Patent ID: 7989733
Filing Date: 2011-08-02
Classification: F01D,F05D,F16C,H05B,Y02B,Y10T

Abstract:
1. A device for heating a cylindrical component in a turbomachine of given diameter, by means of hot gas, comprising: at least two heaters which deliver a stream of hot gas; an annular chamber defined by an outer cylindrical casing, an inner cylindrical wall and first and second walls perpendicular to an axis of the turbomachine such that the annular chamber presents a ring; and deflectors disposed inside the annular chamber between the heaters, the deflectors being arched and inclined towards the axis of the turbomachine and guide the stream of hot gas emerging into the annular chamber in rotational movement about the axis of the turbomachine, wherein the ring comprises a first half and a second half which are separable, wherein the heaters are disposed circumferentially about the annular chamber and are substantially tangential to the annular chamber, and wherein a diameter of the inner cylindrical wall is greater than said diameter of the cylindrical component.