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A balanced rotor component for a gas turbine engine having a aerofoil with a root and an rotor with an axial aerofoil root slot. The aerofoil root has a cavity which holds a balance weight. The cavity is open along at least one wall and the balance weight is spaced from the slot wall to minimise str

A balanced rotor component for a gas turbine engine having a aerofoil with a root and an rotor with an axial aerofoil root slot. The aerofoil root has a cavity which holds a balance weight. The cavity is open along at least one wall and the balance weight is spaced from the slot wall to minimise stress concentrations.

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1. A balanced rotor component for a gas turbine engine, the balanced component rotatable about an axis in use and having at least one axial slot having a profile holding a complementary profile of a root portion of a blade member, wherein the slot holds a balance weight which is in contact with a ba

1. A balanced rotor component for a gas turbine engine, the balanced component rotatable about an axis in use and having at least one axial slot having a profile holding a complementary profile of a root portion of a blade member, wherein the slot holds a balance weight which is in contact with a base of the slot at rest, the balance weight being further located within a cavity in the root portion; wherein lateral sides of the cavity are open; and wherein a side of the balance weight has two portions arranged in axial series joined at an obtuse angle, one of the portions contacting a side wall of the slot and the other portion being spaced from the side wall of the slot. 2. The balanced rotor component according to claim 1, wherein the cavity has at least an axially forward or an axially rearward wall defining the axially forward or axially rearward extent of the cavity. 3. The balanced rotor component according to claim 2, wherein the cavity has both an axially forward and an axially rearward wall. 4. The balanced rotor component according to claim 3, wherein the axially forward and axially rearward walls diverge and converge with respect to a center line defined between the two walls. 5. The balanced rotor according to claim 1, wherein the radially inner surface of the balance weight has a form matching the base of the slot. 6. The balanced rotor according to claim 1, wherein the balance weight has a further side opposing the side of the balance weight, wherein the further side is spaced from one of the lateral side walls of the slot. 7. The balanced rotor according to claim 1, wherein the balance weight has a radially extending protrusion engaging a hole in the root portion.