The invention relates to fan shroud structures and more particularly to a fan shroud structure that that reduces resonance, improves stiffness and manufacturability of the shroud.
Currently, fan shrouds that are in a box shape are excitable (by resonance) in the operating range of the fan motor or other periodic signals in the machine the fan is placed in, such as a vehicle. In addition, due to the box-like structure of typical shrouds, there is a need for substantial structural re-enforcement to minimize warping and distortion. However, the use of such significant re-enforcement can increase the manufacturability (e.g. moldability) of the shroud and cost of materials, while adversely affecting airflow properties.
Thus, there is a need to provide an improved fan shroud structure that reduces resonance, and improves stiffness and manufacturability.
An object of the present invention is to fulfill the need referred to above. In accordance with the principles of the present invention, this objective is obtained by a providing a fan shroud structure constructed and arranged to carry a fan. The fan shroud structure includes a body having a periphery, a main surface, and an annular rim defining a generally central opening. The opening is sized to accommodate blades of a fan. Fan mounting structure is coupled with the body and is disposed generally adjacent to the central opening. The fan mounting structure is constructed and arranged to support a motor of a fan. The body includes a plurality of surfaces features constructed and arranged to affect resonance of the shroud structure with each feature having a surface that is discontinuous with the main surface of the body. Each surface feature also extends from the annular rim to the periphery of the body.
Other objects, features and characteristics of the present invention, as well as the methods of operation and the functions of the related elements of the structure, the combination of parts and economics of manufacture will become more apparent upon consideration of the following detailed description and appended claims with reference to the accompanying drawings, all of which form a part of this specification.
The invention will be better understood from the following detailed description of the preferred embodiments thereof, taken in conjunction with the accompanying drawings, wherein like reference numerals refer to like parts, in which:
With reference to
The shroud structure 10 is preferably part of a fan module that is configured to be mounted between a condenser and a radiator. The shroud structure 10 includes a shroud body 12 having a pair of opposing first sides 14 and a pair opposing second sides 16. The first sides 14 are joined with the second sides 16 at corners 18 so as to form a box-like configuration having a periphery. The shroud body 12 has a front end 20 (
With reference to
Although eight surface features 34 are shown and each feature 34 is shown to be of stepped configuration, the number and configuration of the surface features can vary. For example,
The use of the features 34, 34′ to define discontinuous surfaces in the body 12 not only shifts, reduces, or eliminates resonance in the shroud structure 10 or 10′, but the surface features along with ribs 42 also improve the structural properties of the shroud structure. Thus, a rib 42 is coupled, at the rim 26, between a surface feature 34 and an associated arm 30. Thus, the shroud structure, with features 34, 34′ and associated ribs 42, provides a higher level of stiffness as compared to plain ribbing reinforcement of similar plastic or composite structures.
Conventionally, to ensure sufficient stiffness, reinforcement ribs extend (or a second set added) radially outward toward the perimeter of the shroud structure. However, such additional rib reinforcement requires additional material (at additional cost), requires a more complex molding process, and could adversely affect airflow parameters. Since the features 34, 34′ extend to the perimeter (e.g., sides 14, 16) of the body 12, they provide geometrical stability so that warping and distortion is reduced or eliminated. Thus, due to the features 36, 36′, the above mentioned rib reinforcement is not necessary and a higher frequency shroud structure is provided (e.g., to 40 hertz or higher) of low mass, thermoplastic or composite material. In addition, manufacturability is simplified since molds do not need to include the conventional, complicated rib reinforcement structure.
The foregoing preferred embodiments have been shown and described for the purposes of illustrating the structural and functional principles of the present invention, as well as illustrating the methods of employing the preferred embodiments and are subject to change without departing from such principles. Therefore, this invention includes all modifications encompassed within the spirit of the following claims.
This application is based on U.S. Provisional Application No. 60/496,979, filed on Aug. 21, 2003, and claims the benefit thereof for priority purposes.
Number | Name | Date | Kind |
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5489186 | Yapp et al. | Feb 1996 | A |
6106228 | Bartlett | Aug 2000 | A |
6123051 | Kubina et al. | Sep 2000 | A |
6223548 | Calvert | May 2001 | B1 |
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6474943 | Kataoka et al. | Nov 2002 | B1 |
6554230 | Horski | Apr 2003 | B1 |
Number | Date | Country | |
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20050042088 A1 | Feb 2005 | US |
Number | Date | Country | |
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60496979 | Aug 2003 | US |