Patent Application
20200224980
This disclosure relates generally to brackets attached to a heat exchanger core and more particularly to a system and method of attaching plastic brackets to a heat exchanger core after a heat exchanger core brazing process.
As known, heat exchangers are employed to cool fluids flowing through the vehicle. Examples of heat exchangers include condensers and radiators. Components of the heat exchangers include a heat exchanger core configured to exchange heat between fluids or materials and a header coupled to and in communication with the core. Conduits are coupled to the headers to convey fluids to the headers. Many of the components of the heat exchanger are formed from a metal such as aluminum and are assembled together by a brazing process.
The heat exchangers are commonly mounted to the vehicle body structure or other components of the vehicle, directly or indirectly, by a bracket. Typically, the bracket is coupled to the heat exchangers before or during the brazing of the heat exchanger. The bracket is coupled to the heat exchanger such as to the headers. Further, the bracket can be reinforced to or separately connected to the heat exchanger by rivets or fasteners.
However, the current bracket structures and methods of coupling the bracket can be disadvantageous. Particularly, it may be desired to increase a complexity, strength, and functionality of the bracket depending on the space and structure available to mount the heat exchanger to the vehicle. However, an increase in complexity, strength, and functionality the bracket may undesirably increase a weight and a cost of the heat exchanger when demand requires minimized weight and cost of the heat exchanger. Additionally, a hole is typically required in the heat exchanger for the rivet or fastener of the bracket when the bracket is coupled to the heat exchanger by rivets or fasteners. The hole is susceptible to leaking. Furthermore, it is often desired to minimize a package size of the heat exchanger due to limited space requirements. Minimizing the package size of the heat exchanger can be difficult to accomplish with current brackets and methods of coupling the brackets to the heat exchangers.
Therefore, it is desired to have a bracket and method of coupling the bracket to the heat exchanger after a brazing process of the heat exchanger, wherein the bracket minimizes leakage, a cost, a weight, and a package size of the heat exchanger while maximizing complexity, strength, and functionality of the bracket.
In accordance and attuned with the present invention, a plastic bracket and method of coupling the bracket to the heat exchanger that minimizes leakage, a cost, a weight, and a package size of the heat exchanger while maximizing complexity, strength, and functionality of the bracket has surprisingly been discovered.
According to an embodiment of the disclosure, a heat exchanger for a vehicle includes a heat exchanger core. The heat exchanger core is configured to exchange heat between fluids. The heat exchanger further includes a header. The header is in fluid communication with the heat exchanger. A bracket is coupled to the header by a cold forming process.
According to another embodiment of the disclosure, a heat exchanger for a vehicle includes a heat exchanger core and header assembly configured to exchange heat between fluids. The heat exchanger core and header assembly includes an outer surface. A bracket is coupled to the outer surface of the heat exchanger core and header assembly by a cold forming process. A weld joint is formed between the bracket and the outer surface of the heat exchanger core and header assembly by the cold forming process.
According to yet another embodiment of the disclosure, a method of assembling a heat exchanger and a bracket is disclosed. The method includes the step of assembling a heat exchanger core and a header to the heat exchanger core by a first process. The method additionally includes the step of coupling a bracket to an outer surface of the assembled heat exchanger core and the header by a second process after the first process, wherein the second process is a cold forming process.
The above objects and advantages of the invention, as well as others, will become readily apparent to those skilled in the art from reading the following detailed description of an embodiment of the invention when considered in the light of the accompanying drawings, in which:
The following detailed description and appended drawings describe and illustrate various exemplary embodiments of the invention. The description and drawings serve to enable one skilled in the art to make and use the invention, and are not intended to limit the scope of the invention in any manner. In respect of the methods disclosed, the steps presented are exemplary in nature, and thus, the order of the steps is not necessary or critical unless otherwise noted.
A” and “an” as used herein indicate “at least one” of the item is present; a plurality of such items may be present, when possible. As used herein, “substantially” means “to a considerable degree,” “largely,” or “proximately” as a person skilled in the art in view of the instant disclosure would understand the term. Spatially relative terms, such as “front,” “back,” “inner,” “outer,” “bottom,” “top,” “horizontal,” “vertical,” “upper,” “lower,” “side,” and the like, may be used herein for ease of description to describe one element or feature's relationship to another element(s) or feature(s) as illustrated in the figures. Spatially relative terms may be intended to encompass different orientations of the device in use or operation in addition to the orientation depicted in the figures.
Although the terms first, second, third, etc. may be used herein to describe various elements, components, regions, layers and/or sections, these elements, components, regions, layers and/or sections should not be limited by these terms. These terms may be only used to distinguish one element, component, region, layer or section from another region, layer or section. Terms such as “first,” “second,” and other numerical terms when used herein do not imply a sequence or order unless clearly indicated by the context. Thus, a first element, component, region, layer or section discussed below could be termed a second element, component, region, layer or section without departing from the teachings of the example embodiments.
The heat exchanger 10 includes a pair of tanks or headers 12 and a heat exchanger core 14. The tanks 12 are elongated conduits arranged in a substantially parallel relationship to each other. The tanks 12 convey a flow of fluid such as an inlet flow of fluid and outlet flow of fluid. The fluid can be a fluid configured for heat exchange such as a coolant, refrigerant, water, or any other fluid or material. The tanks 12 can be integrally or separately formed from the heat exchanger core 14. Additionally, the evaporator 10 can have any number of tanks 12 containing the fluid, as desired. The tanks 12 are arranged at opposing ends of the heat exchanger core 14. However, the tanks 12 can be arranged in any order or configuration as desired such as adjacent each other or at other portions of the heat exchanger 10. The tanks 12 are formed from a metal such as aluminum, for example. However, it is understood the tanks 12 can be formed from other materials such as plastic, if desired.
The heat exchanger core 14 is a tube and fin arrangement heat exchanger core. The heat exchanger core 14 includes a plurality of substantially parallel rows of tubes or plates 16 extending from and in fluid communication with the tanks 12. The rows of plates 16 are arranged transversely to the direction of a flow of air through the heat exchanger 10. A plurality of fins 18 are arranged substantially parallel with each other and interposed between the rows of plates 16. The fins 18 are configured to receive the flow of air through the heat exchange core 14.
Other components (not shown) can be included with the heat exchanger 10 such as seals, additional headers or tanks, valves, conduits, gauges or other components commonly included with heat exchangers. The plates 16, the fins 18 and other components are coupled together to form the heat exchanger 10. A brazing process using a clad brazing material that melts under heat to join components together is employed to couple the heat exchange core 14 together and to the tanks 12. However, it is understood other coupling means in addition too or separate from the brazing process can be employed to couple the tanks 12, the heat exchange core 14, and the other components to each other to from the heat exchanger 10.
The heat exchanger 10 has an outer surface 20. The outer surface 20 can have varying surface contours. For example, the tanks 12 can have a generally planar outer surface 22, as illustrated at one of the tanks 12 in
The bracket 30 includes a flange portion 32 for directly engaging the outer surface 20 of the heat exchanger 10 and a structure supporting portion 34 for engaging the vehicle structure. The bracket 30 is coupled to the outer surface 20 of the heat exchanger 10 by a cold gas welding process, described in further detail below with reference to a method of coupling the bracket 30 to the heat exchanger 10. A weld joint 36, schematically represented by the dashed lines, is applied to the bracket 30 and/or the heat exchanger 10 to join the bracket 30 to the heat exchanger 10.
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It is understood, the bracket 30 can be any combination of features illustrated in
The bracket 30 is coupled to the heat exchanger 10 at the weld joint 36 by a cold forming process. As used herein a cold forming process is a cold spray process, high pressure cold spray process, or coating deposition method. According to the cold forming process, solid powder particulates of material or fill material are accelerated in a supersonic gas jet to velocities up to 500-1000 meters per second, for example, towards a substrate such as the heat exchanger 10 or the bracket 30, to form the weld joint 36. Although, other velocities can be contemplated. The gas is nitrogen or helium having a pressure greater than 1.5 megapascals (MPa), a flow rate greater than 2 cubic meters per minute, and a heating power greater or equal to 18 kilowatts. The particulates have a diameter in a range of about 1 to 50 micrometers or 5-50 micrometers for high pressure cold spray. The particulates may be formed from materials such as metals, polymers, ceramics, nano-crystalline, or combinations of the same or alternate materials.
During impact of the particulates with the substrate, the particulates undergo plastic deformation and adhere to a surface of the substrate due to expansion of the gas in the gas jet. To achieve a uniform thickness of the particulates on the substrate, a spraying nozzle is employed to direct the particulates along the substrate along a desired path to form the weld joint 36. The kinetic energy of the particulates, supplied to the substrate by the expansion of gas, is converted to plastic deformation energy during bonding of the particulates to the substrate. The cold forming process is different from thermal spraying techniques (e.g. plasma spraying, arc spraying, flame spraying, or high velocity oxygen fuel spraying) because the particulates are not melted during the spraying step of the process.
Advantageously, unlike other additive manufacturing methods and processes such as selective laser melting or electron beam additive manufacturing, the cold forming process does not melt metals or alternate materials. As a result, components and structures formed from metal materials are not affected by heat-related distortion and the parts do not need to be manufactured in an inert gas or vacuum sealed environment. Therefore, larger components and structures that may be formed from materials that are typically difficult to braze or join with other components and structures can be easily joined or brazed with the cold forming process. Advantageously, the cold forming process also permits non-metallic materials to be easily joined to metallic or non-metallic materials easily.
According to the instant disclosure, the bracket 30 can be formed from a plastic material or a metal as desired without concern whether the material the bracket 30 is formed from will deform. With the cold forming process, the bracket 30 is joined to the heat exchanger 10 after the heat exchanger 10 is formed and assembled by a brazing process. A strength and an integrity of the assembled heat exchanger 10 are not compromised by joining the bracket 30 thereto after the heat exchanger 10 is assembled. The joining of the bracket 30 to the assembled heat exchanger 10 after the brazing process of the heat exchanger 10 minimizes distortion of damage to the assembled heat exchanger 10.
The steps for the assembly of the heat exchanger 10 and the bracket 30 are shown in
The bracket 30 assembled to the heat exchanger 10 according to the present disclosure can be formed from materials, such as plastic, permitting the brackets 30 to have a more complex configuration with greater functionality while minimizing costs and a weight of the bracket 30. The brackets 30 of the present invention are not required to be assembled to the heat exchanger 10 prior to or during the brazing of the heat exchanger 10. Rather, the bracket 30 can be assembled to the heat exchanger 10 after the brazing of the heat exchanger 10.
The foregoing discussion discloses and describes merely exemplary embodiments of the present disclosure. One skilled in the art will readily recognize from such discussion and from the accompanying drawings and claims that various changes, modifications and variations can be made therein without departing from the spirit and scope of the disclosure as defined in the following claims.
