Patent ID: 8474267
Filing Date: 2013-07-02
Classification: F01D

Abstract:
1. A turbo machine comprising: a turbine nozzle including a wall providing spaced apart first and second surfaces; a combustor including a liner having an annular lip engaging one of the first and second surfaces, the combustor extends along an axis of the turbo machine normal to a radial direction; and a floating ring seal supported by the liner in a slip fit relationship, the floating ring seal engaging the other of the first and second surfaces, the floating ring seal slideably movable relative to the liner in a floating direction, which includes a radial component, in response to movement of the liner in the radial direction, wherein the floating direction is transverse to the radial direction and the axis, and wherein the annular lip, a lateral portion of the floating ring seal and the wall are spaces radially relative to one another.