Radially compressible and expandable rotor for a pump having an impeller blade
The invention relates to a radially compressible and expandable rotor ( 13, 13 a, 13 b ) for a pump having at least one impeller blade ( 20, 22, 36, 36 a, 36 b, 36 c, 36 d, 36 e, 36 f, 36 g, 37, 37 a, 37 b, 37 c, 37 d, 37 e, 37 f, 74, 88, 89, 90 ), wherein the impeller blade has an impeller blade body whose material is elastically deformable as well as at least one stiffening strut ( 25, 26, 27, 30, 31, 32, 52, 53, 57, 58, 62, 63, 67, 95 ) which is at least partially embedded in the material of the impeller blade body. The struts are designed suitably in size, shape and arrangement and are integrated in suitable hollow spaces of the impeller blade body for stabilizing the impeller blade. Elements with tensile strength can additionally be provided.
1. A rotor for a blood pump, comprising:
at least one impeller blade configured to rotate about a hub to convey a fluid, the at least one impeller blade having first and second sides oriented such that, when the blade rotates about the hub, the first side is a suction side and the second side is a pressure side, comprising:
an impeller blade body,
a first stiffening strut extending from a hub, the first stiffening strut having distal and proximal ends and a width and a length, the length extending from the distal end to the proximal end, the first stiffening strut being coupled to the hub at the proximal end, and
a second stiffening strut coupled to the hub;
wherein the at least one impeller blade is configured to be radially compressed from a first deployed state to a second compressed state, and wherein the first stiffening strut is deformable independently from the second stiffening strut during radial compression of the at least one impeller blade.
2. The rotor of claim 1 , wherein the at least one impeller blade is configured to uniformly deform as a whole.
3. The rotor of claim 1 , wherein the at least one impeller blade is radially compressed onto a rotor hub.
4. The rotor of claim 1 , wherein the first stiffening strut is coupled to the second stiffening strut at the distal end of the first stiffening strut.
5. The rotor of claim 4 , wherein the first stiffening strut and second stiffening strut are coupled so as to form a loop.
6. The rotor of claim 1 , wherein the first stiffening strut is coupled to the second stiffening strut at the proximal end of the first stiffening strut.
7. The rotor of claim 1 , wherein the first stiffening strut is adhered to the suction side surface of the impeller blade body.
8. The rotor of claim 7 , wherein the first stiffening strut is adhered to a surface of the impeller blade at the proximal end of the first stiffening strut.
9. The rotor of claim 1 , wherein the at least one impeller blade is configured to expand beyond the first deployed state to a third operational state.
10. The rotor of claim 9 , wherein the at least one impeller blade is configured to assume the third operational state under fluid counter pressure.
11. The rotor of claim 10 , wherein the at least one impeller blade is concave about an axis parallel to a chord length of the blade in the first deployed state.
12. The rotor of claim 1 , wherein the first stiffening strut is at least partially embedded in the impeller blade body.
13. The rotor of claim 12 , wherein a thickness of the impeller blade body in a direction between a pressure side and a suction side amounts to at least 80% of a thickness of the at least one stiffening strut in the same direction.
14. The rotor of claim 13 , wherein the first stiffening strut is completely embedded in the impeller blade body material.
15. The rotor of claim 1 , wherein the first stiffening strut is insert molded with the material of the impeller blade body.
16. The rotor of claim 1 , wherein the first stiffening strut is arranged in a recess of the impeller blade body.
17. The rotor of claim 16 , wherein the recess of the impeller blade body is longer in a longitudinal direction of the first stiffening strut than the length of the first stiffening strut.
18. The rotor of claim 16 , wherein the recess of the impeller blade body is longer in a transverse direction of the first stiffening strut than the width of the first stiffening strut.
19. The rotor of claim 1 , wherein the first stiffening strut extends at least partially at an angle of at least 90° to an axial direction of rotation.
20. The rotor of claim 1 , wherein the at least one impeller blade has on the pressure side at least one element with a tensile strength in the form of a band or film which is connected to the first stiffening strut at a radially outer fastening point and at a radially inner fastening point.