This disclosure relates generally to tooling having a durable metallic surface over an additively formed polymer base layer and a method of forming such tooling.
The manufacture, assembly, maintenance, modification and/or upgrade to an aircraft always requires the creation of tools used to make parts for the aircraft. This tooling is often machined from solid metal in order to ensure the surface quality, surface robustness and durability thereof. However, the preparation and construction of such metallic tooling can be costly and time-intensive. Additively manufactured polymer tooling can be manufactured much more quickly and inexpensively than tooling formed from metals, but the durability, surface quality and surface robustness of polymer-based tooling is a concern.
Accordingly, there is a need for an improved method of forming tooling which can be formed more quickly like additively formed polymer tooling and which also provides the surface quality, surface robustness and durability provided by metallic tooling.
In one aspect, a tool has a base layer additively formed from a polymer material in a desired tool shape. A sealant layer is formed over an outer surface the base layer, the sealant being electrically conductive. Finally, a metallic coating is formed over the sealant layer.
The sealant may be a low-modulus material, such as a silicone rubber or an elastomer. Preferably, the sealant is made electrically conductive by the addition of a filler material added to the sealant. The filler material may be one of carbon black, carbon fibers, graphene, carbon nanotubes, metal whiskers, or other conductive materials and combinations therefrom. The metallic coating may be a multilayer metallic coating. The metallic coating may be formed by electroplating or by electrodeposition.
In another aspect, a tool has a base layer additively formed from a polymer material in a desired tool shape. A sealant layer is formed over an outer surface the base layer, the sealant being not electrically conductive. An electrically conductive layer is formed over the sealant layer. Finally, a metallic coating is formed over the electrically conductive layer.
In a third aspect, a method of forming a tool. A base layer is formed in a desired tool shape additively from a polymer material. A sealant layer is formed over an outer surface the base layer, the sealant being electrically conductive. Finally, a metallic coating is formed over the electrically conductive layer.
In a fourth aspect, a method of forming a tool. A base layer is formed in a desired tool shape additively from a polymer material. A sealant layer is formed over an outer surface the base layer, the sealant being a low-modulus material comprising a silicone rubber or an elastomer. An electrically conductive layer is formed over the sealant layer. Finally a metallic coating is formed over the electrically conductive layer.
The features, functions, and advantages that have been discussed can be achieved independently in various embodiments or may be combined in yet other embodiments, further details of which can be seen with reference to the following description and drawings.
The following detailed description, given by way of example and not intended to limit the present disclosure solely thereto, will best be understood in conjunction with the accompanying drawings in which:
In the present disclosure, like reference numbers refer to like elements throughout the drawings, which illustrate various exemplary embodiments of the present disclosure.
Referring now to the drawings, and in particular to
In
In
In
Referring now to
The tooling of the present disclosure includes a metallic outer coating which is robustly attached to the underlying substrate (as described above) in a manner that prevents debonding, spalling, or cracking of such outer coating during use of the tooling. In particular, the tooling formation described herein allows for very strong bonds to be created between the metallic outer coatings and the underlying substrate. Additionally, the addition of the low-modulus material between the underlying substrate and the metallic outer coating accounts for mismatches in the coefficient of thermal expansion (CTE) of these dissimilar materials, which often occur when the tooling is used at high temperatures, such as during the cure of a thermoset composite. As such, the addition of the low-modulus material between the underlying substrate and the metallic outer coating also serves to prevent debonding, spalling, or cracking of the metallic outer coating during use of the tooling at high temperature (e.g., a high-temperature cure).
Although the present disclosure has been particularly shown and described with reference to the preferred embodiments and various aspects thereof, it will be appreciated by those of ordinary skill in the art that various changes and modifications may be made without departing from the spirit and scope of the disclosure. It is intended that the appended claims be interpreted as including the embodiments described herein, the alternatives mentioned above, and all equivalents thereto.
Number | Name | Date | Kind |
---|---|---|---|
8778498 | Tsotsis | Jul 2014 | B1 |
8916248 | McCrea et al. | Dec 2014 | B2 |
20110020631 | Miller et al. | Jan 2011 | A1 |
20120234681 | Lomansney et al. | Sep 2012 | A1 |
20140004352 | McCrea et al. | Jan 2014 | A1 |
20140030592 | Maegawa et al. | Jan 2014 | A1 |
20160002790 | Whitaker et al. | Jan 2016 | A1 |
20160002813 | Lomasney | Jan 2016 | A1 |
20160009051 | Tsotsis | Jan 2016 | A1 |
20160288372 | Tsotsis | Oct 2016 | A1 |
Number | Date | Country |
---|---|---|
2254820 | Oct 1992 | GB |
Entry |
---|
European Patent Office Extended Search Report dated Aug. 11, 2017 for Application No. 17151815.2. |
Number | Date | Country | |
---|---|---|---|
20170283972 A1 | Oct 2017 | US |