Schwebende Wand mit Erhöhtem Prallfilm für einen Gasturbinenmotor
Anmelder: RTX Corporation 🇺🇸
Details
- Veröffentlichungs-Nr.
- EP4528163
- Aktenzeichen
- EP24201096
- Anmeldetag
- 18. September 2024
- Veröffentlichung
- 26. März 2025
- Rechtsraum
- EP
- IPC
- F23R3/00
Abstract
An assembly for a combustor (56) for a gas turbine engine, including: a plurality of heat shield panels (58) attached to at least one combustor liner (60), each one of the plurality of heat shield panels (58) including a panel portion (100) and a first forward rail (94) and a second rearward rail (96) each extending from an outer surface of the panel portion (100), the panel portion (100) including an inner surface (102) opposite of the outer surface, the panel portion (100) also includes a forward end (104) and a rearward end (106), the forward end (104) of the panel portion (100) is axially forward of the rearward end (106) of an adjacent heat shield panel of the plurality of heat shield panels (58) such that a gap (108) is defined between the outer surface of the panel portion (100) of one heat shield panel of the plurality of heat shield panels (58) and an inner surface (102) of the panel portion (100) of an adjacent heat shield panel of the plurality of heat shield panels (58), the panel portion (100) also includes a plurality of apertures (110) extending from the outer surface to the inner surface (102); and a plurality of cooling pins (112) extending upwardly and away from the outer surface towards a surface of the at least one combustor liner (60).
Anmelder
- Firma
- RTX Corporation
- Land
- 🇺🇸 USA
US-amerikanischer Luft- und Raumfahrt- sowie Verteidigungskonzern, entstanden aus Raytheon und United Technologies. Entwickelt und fertigt Triebwerke, Avionik, Radarsysteme, Raketen- und Verteidigungstechnik für zivile und militärische Kunden.
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