Combustor liner with integrated anti-rotation and removal...

Details Combustor liner with integrated anti-rotation and removal... Combustor liner with integrated anti-rotation and removal...

F - Mech Eng,Light,Heat,Weapons

23

R

F23R 3/60 (2006.01) F23R 3/00 (2006.01)

Patent

CA 2677372

A combustor liner for a gas turbine engine including first and second annular liner portions engaged to one another with an interference fit. The first liner portion includes at least one anti-rotation feature extending therefrom and engaging the second liner portion and having a threaded hole defined therethrough at least substantially perpendicularly to an adjacent radially extending surface of the second liner portion for threadingly receiving a pushing tool for pushing against that surface.

Une chemise de chambre de combustion pour un moteur de turbine à gaz comprend une première et une deuxième parties annulaires de chemise engagées l'une à l'autre avec un ajustement à serrage. La première partie de chemise inclut au moins une caractéristique antirotation se prolongeant à partir de la deuxième partie de chemise et l'engageant et dotée d'une ouverture filetée définie traversant au moins essentiellement de manière perpendiculaire une surface adjacente se prolongeant de manière radiale de la deuxième partie de chemise pour recevoir de manière filetée un outil de poussage pour pousser contre cette surface.

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