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US 2022/0065166 A1Published application
Structural assembly for a gas turbine engine
AssigneeRolls-Royce Deutschland Ltd & Co KG
InventorsStefan MITTELSTAEDT, Jiri SACHA
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Abstract
The invention regards a structural assembly for a gas turbine engine which includes a bearing with a statically arranged outer ring and a rotatably arranged inner ring, the bearing outer ring including a radially outer surface. The assembly further includes a housing structure supporting the statically arranged outer ring. It is provided that the housing structure forms a housing ring against which the radially outer surface of the bearing outer ring lies and which supports the bearing outer ring radially outwards.
Claims19
A structural assembly for a gas turbine engine comprising:
- a bearing comprising a statically arranged outer ring and a rotatably arranged inner ring, the bearing outer ring comprising a radially outer surface,
- a housing structure supporting the statically arranged outer ring,
- wherein
- the housing structure forms a housing ring against which the radially outer surface of the bearing outer ring lies and which supports the bearing outer ring radially outwards.
1 more element
Dependencies are inferred from the claim text.