Material conveying screw and method for producing same

Patent metadata

Field	Value
Publication number	US-11260648-B2
Application number	US-201616062802-A
Country	US
Kind code	B2
Filing date	Dec 16, 2016
Priority date	Dec 18, 2015
Publication date	Mar 1, 2022
Grant date	Mar 1, 2022

Abstract

A screw having a longitudinal body and, around this longitudinal body, at least one flight extending in the shape of a helix, the flight including, over part of its length, internal partitioning delimiting a plurality of internal channels that extend in the shape of helices following the helix shape of the flight. The screw includes manifold-like cavities into which the ends of the interior canals open, the manifold-like cavities extending radially and opened into a longitudinal bore of the body at longitudinally spaced locations. This screw can be produced by additive manufacturing using laser-induced fusion.

First claim

The invention claimed is:

1. A one-piece screw made by additive manufacturing comprising:
a longitudinal body; and
around the longitudinal body, at least one flight extending in the form of a helix,
wherein the flight comprises, over part of its length, interior partitioning delimiting a plurality of interior canals that extend in the form of helices following the helix shape of the flight and comprising cavities into which the ends of the plurality of interior canals open,
wherein the interior partitioning comprises a core and a plurality of interior partitions that radiate from the core so as to delimit the plurality of interior canals positioned around the core, a first part of the plurality of interior partitions meeting an exterior wall of the flight and a second part of the plurality of interior partitions meeting the outer surface of the longitudinal body, and
wherein the cavities extend radially and open into a longitudinal bore of the longitudinal body at longitudinally spaced locations.

2. The screw according to claim 1 , wherein the plurality of interior partitions have equal thicknesses.

3. The screw according to claim 1 , wherein the exterior wall and the plurality of interior partitions have equal thicknesses.

4. The screw according to claim 1 , wherein the longitudinal body is provided with the longitudinal bore in which splines are provided.

5. The screw according to claim 1 , wherein the longitudinal body comprises a transmission shaft provided with a cylindrical longitudinal bore.

6. The screw according to claim 1 , wherein a combined cross-section of the plurality of interior canals is at least equal to fifty percent of a total cross-section of the flight.

7. A method for manufacturing a screw according to claim 1 , wherein the screw is created by additive manufacturing by deposition and agglomeration of successive layers of powder that are perpendicular to an axis of the screw that is to be manufactured.

8. A method for manufacturing a screw according to claim 1 , wherein the screw is created by additive manufacturing by deposition and agglomeration of successive layers of powder that are parallel to an axis of the screw that is to be manufactured.

9. An assembly comprising:
the screw according to claim 1 ; and
a mounting and transmitting shaft engaged into the longitudinal bore of the screw and secured to the screw and provided with a longitudinal bore.

10. The assembly according to claim 9 , wherein a wall of the mounting and transmitting shaft has radial orifices communicating with the cavities of the screw.

Assignees

• Michelin & Cie

Inventors

• Ougier Christophe
• Letocart Arnaud

Classifications

• B22F10/28

  Powder bed fusion, e.g. selective laser melting [SLM] or electron beam melting [EBM] · CPC title

• B22F10/20

  Direct sintering or melting · CPC title

• B29C48/845 Primary

  Heating · CPC title

• B22F2999/00

  Aspects linked to processes or compositions used in powder metallurgy · CPC title

• B29C48/92

  Measuring, controlling or regulating · CPC title