Rapid processing of laminar composite components
US-12180120-B2 · Dec 31, 2024 · US
US9611743B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-9611743-B2 |
| Application number | US-201113261562-A |
| Country | US |
| Kind code | B2 |
| Filing date | Jul 1, 2011 |
| Priority date | Jul 15, 2010 |
| Publication date | Apr 4, 2017 |
| Grant date | Apr 4, 2017 |
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The invention relates to a radially compressible and expandable rotor for a pump having at least one impeller blade, wherein the impeller blade has an impeller blade body whose material is elastically deformable as well as at least one stiffening strut 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.
Opening claim text (preview).
The invention claimed is: 1. A radially compressible and expandable rotor for a pump comprising at least one impeller blade, wherein the impeller blade has an impeller blade body whose material is elastically deformable as well as at least one stiffening strut which is at least partially embedded in the material of the impeller blade body, wherein the impeller blade thickness between the pressure side and the suction side amounts to at least 80% of the thickness of the at least one strut in the same direction. 2. The rotor of claim 1 , wherein the impeller blade thickness between the pressure side and the suction side amounts to 100% of the thickness of the at least one strut in the same direction. 3. The rotor of claim 2 , wherein the impeller blade thickness between the pressure side and the suction side is more than the largest thickness of a strut of said at least one strut. 4. The rotor in accordance with claim 1 , wherein the thickness of the at least one impeller blade is constant in the region in which the at least one strut is positioned, including the region disposed between the at least one strut in the direction transversely to the longitudinal direction of the at least one strut, when viewed substantially perpendicular to the longitudinal direction of the at least one strut. 5. The rotor in accordance with claim 1 , wherein the rotor adopts a first state without any external force effect, starting from which it can move by radial compression into a second state, and starting from which the at least one impeller blade can be erected in operation in particular by the fluid counter pressure and/or centrifugal forces which occur on the rotation up to a third, expanded state. 6. The rotor in accordance with claim 5 , wherein the rotor is hubless and the at least one strut extends in the radial direction with respect to the axis of rotation from a first axial spacing to a second axial spacing. 7. The rotor in accordance with claim 5 , wherein the at least one impeller blade is connected to a hub and is pivotable with respect to it. 8. The rotor in accordance with claim 7 , wherein the at least one strut extends up to and into the hub. 9. The rotor in accordance with claim 6 , wherein the at least one strut extends radially from said first axial spacing radially outside the hub up to said second axial spacing. 10. The rotor in accordance with claim 1 , wherein a plurality of struts are provided which are connected to one another. 11. The rotor in accordance with claim 10 , wherein the plurality of struts are connected to one another at their ends close to the axis of rotation. 12. The rotor in accordance with claim 1 , wherein the at least one strut is connected to one another only within the half of their radial extent close to the axis of rotation. 13. The rotor of claim 1 , wherein said elastic material comprises an elastic polymer or a memory alloy or nitinol. 14. The rotor in accordance with claim 1 , wherein the element with tensile strength contains glass fibers or polycarbonate fibers. 15. The rotor in accordance with claim 1 , wherein the element with tensile strength adheres at least partially to the surface of a strut or of the impeller blade body. 16. The rotor in accordance with claim 15 , wherein the element with tensile strength is adhered, sprayed on or printed on. 17. The rotor in accordance with claim 16 , wherein the element with tensile strength extends in a meandering manner in the first state of the rotor. 18. The rotor in accordance with claim 1 , wherein the impeller blade is pivotably supported in a recess of a hollow cylindrical hub at a jacket side. 19. The rotor in accordance with claim 18 , wherein an inner end of the impeller blade projects through the recess into the cylindrical hollow space of the hub. 20. The rotor in accordance with claim 1 , wherein the stiffening strut is comprised of a first material and the impeller blade body is comprised of a second material, wherein the first material is different from the second material.
Human Necessities · mapped topic
Construction, i.e. structural features, e.g. of weight-saving hollow blades (F01D5/148, F01D5/16 and F01D5/20 take precedence; blade shape F01D5/141; blades with cooling or heating channels or cavities F01D5/18; heating, heat-insulating or cooling means on blades F01D5/18) · CPC title
Human Necessities · mapped topic
Human Necessities · mapped topic
the blood flow through the rotating member having both radial and axial components, e.g. mixed flow pumps · CPC title
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