Friction stirring interlocking of dissimilar materials
10369748 ยท 2019-08-06
Assignee
Inventors
- Scott A. Whalen (Richland, WA, US)
- MD. Reza-E-Rabby (Richland, WA, US)
- Kenneth A. Ross (West Richland, WA, US)
- Aashish Rohatgi (Richland, WA, US)
Cpc classification
B23K20/129
PERFORMING OPERATIONS; TRANSPORTING
B29C66/1122
PERFORMING OPERATIONS; TRANSPORTING
B29C66/7212
PERFORMING OPERATIONS; TRANSPORTING
B23K2103/20
PERFORMING OPERATIONS; TRANSPORTING
B29C66/7212
PERFORMING OPERATIONS; TRANSPORTING
B23K20/127
PERFORMING OPERATIONS; TRANSPORTING
B21J15/027
PERFORMING OPERATIONS; TRANSPORTING
B29C66/45
PERFORMING OPERATIONS; TRANSPORTING
B29C66/7422
PERFORMING OPERATIONS; TRANSPORTING
B29C66/21
PERFORMING OPERATIONS; TRANSPORTING
International classification
B23K20/12
PERFORMING OPERATIONS; TRANSPORTING
B29C65/06
PERFORMING OPERATIONS; TRANSPORTING
Abstract
A method for solid state joining of dissimilar materials using a friction stir welding device wherein a pin is inserted through an aperture defined in a first material and a second material to hold the materials together and then held in place by friction stir welding a portion of the pin to a material adjacent said pin, or by friction stir welding a cap or plug that holds the pin in place to the adjacent material. The result is a connection or join wherein the central portion of the pin is not friction stir welded but the portions holding the pin in place (the ends or caps) generally are.
Claims
1. A method for solid state joining of dissimilar materials using a friction stir welding device, the method comprising the steps of: inserting a pin having two ends within an aperture defined in a first material and a carbon reinforced composite material; and friction stir welding each end of the pin to a portion of the first material.
2. The method of claim 1 wherein said first material is aluminum.
3. The method of claim 1 wherein said first material is steel.
4. The method of claim 1 wherein said first material is configured in to a C-shape, and the carbon reinforced composite material is embodied in an insert configured to fit within said C-shaped material.
5. A method for solid state joining of dissimilar materials using a friction stir welding device comprising the steps of: inserting an insert within an aperture defined in a first material made of aluminum configured into a C-shape and a second material embodied in an insert configured to fit within said C-shape, and friction stir welding a portion of said insert to a material adjacent to said insert.
6. The method of claim 5 wherein said second material is steel.
7. The method claim 5 wherein said second material is a carbon reinforced composite.
8. The method of claim 5 wherein said insert is a pin has two ends and is friction stir welded in each end to the first material.
9. The method of claim 5 wherein said first material is aluminum and said second material is steel.
10. The method of claim 5 wherein said first material is steel and said second material is aluminum.
Description
BRIEF DESCRIPTION OF THE DRAWINGS
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DETAILED DESCRIPTION
(9) The following description includes examples of various embodiments of the present disclosure. It will be clear from this description of that the invention is not limited to these illustrated embodiments but also includes a variety of modifications and embodiments thereto. Therefore, the present description should be seen as illustrative and not limiting. There is no intention in the specification to limit the invention to the specific form disclosed, but, on the contrary, the invention is to cover all modifications, alternative constructions, and equivalents falling within the spirit and scope of the invention as defined in the claims.
(10) Friction Stir Interlocking (FSI) is a new methodology for joining dissimilar materials such as lightweight metals to composites, thermoset plastics, or other non-metallic materials. Metals with vastly different melting temperatures which cannot be joined by conventional welding can also be joined by FSI. Currently the state-of-the-art for joining Mg and Al to carbon fiber (CF) and other non-metal is conventional mechanical fastening and adhesive bonding. Solid-phase approaches such as Friction Stir Welding, Scribe, Riveting, Pillaring and Spot Welding are all being investigated but face significant challenges with joint strength, fatigue, damaging the carbon fiber materials, slow process speed and galvanic corrosion. The FSI process described herein provides solutions to many of these issues.
(11) In one embodiment shown in
(12) In a variety of other embodiments are variety of other shapes, patterns and cross sections for the various pins 12 and corresponding holes 14 through which they can be inserted. As a friction stir process, numerous interlocks can be created quickly and uniformly, in a single pass, offering reduced cost and improved process efficiency compared to conventional metal-to-non-metal fasteners. Galvanic corrosion between the metal fasteners and carbon fibers can be nearly eliminated using FSI. In many instance the short process time (a few seconds) and low process temperature (as low as 250 C. for Mg) make this friction stir interlocking FSI approach attractive for joining Mg and Al to carbon fiber CF without substantially degrading the CF material properties.
(13) In another embodiments of the invention (shown in the various
(14) In other embodiments the plate of insert material such as Mg. or Al can be placed over a CFRP or CFRC assembly and then friction stir wielded along a weld path joining the plate to the insert embedded during fabrication of the CFRP or CFRC. Linear inserts such as these that are shown are can be advantageous because they provide a continuous joint along the dissimilar interface. Spot welding inserts using similar methods could also be embedded during the manufacturing of the carbon fiber composite. Forming carbon fiber composites around inserts allow for resign to adhere to the insert and allow for mechanical interlocking. This method allows for faster FSW processes and reduces heat input into carbon fiber.
(15) In other variations, magnesium overcasting can be performed using any of a variety of metals such as Mg or Al and alloys thereof. In one particular instance a high-pressure die cast (HPDC) Mg alloy is directly cast over a short section of the CFRC component such that the carbon fiber reinforced composite CFRC section is completely embedded within the Mg casting to create a strong mechanical interlocking joint. Embedded inserts may also be used to enhance joint strength. Although CFRC will in general burn/decompose easily at the temperature corresponding to the melting point of Mg alloys (T>600 C), rapid solidification of molten Mg (i.e. within 1-2 seconds) and subsequent cooling during HPDC will sufficiently limit the surface decomposition of the bulk CFRP to form a robust mechanical joint.
(16) The advantage of the Mg-CFRC overcasting method is that it avoids the need for machining or disturbance of the casting or CFRC while enabling joint geometries that are otherwise cumbersome to machine or not feasible by conventional mechanical fastening methods. While challenges may arise in creating a Mg-CFRC joint by overcasting because of the burn-off/thermal decomposition of the CFRC composite when it comes in contact with molten Mg and also during subsequent cooling of the solidified casting. This challenge can be addressed in two ways: 1) the Mg solidification rate is controlled to minimizing the duration for which the CFRC is exposed to temperature above its thermal decomposition temperature and (2) temperature-resistant coatings (e.g. graphite, boron nitride, etc.) on the CFRP are used to prevent erosion via direct contact with flowing molten metal.
(17) In other circumstances, various other interlocking configurations and applications are shown.
(18) In one example shown in
(19) In another embodiment of the invention the aluminum pin 12 is replaced with a steel pin 12 and the approach is to lock the steel pin into the aluminum via friction stir welding. This is done by FSW through aluminum plugs 22 inserted on each side of the steel pin 12 as shown in
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(21) While various preferred embodiments of the invention are shown and described, it is to be distinctly understood that this invention is not limited thereto but may be variously embodied to practice within the scope of the following claims. From the foregoing description, it will be apparent that various changes may be made without departing from the spirit and scope of the invention as defined by the following claims.