A turbine engine includes an element (3), comprising a wall (11) and at least one load-bearing member (17) extending substantially perpendicularly relative to the wall (11), with said member (17) being intended to be attached onto a mounting (18) used for the attachment thereof onto an aircraft structural part. A thermal protection member (23) surrounds said member (17), with said thermal protection member (23) including a base flexibly supported on the wall (11) of the element (3), with said base matching the shape of said wall and at least one covering part which surrounds said load-bearing member.
Turbine engine, such as for example an aircraft turbojet engine or a turboprop engine.
2020-09-30
Patent
Electronic Resource
English
TURBINE ENGLINE, SUCH AS FOR EXAMPLE AN AIRCRAFT TURBOJET ENGINE OR A TURBOPROP ENGINE
European Patent Office | 2017
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