发明申请
US20080260524A1 HEAT SHIELD FOR SEALING A FLOW CHANNEL OF A TURBINE ENGINE 有权
用于密封涡轮发动机的流动通道的热风罩

HEAT SHIELD FOR SEALING A FLOW CHANNEL OF A TURBINE ENGINE
摘要:
A heat shield arrangement for local separation of a flow channel within a turbine engine, with respect to a stator housing radially surrounding the flow channel is provided. The heat shield includes two axially opposite joining contours which are each engageable with two components which are axially adjacent along the flow channel. Each provides a complementary reception contour for the joining contours. At least one of the reception contours has an axial clearance, in which the associated joining contour is axially displaceably mounted. At least one seal is provided between the axially displaceable joining contour and the reception contour. The seal is mounted movably within the reception contour or the joining contour in such a way that the seal is deflectable against a surface region of the reception contour or of the joining contour.
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