主权项 |
1. An arrangement for a gas turbine engine in which an inner cylindrical casing is connected to a concentric outer cylindrical casing, comprising:
an inner cylindrical casing; an outer cylindrical casing concentric with the inner cylindrical casing; and a connector connecting the inner and the outer cylindrical casings, wherein the connector comprises a cylindrical connector disposed between and concentric with the inner and the outer cylindrical casings, wherein the cylindrical connector is stiff in a direction of a concentric axis but flexible in a direction radially with respect to the concentric axis such that a relative thermal expansion of the inner and the outer cylindrical casings in the radial direction is permitted whilst simultaneously maintaining a relative position of the inner and the outer cylindrical casings in the axial direction, wherein the cylindrical connector comprises:
an annular first end secured to the inner cylindrical casing,an annular second end secured to the outer cylindrical casing, anda cylindrical main body between the annular first and the second ends,wherein the cylindrical main body is flexible in the radial direction to permit the relative thermal expansion of the inner and the outer cylindrical casings in the radial direction,wherein the cylindrical main body comprises:
a cylindrical first section,an annular second section, anda cylindrical third section,wherein the cylindrical first section extends axially away from the annular first end to a radially inner part of the annular second section,wherein the cylindrical third section extends axially from a radially outer part of the annular second section towards the annular second end. |