23. April 2021

Veröffentlichung

3. Januar 2024

Erteilung

3. Januar 2024

Rechtsraum

EP

IPC

B29C70/34F01D25/24

Abstract

An assembly (60) and a method for forming a gas turbine engine (20) includes a layup tool (62) including a main body (MB) extending along a longitudinal axis (X) and a flange (68) extending radially from the main body (MB), the flange (68) defining an edge face (68E) slopes towards the main body (MB) to an axial face (68A). At least one compression tool (64) has a tool body (70) having a first tool section (72) and a second tool section (74) extending transversely from the first tool section (72). The first tool section (72) is translatable along a retention member (76) in a first direction (D1) substantially perpendicular to the edge face (68E) such that relative movement causes the second tool section (74) to apply a first compressive force (CI) on a composite article trapped between the axial face (68A) of the flange (68) and the second tool section (74).

Anmelder

Firmen

RTX Corporation
Raytheon Technologies Corporation

Land

🇺🇸 USA

Fachgebiete