COMPLEMENTARY STRUCTURE
20180111183 ยท 2018-04-26
Assignee
Inventors
Cpc classification
F04D27/009
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
B21D31/04
PERFORMING OPERATIONS; TRANSPORTING
F23R2900/00018
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
B23K9/0026
PERFORMING OPERATIONS; TRANSPORTING
B21D51/10
PERFORMING OPERATIONS; TRANSPORTING
B21D13/10
PERFORMING OPERATIONS; TRANSPORTING
B21D53/84
PERFORMING OPERATIONS; TRANSPORTING
B23P15/00
PERFORMING OPERATIONS; TRANSPORTING
B21D47/00
PERFORMING OPERATIONS; TRANSPORTING
International classification
B21D53/84
PERFORMING OPERATIONS; TRANSPORTING
F04D27/00
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
Abstract
A method of manufacturing an annular component comprises providing an annular shell to form the outer wall of the component and a plurality of flat annular rings wherein a radially inner edge of each ring is shaped to correspond to a cross-section of the shell at a different position along its length. The method comprises attaching each ring to the ring(s) adjacent to it at a plurality of circumferentially spaced discrete positions. The method comprises deforming each flat annular ring into a corrugated three-dimensional shape, wherein the corrugations extend out of the flat plane and comprise radially defined peaks and troughs. The method comprises locating the shell within the plurality of attached, deformed annular rings. The method comprises attaching the plurality of attached, deformed annular rings to the shell to form the component, so that the plurality of attached, deformed annular rings provide structural reinforcement to the shell.
Claims
1. A method of manufacturing an annular component, the method comprising the steps of: providing an annular shell to form the outer wall of the component; providing a plurality of flat annular rings wherein a radially inner edge of each ring is shaped to correspond to a cross-section of the shell at a different position along its length; attaching each ring to the ring(s) adjacent to it at a plurality of circumferentially spaced discrete positions; deforming each flat annular ring into a corrugated three-dimensional shape, wherein the corrugations extend out of the flat plane and comprise radially defined peaks and troughs; locating the shell within the plurality of attached, deformed annular rings; and attaching the plurality of attached, deformed annular rings to the shell to form the component, so that the plurality of attached, deformed annular rings provide structural reinforcement to the shell.
2. The method according to claim 1, wherein the step of attaching each ring to the ring(s) adjacent to it is performed before the step of deforming each flat ring into a corrugated three-dimensional shape.
3. The method according to claim 2, further providing two flat annular end plates; wherein each flat annular end plate is attached to a flat annular ring, after the step of attaching each ring to the rings adjacent to it; the method further comprises the step of: pulling the two end plates away from each other in order to deform each flat annular ring into the corrugated three-dimensional shape.
4. The method according to claim 1, wherein the step of attaching each ring to the rings adjacent to it is performed after the step of deforming each flat ring into a corrugated three-dimensional shape.
5. The method according to claim 1, wherein the shape of the flat annular rings varies sinusoidally around its circumference.
6. The method according to claim 1, wherein the attachments between each two adjacent rings form a set of connections; and each set of connections is regularly, circumferentially offset from adjacent sets of connections.
7. The method according to claim 1, wherein the shell is frustoconical; and the plurality of rings are formed concentrically from a single sheet.
8. The method according to claim 7, wherein connections are left between rings that form the attachments between adjacent rings.
9. The method according to claim 1, wherein the rings are formed of a conductive material; and the attachments between rings are achieved by applying non-conductive material between adjacent rings at discrete regular locations and applying an electric current through the plurality of rings such that welding of adjacent rings occurs where the non-conductive material is applied.
10. The method according to claim 1, wherein the width of each ring in the radial direction is more than five times the thickness of the ring in the axial direction.
11. The method according to claim 1, wherein each ring forms a corrugated shape within the three-dimensional structure.
12. The method according to claim 11, wherein the distance between the peaks and troughs of the corrugations is equal to or greater than the width of each ring in the radial direction.
13. The method according to claim 1, wherein the shell is metallic; and/or the rings are metallic.
14. A bleed outlet duct comprising: an annular shell which forms an outer wall of the duct; and a plurality of flat annular rings wherein a radially inner edge of each ring is shaped to correspond to a cross-section of the shell at a different position along its length, wherein each ring is attached to the ring(s) adjacent to it at a plurality of circumferentially spaced discrete positions; wherein each flat annular ring is deformed into a corrugated three-dimensional shape, and wherein the corrugations extend out of the flat plane and comprise radially defined peaks and troughs; wherein the shell is located within the plurality of attached, deformed annular rings; and wherein the plurality of attached, deformed annular rings is attached to the shell to form the duct, so that the plurality of attached, deformed annular rings provide structural reinforcement to the shell.
15. An annular component comprising: an annular shell; a complementary structure attached to a radially outer wall of the shell and providing structural reinforcement to it; characterised in that the complementary structure is an expanded three-dimensional structure.
16. The component according to claim 15, wherein the complementary structure comprises a plurality of corrugated annular rings forming a structure extending along an axial direction of the shell.
17. The component according to claim 16, wherein the distance between the peaks and troughs of the corrugations is more than three times the width of each ring in the radial direction.
18. The component according to claim 15, wherein the width of each ring in the radial direction is more than five times the thickness of the ring in the axial direction.
Description
BRIEF DESCRIPTION OF THE DRAWINGS
[0058] Embodiments will now be described by way of example only, with reference to the Figures, in which:
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DETAILED DESCRIPTION OF THE DISCLOSURE
[0069] With reference to
[0070] The cross sections 52 represent the cross sections of the annular component 50 that the annular rings (one of which is shown as a singular annular ring 54) correspond to. The inside edge 56 of the single annular ring 54 matches the shape of the cross section 58. In the complete design, further annular rings would be provided (i.e. a plurality of annular rings) with each ring corresponding to a cross section 52. Cross section 60 is an example of an adjacent cross section to cross section 58. The ring 54 would therefore have an adjacent ring that corresponds to cross section 60. Cross section 58 is adjacent to cross section 60. Cross section 60 is also adjacent to another cross section (not labelled) on the other side to cross section 58.
[0071] In
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[0073] In
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[0075] The attachments 66-71 are evenly (e.g. regularly) circumferentially spaced around the inner edge of the largest ring 63, between the largest ring and the second largest ring. Attachments 66-71 represent a set of connections. In
[0076] The attachments of
[0077] Attachment 72 is part of an adjacent set of connections to the set of connections formed by attachments 66-71. Attachment 72 can be seen to be circumferentially offset from attachments 70 and 71. In
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[0083] A method of manufacturing an annular component with a shell and a complementary structure will now be described with reference to the accompanying drawings. A shell 50 is provided, for example that shown in
[0084] An alternative method of manufacturing an annular component with a shell and a complementary structure will be described with reference to
[0085] It will be understood that the invention 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.