Flight gas turbine for aircraft, has bearing element with ring encompassing picollo tube elements and elastically deformed in axial direction relative to engine axis, and carrier element extended parallel to axis of tube elements

摘要

The turbine has a bearing element (33) with a ring encompassing picollo tube elements (29). A U-shaped resilient intermediate element i.e. elastic band, extends transverse to a longitudinal axis of the tube elements. An elongated resilient carrier element is fastened with the intermediate element. The carrier element has an end region fastened with the intermediate element and another end region bent toward the former end region. The carrier element is extended parallel to the axis of the elements. The bearing element is elastically deformed in axial direction relative to an engine axis.