GAS TURBINE ENGINE WITH STATOR SEGMENTS

A gas turbine engine (20) includes a case assembly (60) and a stator segment (62). The case assembly defines a first slot (70) having a first surface (80) and a second surface (82). The stator segment includes a shroud body (100) axially extends between a first body end (110) and a second body end (...

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Bibliographische Detailangaben
Hauptverfasser:	WARNER, Charles H, PONCHAK, Jeffrey D, MORROW, Alex Daniel
Format:	Patent
Sprache:	eng ; fre ; ger
Schlagworte:	BLASTING ENGINE PLANTS IN GENERAL HEATING LIGHTING MACHINES OR ENGINES IN GENERAL MECHANICAL ENGINEERING NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAMTURBINES STEAM ENGINES WEAPONS
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Beschreibung
Zusammenfassung:	A gas turbine engine (20) includes a case assembly (60) and a stator segment (62). The case assembly defines a first slot (70) having a first surface (80) and a second surface (82). The stator segment includes a shroud body (100) axially extends between a first body end (110) and a second body end (112). A first flange (120) extends into the first slot. The first flange has a first flange first side (130), a first flange second side (132), a first flange first surface (134) and a first flange second surface (136) each circumferentially extending between the first flange first side and the first flange second side. A first portion (140) of the first flange first surface engages the first surface. A second portion (142) of the first flange first surface engages the first surface. A third portion (144) of the first flange first surface is spaced apart from the first surface.