Rotor blade with edge protection

Abstract

The invention relates to sheath for a blade that has a uniform assembly direction over the radial height of the sheath whether the blade has a straight or curved trajectory. This is achieved by the a sheath formed around the edge, having a first inner surface wherein a first tangential vector projected tangentially to the first inner surface in a direction away from the head portion in an longitudinal plain forms a first angle with the rotational axis that does not vary over the radial height of the sheath while a second tangential vector projected tangentially from any point of the second inner surface of the sheath in a direction towards the head portion intersects the first tangential vector.

Claims

1. A rotating blade having: a rotational axis defining a circumferential direction that is concentric to the rotational axis a first surface; a second surface diametrically opposed the first surface; an curved edge, defined by a junction, in a radial direction, between the first surface and the second surface, wherein the curved edge is curved from the radial direction in the circumferential direction; a core defining the basic shape of the rotating blade a sheath covering a section of the core so as to form a portion of the first surface, the second surface and the curved edge, the sheath comprising: a first radial end; a second radial end radially distal from the first radial end; a head portion forming the portion of the curved edge between the first radial end and the second radial end; a first portion, extending from the head portion to form a portion of the first surface, having a first inner surface facing the core; and a second portion, extending from the head portion to form a portion of the second surface, having a second inner surface that faces the core, wherein the orientation of the first surface and the second surface relative to each other is such that over the radial height of the sheath, the sheath has a fixed assembly angle on the core.

2. The rotating blade of claim 1, wherein the rotational axis defines a longitudinal plain extending radially from the rotating axis and the fixed assembly direction is a result of the first inner surface being such that at any circumferential cross section a first tangential vector, the first inner surface forms a fixed first angle with the longitudinal plain while at the same circumferential cross section the extension of the second inner surface from the head portion the second inner surface remains constant and/or diverges from the first inner surface.

3. The rotating blade of claim 1, wherein the first inner surface, in any circumferential section between the radial first end and the second radial end, is essential straight.

4. The rotating blade of claim 1, wherein the curved edge is a leading edge.

5. The rotating blade of claim 1, wherein the first surface is a pressure surface of the blade and the second surface is a suction surface of the blade.

6. The rotating blade of claim 1, wherein the first surface is a suction surface of the blade and the second surface is a pressure surface of the rotating blade.

Description

BRIEF DESCRIPTION OF THE DRAWINGS

(1) By way of example, an embodiment of the present disclosure is described more fully hereinafter with reference to the accompanying drawings, in which:

(2) FIG. 1 is a top view of a blade according to an exemplary embodiment of the disclosure;

(3) FIG. 2 is a sectional top view of a portion of the blade of FIG. 1 showing the angular alignment of inner surfaces of an exemplary sheath relative to an axis of rotation of the blade;

(4) FIG. 3 is a side view of the blade of FIG. 1; and

(5) FIG. 4 are top view of partial axial sections shown in FIG. 3

DETAILED DESCRIPTION

(6) Exemplary embodiments of the present disclosure are now described with references to the drawings, wherein like reference numerals are used to refer to like elements throughout. In the following description, for purposes of explanation, numerous specific details are set forth to provide a thorough understanding of the disclosure. However, the present disclosure may be practiced without these specific details, and is not limited to the exemplary embodiments disclosed herein.

(7) An exemplary embodiment shown in FIG. 1 is a rotating blade that is configured and arranged to rotate around a rotational axis 2, which in the radial direction forms a longitudinal plain. The blade comprises a leading edge 7, trailing edge 8 a pressure surface 5 and a suction surface 6. The leading edge 7 is curved along a radial height 3 in a circumferential direction 4 relative to the rotational axis 2, and additionally comprises a sheath 10 that covers a portion of the core 11 of the blade and forms at least a portion of the leading edge 7.

(8) In a not shown exemplary embodiment, a blade comprises a sheath 10 that covers a portion of the core 11 of the blade and forms at least a portion of a curved trailing edge 8 of the blade wherein the curvature is along a radial height 3 of the blade in a circumferential direction 4.

(9) In order to assist bonding of the sheath 10 to the edge 7, 8, it is advantageous to increase the surface area of contact between the sheath 10 and the body of the blade. This is achieved by the sheath 10 including a suction portion 22 and a pressure portion 12 that each project from a head portion 20 of the blade so as to form part of the suction surface 6 and pressure surface 5 respectively. Even though erosion protection is primarily required on the suction surface of the blade, maximising the contact surface area of the sheath 10 on the pressure surface 5 maximises the adhesion surface between the sheath 10 and the body of the blade, which is enhanced by the inner surface of the pressure portion 12 and the inner surface of the suction portion 22 forming a cavity between themselves that is shaped to enable the insertion of a portion of the core 11 therein.

(10) As shown in FIG. 2, the sheath 10 is configured to protect the blade body from erosion in a circumferential curved edge region of the blade by forming part of an edge 7, 8 region of the blade.

(11) In an exemplary embodiment shown in FIG. 2, to enable fitting of the sheath 10 as a single piece to the curved edge 7, the sheath 10 is configured such that the sheath 10 has a fixed assembly angle on the core 11 over the radial height 3 of the sheath 10. In an exemplary embodiment, this is achieved by the pressure inner surface 14 of the pressure portion 12 of the sheath 10 being configured such that at any circumferential section of the blade, a tangential vector 18 projected from any point of the pressure inner surface 14 forms a first angle 16 with the rotational axis 2. This first angle 16 does not vary over the radial height 3 of the sheath 10. That is, the first angle 16 is uniform over the entire radial height 3 of the sheath 10. When the pressure inner surface 14 is in each circumferential cross section forms a flat plain, the first angle 16 is the assembly angle 16 and as a result defines the assembly direction of the sheath 10 on the core 11. As a result of the fixing of the first angle 16, as can be seen in FIG. 4 the length of the pressure portion 12 varies with radial height 3 due to the curvature of the blade resulting in a change in angle of the pressure surface 5 relative to the rotational axis 2.

(12) To further enable the fixed assembly angle despite the curvature of the edge 7, 8 the suction inner surface 24 extends from the head portion 20 either parallel to or divergent from the pressure side inner surface 14. When diverging, a tangential vector 28 to the suction inner surface 24 forms a second angle 26 with the tangent line 18 of the pressure inner surface 14. In this embodiment, the suction inner surface 24 may be either straight or curved.

(13) As long there is no point of convergence between the two tangent lines 18, 28 and there is a fixed angle 16 at either the pressure inner surface 14 or the suction inner surface 24, it is possible to have a fixed assembly direction along the entire radial height 3 of the sheath 10, thus enabling the fitting of a ridged, inflexible sheath 10 to a curved edge of a blade as a single piece.

(14) Although the disclosure has been herein shown and described in what is conceived to be the most practical exemplary embodiments, the present disclosure can be embodied in other specific forms. For example, while illustrated embodiments shows the application of a sheath 10 to the leading edge of a blade, the invention may be equally applied using the described exemplary embodiments, to the trailing edge of the blade. Alternatively, although exemplary embodiments provide that the pressure inner surface 14 has a fixed first angle 16, the fixed suction inner surface 24 may alternatively have the fixed angle rather or in addition to the pressure inner surface 14. Yet further, although the pressure inner surface 14 is shown for each circumferential cross-section to be straight, it is possible to provide the inner surface 14 with an outwardly flaring inner surface in which one point of the pressure inner surface 14 defines the assemble angle 16. The presently disclosed embodiments are therefore considered in all respects to be illustrative and not restricted. The scope of the disclosure is indicated by the appended claims rather that the foregoing description and all changes that come within the meaning and range and equivalences thereof are intended to be embraced therein.