Vorrichtung und Verfahren zur Formung von Gasturbinentriebwerkskomponenten

Details

Veröffentlichungs-Nr.

EP3741499

Aktenzeichen

EP20171932

Anmeldetag

28. April 2020

Veröffentlichung

2. Oktober 2024

Erteilung

2. Oktober 2024

Rechtsraum

EP

IPC

B23P15/04F01D5/14B22F3/24B22F7/06C22C1/04F01D5/28F04D29/54F04D29/58B21D22/02B21D37/16B21D53/78B21D26/053B22F10/20F04D29/32B22F5/04

Abstract

A mounting plate (280) for forming a gas turbine engine component (160) comprising a plate body (280A) defining an abutment (280E) dimensioned to mate with a forming die (182, 183). The plate body (280A) defines at least one internal cooling circuit (288). The at least one internal cooling circuit (288) includes a passageway (289) having an intermediate portion (289C) interconnecting inlet and outlet portions (289A, 289B). The intermediate portion (289C) is dimensioned to follow a perimeter of the abutment (280E). The intermediate portion (289C) includes a plurality of fins (290) extending partially from a first sidewall (280F) towards a second sidewall (280G) opposed to the first sidewall (280F). A method of forming a gas turbine engine component (160) is also disclosed.

Anmelder

Firmen

RTX Corporation
Raytheon Technologies Corporation

Land

🇺🇸 USA

Fachgebiete