This disclosure relates generally to tube-and-fin style heat exchangers. More particularly, this disclosure relates to a bullet nose grommet for facilitating assembly of a radiator formed by a plurality of tube-and-fin assemblies mounted between coolant manifolds.
Large heavy duty machines, such as dozers, loaders and excavators, require large radiators for engine cooling. One common radiator design is the tube-and-fin structure, where numerous tube-and-fin assemblies are mounted to upper and lower coolant manifolds and arranged in columns and rows. Copper grommetted tube (CGT) radiators, in which copper tube-and-fin assemblies are secured to coolant manifolds or other radiator components, are expensive. The pursuit of cost reduction in manufacturing the machines has led to the development of aluminum grommetted tube (AGT) radiators. Aluminum is less expensive and lighter than copper than copper, but is less malleable.
The tube-and-fin assemblies that make up a CGT or AGT radiator are secured to the coolant manifolds and sealed thereto with flexible grommets or seals. Each of the tubes may comprise an annular bead extending outwardly around a lower end of the tube, and each of the seals includes a circumferential groove for receiving the bead and holding the tube-and-fin assembly in place. One such tube and seal construction radiator disclosed in U.S. Pat. No. 3,391,732 issued to Murray on Jul. 29, 1966, includes upper and lower radiator tank members having holes in the lower and upper surfaces, respectively, with removable lengths of finned conduit extending there between and resilient grommets positioned in the holes so as to surround the conduits adjacent the ends thereof to prevent leakage there around. A radially outwardly extending flange is formed adjacent the lower end of each of the conduits and the lower grommets have grooves in the inner surfaces thereof. The grooves receive the flanges on the conduits and substantially prevent inadvertent disengagement of the conduits from the holes. Additional combinations of radiator constructions having conduits with conduit ends engaged by grommets or seals to retain the conduit ends within openings of a header plate are disclosed in U.S. Pat. No. 5,433,268 issued to Janezich et al. on Jul. 18, 1995.
In tube and grommet combinations such as those taught in the references cited above, the body of the grommet is typically fabricated from rubber or other resilient material, and has an outer diameter that is greater than the inner diameter of the opening through the header plate so that the grommet fits tightly within the opening when the grommet is inserted therein. This dimensional relationship assists in ensuring a tight seal between the grommet and the header plate, but can cause issues during assembly of the radiators. The bottom edge of the grommet is larger than the opening in which the grommet will be installed, and an interference relationship exists when the grommet is lined up with the opening. When a force is applied to press the grommet into the opening, the force must compress the grommet until the force overcomes the interference between the bottom edge of the grommet and the outer surface of the header plate. The required force is further increased when the grommet is misaligned with the header plate opening, and the grommet may even fall over or partially fall into the opening and require repositioning before the grommet can be installed in the opening. In conventional CGT and AGT radiators, hundreds of tubes are installed between the headers, and each tube requires a grommet for each header. Consequently, a radiator having 760 tubes will require 1520 grommets that must each be installed in a corresponding opening. With the high number of components to be assembled, the manufacturing time can be increased substantially where systematic problems exist in installing the previously known grommets in the header plates. In view of this, a need exists for an improved grommet design for radiator assemblies providing more reliable positioning of the grommets with respect to the header plate openings in which they will be inserted to reduce the manufacturing time required for the radiator assembly, and reducing the force necessary to install the grommets within the header plate openings.
In one aspect of the present disclosure, a grommet for insertion into an opening of a header plate of a radiator is disclosed. The grommet may include a generally cylindrical body having a top surface, a bottom surface, and a cylindrical outer surface having a body outer diameter, an annular shoulder proximate the top surface of the body and extending outwardly beyond the outer surface of the body and having a shoulder outer diameter that is greater than the body outer diameter, and an annular bead proximate the bottom surface of the body and extending outwardly beyond the outer surface of the body and having a bead outer diameter that is greater than the body outer diameter. The annular bead comprises a tapered bottom portion having a decreasing outer diameter as the tapered bottom portion extends downwardly toward the bottom surface of the body, with the tapered bottom portion terminating with a bottom outer diameter that is less than the body outer diameter.
In another aspect of the present disclosure, a grommet for insertion into an opening of a header plate of a radiator is disclosed. The grommet may include a generally cylindrical body having a top surface, a bottom surface, a cylindrical outer surface having a body outer diameter, and an inner surface defining a cylindrical bore extending from the top surface of the body to the bottom surface of the body. The grommet may also include an annular shoulder proximate the top surface of the body and extending outwardly beyond the outer surface of the body and having a shoulder outer diameter that is greater than the body outer diameter, and an annular bead proximate the bottom surface of the body and extending outwardly beyond the outer surface of the body and having a bead outer diameter that is greater than the body outer diameter. The annular bead may include a curved top portion and a tapered bottom portion having a decreasing outer diameter as the tapered bottom portion extends from the curved top portion downwardly toward the bottom surface of the body, with the tapered bottom portion terminating with a bottom outer diameter that is less than the body outer diameter. A cylindrical body bottom portion of the grommet may extend from the tapered bottom portion of the annular bead to the bottom surface of the body. The body bottom portion may have a bottom portion outer diameter equal to the bottom outer diameter of the tapered bottom portion.
Additional aspects are defined by the claims of this patent.
Although the following text sets forth a detailed description of numerous different embodiments of the present disclosure, it should be understood that the legal scope of protection is defined by the words of the claims set forth at the end of this patent. The detailed description is to be construed as exemplary only and does not describe every possible embodiment since describing every possible embodiment would be impractical, if not impossible. Numerous alternative embodiments could be implemented, using either current technology or technology developed after the filing date of this patent, which would still fall within the scope of the claims defining the scope of protection.
It should also be understood that, unless a term is expressly defined in this patent using the sentence “As used herein, the term ‘______’ is hereby defined to mean . . . ” or a similar sentence, there is no intent to limit the meaning of that term, either expressly or by implication, beyond its plain or ordinary meaning, and such term should not be interpreted to be limited in scope based on any statement made in any section of this patent (other than the language of the claims). To the extent that any term recited in the claims at the end of this patent is referred to in this patent in a manner consistent with a single meaning, that is done for sake of clarity only so as to not confuse the reader, and it is not intended that such claim term be limited, by implication or otherwise, to that single meaning. Finally, unless a claim element is defined by reciting the word “means” and a function without the recital of any structure, it is not intended that the scope of any claim element be interpreted based on the application of 35 U.S.C. §112(f).
The grommet 30 and the opening 42 are dimensioned so that the grommet 30 may be press fit into the opening 42 of the header plate 26, and retained in the opening 42 after the being inserted there through.
At the opposite end of the body 32 from the annular shoulder 34, an annular detent or bead 44 extends outwardly from the body 32 to provide an additional structure for engaging the header plate 26 to retain the grommet 30 within the opening 42. The annular bead 44 extends outwardly to a maximum extent where the annular bead 44 has a bead outer diameter OD3 that is greater than the body outer diameter OD2. The annular bead 44 includes a rounded or curved top portion 46 that transitions to a tapered bottom portion 48. The curved top portion 46 may have radius of curvature and an outer surface having a substantially circular arc. However, the outer surface of the curved top portion 46 may have a non-circular arc with an alternative type of non-circular curvature, such as elliptical, ovoid and the like. The arc of the curved top portion 46 extends downwardly past the location of the maximum bead outer diameter OD3 and turns back inwardly toward the bore 36 to a point at which the curved top portion 46 transitions to the tapered bottom portion 48. The tapered bottom portion 48 may have an outer surface having a frusto-conical shape that tapers from a maximum outer diameter at the point of transition from the curved top portion 46 to a minimum bottom outer diameter OD4 as the tapered bottom portion 48 approaches a bottom surface 50 of the grommet 30.
In the illustrated embodiment, the tapered bottom portion 48 terminates at a cylindrical bottom portion 52 extending between the tapered bottom portion 48 and the bottom surface 50 of the grommet 30. As shown, the cylindrical bottom portion 52 has a constant outer diameter that is equal to the bottom outer diameter OD4 of the tapered bottom portion 48. The bottom outer diameter OD4 is smaller than the body outer diameter OD2 and is also smaller than the opening inner diameter ID2 of the header plate 26. Dimensioned in this way, the bottom portion 52 may be inserted into the opening 42 of the header plate 26 with minimal engagement with the inner surface defining the opening 42 to facilitate installation of the grommet 30 within the opening 42 as will be discussed further below. In alternative embodiments, the bottom portion 52 may taper inwardly as the bottom portion 52 extends toward the bottom surface 50 but at a shallower angle than the tapered bottom portion 48 of the annular bead 44, or the bottom portion 52 may taper outwardly and terminate at the bottom surface 50 with an outer diameter that is greater than the bottom outer diameter OD4. In each alternative, however, the outer diameter at the bottom surface 50 may be smaller than the opening inner diameter ID2, or at most be approximately equal to the opening inner diameter ID2 so that minimal force is required to insert the bottom portion 52 of the grommet 30 into the opening 42.
The lower portion of the grommet 30 of the present embodiment is shown in greater detail in
The process for installing the tube-and-fin assemblies 10 and the grommets 30 in the header plates 26 of the coolant manifolds of the radiator may be performed manually or may be automated, but either assembly process may be improved by the configuration of the bullet nose grommets 30 in accordance with the present disclosure.
The bottom portion 52 is inserted into the opening 42 until the tapered bottom portion 48 of the annular bead 44 engages an upper edge of the opening 42 as shown in
Once the grommet 30 is in the position shown in
After the grommet 30 is installed within the opening 42, the bottom end 24 of the tube 12 is inserted into the bore 36 of the grommet 30 to complete the installation of the tube-and-fin assembly 10 in the opening 42 of the header plate 26. The bottom end 24 of the tube 12 is inserted into the bore 36 of the grommet 30 at the top surface 35. The outer diameter of the bottom end 24 may be greater than the bore inner diameter ID1 so that a seal may be formed between the outer surface of the bottom end 24 of the tube 12 and the inner surface of the bore 36. As the bottom end 24 slides downward into the bore 36, the bead 40 of the bottom end 24 comes into contact with the top surface 35 of the grommet 30. As the bottom end 24 is pressed further down into the bore 36, the bead 40 causes the portion of the bore 36 at the annular shoulder 34 to deflect outwardly to allow the bead 40 to enter the bore 36. Eventually, the bead 40 is received into the annular groove 38 of the grommet 30 and the portion of the bore 36 above the annular groove 38 collapses around the corresponding portion of the bottom end 24 to engage the bead 40 and retain the bottom end 24 of the tube 12 within the bore 36 as shown in
The bullet nose grommet 30 as illustrated and described herein provides more reliable positioning of the grommet 30 within the opening 42 of the header plate 26 during assembly of the tube 12 and header plate 26. Proper alignment of the grommet 30 provided by the tapered bottom portion 48 of the annular bead 44 and the cylindrical bottom portion 52 of the body 32 allows the grommet 30 to be press fit into the opening 42 of the header plate 26 without requiring the additional force that is necessary to press a misaligned grommet into the opening 42. The grommet 30 is less likely to become dislodged or fall over, thereby reducing the additional assembly time and effort required with previously-known grommets to reposition the grommets after falling over. Ease of installation of the tube-and-fin assemblies 10 provided by the bullet nose grommet 30 can result in a significant savings in assembly time and cost for CGT, AGT and other types of radiators where hundreds or thousands of tube-and-fin assembly 10 and grommet 30 combinations must be installed in a single radiator.
While the preceding text sets forth a detailed description of numerous different embodiments, it should be understood that the legal scope of protection is defined by the words of the claims set forth at the end of this patent. The detailed description is to be construed as exemplary only and does not describe every possible embodiment since describing every possible embodiment would be impractical, if not impossible. Numerous alternative embodiments could be implemented, using either current technology or technology developed after the filing date of this patent, which would still fall within the scope of the claims defining the scope of protection.