Multiple Part Component and Method of Assembly
20180209458 ยท 2018-07-26
Assignee
Inventors
Cpc classification
F16B5/08
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
International classification
Abstract
This application describes a manufactured component and method for forming the component. The component comprises: a plurality of parts (212, 214) joined together by a straight line joint (216) and a multi-faceted joint (218). The plurality of parts define a cavity (236) having an internal surface (226) and an external (222) surface. The straight line joint extends through a wall of the component along a straight line between the external surface the internal surface; and, the multi-faceted joint includes an external joint line extending from an external surface to meet an internal joint line which extends from an internal surface, the external and internal joint lines being at an angle to one another. The internal joint line and the straight line joint are aligned with one another such that a straight line extending from the straight line joint will coincide with the internal joint.
Claims
1. A manufactured component, comprising: a plurality of parts joined together by a straight line joint and a multi-faceted joint, the plurality of parts defining a cavity having an internal surface and an external surface; wherein the straight line joint extends through a wall of the component along a straight line between the external surface and the internal surface; and, the multi-faceted joint includes an external joint line extending from the external surface to meet an internal joint line which extends from the internal surface, the external and internal joint lines being at an angle to one another, wherein the internal joint line and the straight line joint are aligned with one another such that a straight line extending from the straight line joint will coincide with the internal joint line.
2. A manufactured component as claimed in claim 1, wherein the component includes a plurality of walls interconnected at nodes, wherein the multi-faceted joint is located at a node.
3. A component as claimed in claim 1, wherein the angle between a through-thickness line of the external joint line and a through-thickness line of the internal joint line lie between 60 and 135 degrees to one another.
4. A component as claimed in claim 1, wherein one part of the plurality of parts includes a node and two walls extending therefrom to respective free ends, wherein at least a portion the respective free ends include end faces which lie in a common plane to one another to provide a straight line joint surface and an internal joint surface.
5. A component as claimed in claim 1 wherein the internal joint line of the multi-faceted joint is shorter than the external joint line.
6. A component as claimed in claim 1, wherein the cavity is substantially triangular in a cross-section.
7. A component as claimed in claim 1, wherein the straight line which extends between the straight line joint and the internal joint line is parallel to a wall of the cavity.
8. A method of manufacturing a hollow component having an internal surface and an external surface, the method comprising: providing a plurality of parts for assembly, each part including a joint surface for joining with another of the plurality of parts; assembling the plurality of parts to provide a preform having: a multi-faceted joint which includes an external joint line extending from an external surface to meet an internal joint line which extends from an internal surface, the external and internal joint lines being at an angle to one another; and, a straight line joint which extends from an external surface to an internal surface along a straight line wherein the straight line joint and internal joint lie along a common line; using a first beam to weld the straight line joint and the internal joint line of the multi-faceted joint, and, using a second beam to weld the external joint line of the multi-faceted joint.
9. A method as claimed in claim 8, wherein the beams are electron beams.
10. A method as claimed in claim 8, wherein the first beam and second beam are at an angle of between 60 and 135 degrees.
11. A method as claimed in claim 10, wherein the first beam and second beam are provided at right angles to one another.
12. A method as claimed in claim 8, wherein the plurality of parts are machined prior to being assembled.
Description
BRIEF DESCRIPTION OF THE DRAWINGS
[0027] Embodiments of the invention will now be described with the aid of the following drawings of which:
[0028]
[0029]
[0030]
[0031]
[0032]
[0033]
DETAILED DESCRIPTION OF THE DRAWINGS
[0034]
[0035] The multi-faceted joint is in the form of a rebate joint 218 which is more clearly shown in
[0036] Returning to
[0037] The separation between the internal joint and straight line joint may be any which allow a successful weld. Typically, the range would be somewhere between 10 mm and 300 mm. The internal joint 224 may have a length anywhere between the weld thickness of the external joint, and approximately twice the length of the straight line joint. The internal joint may be terminated with a thickness of greater than 2 mm of the internal joint length to allow the energy beam sufficient depth to dissipate without breaking through. However, the internal joint may break through in some instances. In such a case, the multifaceted joint may be a T shaped joint with the internal line extending between an internal surface and an external surface, and the external line terminating at or beyond the internal joint line.
[0038]
[0039] The welds could be done in any sequence but the advantage of doing the straight line and internal joint in a first weld is that it fixes the position of rebate joint and prevents any deleterious movement. Welding with the external joint of the rebate joint first could result in the straight line joint moving resulting in some misalignment.
[0040] The energy beam may be an electron beam which is particularly suited to through-welding of multiple joints simultaneously. Laser beams may also be used.
[0041] It will be appreciated that the laser or electron beam will be moved along the component welding the joints along the length or circumference of the component.
[0042] Returning to
[0043] The cavity 236 is defined predominantly by three walls arranged in triangular formation which is substantially isosceles having a base 232 and two sides 230, 234, extending therefrom. In the case of an annular component as shown in
[0044] The rebate joint 218 may be formed from two or more abutting surfaces which are provided by two or more different parts. The rebate may be in any form which comprises intersecting transverse straight joint lines. The rebate may from a notch in one of the wall lengths or a node. The notch may be in the form of a step or v-shaped. The notch may have orthogonal surfaces or facets arranged at an angle to one another. The surfaces may be at any angle to one another which provides sufficient angular change that the two joint lines may be welded with separate beams.
[0045] The angle may be between 60 and 135 degrees but will typically be an angle which aids location of the two components by offering some positive engagement and which also does not obstruct the energy beam welding process. In the example shown the angle is approximately 90 degrees.
[0046] One or other of the external or internal joint surfaces fulfills two functions. The first is to provide a location feature for locating and seating the components together. The second is to provide an end stop of material for the weld beam to dissipate into without breaching the confines of the component.
[0047] The external joint surface and internal joint surface may be similar or different lengths. For example, one of the internal or external joint surfaces may be significantly shorter than the other. Typically, the shorter joint line will be the internal one to reduce the energy required of the beam which welds the straight line joint. The internal joint may be approximately half the length of the external joint.
[0048] The walls of the component which define the cavity may be split between the two components in any ratio, provided the straight line first joint and internal joint of the rebate joint can be concentrically aligned. Thus, as shown in
[0049] The second component includes a single wall extending between two nodes. This wall does not include any joints.
[0050] The line or plane along which the straight line joint and internal joint of the rebate extend may lie parallel to one of the walls or another feature of the component which can be readily used as a reference plane for holding the component in an energy beam welding device or fixture. Providing this relation between the joint line and an external feature allows the combined weld line to be aligned to an axis of the machine which can simplify the movement of the energy beam source.
[0051]
[0052] As with the previous example, the line of the internal surface joins are concentric with the straight line of the first joint. Hence, a cross cavity extension to straight line of the first joint coincides with the internal joint of the rebate joint. This alignment allows the internal joint of the rebate joint to be welded simultaneously with the first joint and using the same energy beam. The external joint of the rebate joint is subsequently, or previously, welded with a second beam. Here the angle between the internal surface joint line and external surface joint line is around 135 degrees.
[0053]
[0054]
[0055] Thus, as can be seen in
[0056] In
[0057] Typically, lateral offset will be less than 0.5 mm and angular misalignment between the line of the internal joint and the beam line will be less than 45 degrees.
[0058] The internal and external surfaces of the parts of the component may be machined prior to assembly into a pre-weld preform.
[0059] It will be appreciated that the various joints are described in relation to lines in the transverse section and their associated two dimensional surfaces. It will be appreciated that the surfaces or facets which provide the joint surfaces may lie in planes in which case the straight line joint and internal surface joint of the rebate joint may lie in a common plane. However, where the joint extends along a curved path, the surfaces will not be planar but there will continue to be a straight line between straight line joint and a first end of the internal surface joint of the rebate joint such that the two joins can be fused simultaneously and with a common beam.
[0060] The above described example contemplates the invention being used on a simple annular structure. However, the multipart component may include many different parts which may include many different walls and nodes between the walls and multiple joins.
[0061] It will be understood that the invention is not limited to the described examples and embodiments and various modifications and improvements can be made without departing from the concepts described herein and the scope of the claims. Except where mutually exclusive, any of the features may be employed separately or in combination with any other features in the disclosure extends to and includes all combinations and sub-combinations of one or more described features.