Sensor bracket for at least one sensor on a gas turbine
AssigneeRolls-Royce Deutschland Ltd & Co KG
InventorOlaf LENK
Life of this patent
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Abstract
A sensor bracket (1) for at least one sensor (5) on a gas turbine, made of at least one fiber-composite material (10), with the fibers (7) embedded in the fiber-composite material (10) being oriented at an angle α relative to an axis x extending vertically to a free end edge (3) of the sensor bracket (1) in a plane established by the fibers (7), and the stiffness and the natural frequencies of the sensor bracket (1) being defined by said angle α, with the natural frequencies of the sensor bracket (1) lying outside of the frequency range of the sensor bracket (1), which includes the measuring range of the sensor (5).
Claims18
A sensor bracket for at least one sensor on a gas turbine, comprising at least one fiber-composite material having fibers embedded in the fiber-composite material that are oriented at an angle α relative to an axis x extending vertically to a free end edge of the sensor bracket in a plane established by the fibers, wherein a stiffness and natural frequencies of the sensor bracket are defined by the angle α such that the natural frequencies of the sensor bracket lie outside a frequency range of the sensor bracket, which includes a measuring range of the sensor.
Dependencies are inferred from the claim text.