HEAT SHIELD WITH AXIAL RETENTION

A heat shield assembly (158) for an engine case of a gas turbine engine (20) may include a heat shield (130) having an annular shape. A first groove (164) may be formed circumferentially along an inner surface (144) of the heat shield (130). A support lock (116) may have a second groove (180) extend...

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Bibliographische Detailangaben
Hauptverfasser: SANDER, David J, LEMOINE, Jonathan
Format: Patent
Sprache:eng ; fre ; ger
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Zusammenfassung:A heat shield assembly (158) for an engine case of a gas turbine engine (20) may include a heat shield (130) having an annular shape. A first groove (164) may be formed circumferentially along an inner surface (144) of the heat shield (130). A support lock (116) may have a second groove (180) extending radially inward from a distal surface (170) of the support lock (116). A retention ring (162) may be configured to fit within the first groove (164) of the heat shield (130) and the second groove (180) of the support lock (116).