Turbine engine such as, for example, an airplane turbojet or turboprop engine

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专利权人:

Safran Aircraft Engines

发明人:

申请号：

GB20170004532

公开号：

GB201704532(D0)

申请日:

2015.09.21

申请国别(地区):

英国

年份:

2017

代理人:

摘要：

The invention relates to a turbine engine provided with an element (3), comprising a wall (11) and at least one load-bearing member (17) extending substantially perpendicularly relative to the wall (11). Said member (17) is to be attached onto a mounting (18) for attachment onto an aircraft structural part, where a thermal protection member (23) surrounds said member (17). Said thermal protection member (23) includes a base flexibly supported on the wall (11) of the element (3). Said base closely fits said wall and at least one covering part that surrounds said load-bearing member.

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