Bearing device for load reduction
AssigneeRolls-Royce Deutschland Ltd & Co KG
InventorsMartin BOEHME, Gideon Daniel VENTER
Life of this patent
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Abstract
A bearing assembly for a gas turbine engine comprises a bearing; a bearing bracket, which holds the bearing and is secured by a predetermined breaking device on a connecting element, which can be connected or is connected to a loadbearing structure of the gas turbine engine; a first toothed component mounted on the bearing bracket; and a second toothed component fixed on the connecting element, wherein, after the destruction of the predetermined breaking device, the first toothed component and the second toothed component can be or are brought into engagement with one another in such a way that one of the toothed components can be made to roll on the other. A gas turbine engine and a method are furthermore provided.
Claims14
A bearing assembly for a gas turbine engine, comprising:
- a bearing;
- a bearing bracket, which holds the bearing and is secured by a predetermined breaking device on a connecting element, which can be connected or is connected to a loadbearing structure of the gas turbine engine;
- and
- a first toothed component mounted on the bearing bracket;
- and
- a second toothed component fixed on the connecting element, wherein, after the destruction of the predetermined breaking device, the first toothed component and the second toothed component can be or are brought into engagement with one another in such a way that one of the toothed components can be made to roll on the other.
Dependencies are inferred from the claim text.