MANUFACTURING METHOD
20190193161 ยท 2019-06-27
Assignee
Inventors
Cpc classification
B33Y10/00
PERFORMING OPERATIONS; TRANSPORTING
A61F2/3609
HUMAN NECESSITIES
B29C64/40
PERFORMING OPERATIONS; TRANSPORTING
B33Y40/20
PERFORMING OPERATIONS; TRANSPORTING
B22F7/08
PERFORMING OPERATIONS; TRANSPORTING
B23K26/34
PERFORMING OPERATIONS; TRANSPORTING
B22F10/28
PERFORMING OPERATIONS; TRANSPORTING
B33Y80/00
PERFORMING OPERATIONS; TRANSPORTING
B22F10/25
PERFORMING OPERATIONS; TRANSPORTING
B22F7/06
PERFORMING OPERATIONS; TRANSPORTING
B28B1/001
PERFORMING OPERATIONS; TRANSPORTING
B22F3/24
PERFORMING OPERATIONS; TRANSPORTING
B22F3/1208
PERFORMING OPERATIONS; TRANSPORTING
B22F10/47
PERFORMING OPERATIONS; TRANSPORTING
B29C64/153
PERFORMING OPERATIONS; TRANSPORTING
Y02P10/25
GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
International classification
B33Y10/00
PERFORMING OPERATIONS; TRANSPORTING
B29C64/40
PERFORMING OPERATIONS; TRANSPORTING
B28B1/00
PERFORMING OPERATIONS; TRANSPORTING
B22F3/105
PERFORMING OPERATIONS; TRANSPORTING
B33Y40/00
PERFORMING OPERATIONS; TRANSPORTING
B29C64/153
PERFORMING OPERATIONS; TRANSPORTING
Abstract
There is provided a method of manufacture of a component from multiple materials, and a consolidated component formed thereby. The method includes the steps of forming a component body comprising a first material, the component body defining a cavity, filling at least a portion of the cavity with a second material, and performing hot isostatic pressing of the component body and second material to form a consolidated component. The process offers a reduced-complexity, reduced-part-count method of manufacture for components formed of multiple materials.
Claims
1. A method of manufacturing a component from multiple materials including the steps of: forming a component body comprising a first material, the component body defining a cavity; filling at least a portion of the cavity with a second material; and performing hot isostatic pressing of the component body and second material to form a consolidated component.
2. The method of manufacturing according to claim 1 wherein the second material is a powder material.
3. The method according to claim 1 comprising forming the component body using an additive manufacturing process.
4. The method according to claim 3 wherein the additive manufacturing process is one of laser/electron beam melting/sintering, powder bed fusion, 3D printing, selective laser sintering/melting, a blown powder process, direct laser deposition, freeform manufacture, or additive layer manufacturing.
5. The method according to claim 1 comprising forming the component body by machining.
6. The method according to claim 1 comprising forming the component body comprising one or more sacrificial portions which partly define the cavity.
7. The method according to claim 6 further comprising removing the sacrificial portion(s) of the component body after the step of performing hot isostatic pressing.
8. The method according to claim 1 comprising forming the component body as a net or near-net shape component.
9. A consolidated component formed by the method according to claim 1.
Description
DESCRIPTION OF THE DRAWINGS
[0030] Embodiments will now be described by way of example with reference to the accompanying drawings in which:
[0031]
[0032]
[0033]
[0034]
DETAILED DESCRIPTION
[0035]
[0036]
[0037] The component body 101 is formed to define a cavity 107. Here, the component body 101 is formed to be a near-net shape component comprising sacrificial portions 109. In the present example, the cavity in the component body is partially defined by these sacrificial portions of the component body, and partially defined by non-sacrificial portions. The shape of the cavity is selected so as to control deformation during the hot isostatic pressing step.
[0038] In
[0039] The entire component then undergoes a hot isostatic pressing cycle, during which the second material powder 111 densifies and bonds to the component body 101 at the cavity walls, thereby forming a consolidated component 120.
[0040] Post-densification, the consolidated component is further processed (e.g. machined) to remove sacrificial portions 109 of the component body, along with excess second material. The final product, shown in
[0041]
[0042] In the same manner as discussed in relation to the previous example, once the cavity 207 has been filled with powder 211 the component undergoes a hot isostatic pressing cycle to form the consolidated component 220 followed by removal of sacrificial portions of the component body. The final product is a consolidated component comprising a pipe body portion 215 of a first material having exposed integrated interior surface cladding 217 of a second material at the location of the original cavity.
[0043]
[0044] In the same manner as discussed in relation to the previous example, the component undergoes a hot isostatic pressing cycle to form the consolidated component 320 followed by removal of sacrificial portions of the component body. The final product is a consolidated component comprising a hip joint body portion 315 of a first material having an integrated surface covering 317 of a second material at the location of the original cavity.
[0045] It will be understood that the disclosure is not limited to the embodiments above-described and various modifications and improvements can be made without departing from the concepts described herein. Except where mutually exclusive, any of the features may be employed separately or in combination with any other features and the disclosure extends to and includes all combinations and sub-combinations of one or more features described herein.