The present invention relates to a fan and the rotor structure thereof.
Generally, in a conventional fan, the shaft and the case of the rotor structure are engaged by interference fit. In a large fan with significant size and weight, however, the shaft and the case may separate in operation due to the weight of the rotor structure. Typically, a rivet joint is used for large fans to engage the shaft and the case. With a rivet joint, the contact area of the shaft and the case increases to support the increased weight of the rotor structure.
In the conventional rotor structure 100, however, the copper sheath 106 is riveted to the case 102 by compression, so that the shock resistance of the rotor structure is limited. When the weight of the rotor structure increases, it is possible that the rivet joint 110 will fracture or separate due to the weight thereof, and the shaft 108 and the case 102 may separate.
Further, the copper sheath 106 is riveted to the case 102 by compression, so a portion of the s electrocoating layer on the case 102 is scraped by the copper sheath 106. Thus, due to degradation of the electrocoating layer, the case 102 and the copper sheath 106 are exposed and may rust. In addition, a gap exists between the case 102 and the copper sheath 106 due to the rivet joint 110. Further, the shaft 108 is disposed in the copper sheath 106 by interference fit, such that a portion of the shaft 108 is exposed and may rust. In either case, the rotor structure and other elements in the fan may be damaged.
Accordingly, the invention provides a rotor structure to increase anti-rusted property thereof and to extend the fan life. The present invention also provides a rotor structure having better pressurization. A fan with the rotor structure with extended life can be obtained.
A rotor structure is disclosed. The rotor structure comprises a case, an upper linking structure, a lower linking structure, and a shaft. The case comprises an opening at the axle center. The upper linking structure comprises a fixing portion and a threaded portion. The minimum radius of the fixing portion is longer than the radius of the opening. The threaded portion is disposed in the opening. The lower linking structure has a thread corresponding to the threaded portion. The upper linking structure and the lower linking structure are screwed together to secure the case therebetween. The shaft is fixed in the upper linking structure or the lower linking structure.
In a further embodiment, a rotor structure is disclosed, which comprises a securing structure and a shaft. The securing structure is screwed or wedged in a case, and the shaft is fixed to the securing structure. The securing structure comprises an upper linking structure and a lower linking structure. The upper linking structure comprises a fixing portion and a threaded portion. The minimum radius of the fixing portion is longer than the maximum radius of the threaded portion. The lower linking structure comprises a thread corresponding to the threaded portion. The upper linking structure and the lower linking structure is screwed together to secure the case therebetween. The rotor structure can be applied to a fan.
In the rotor structure, the case and the shaft can be combined by at least one securing structure. Thus, combination and the airtight connection between the case, the shaft and the securing structure are increased. Additionally, the manufacturing process of the rotor structure is simplified, and the manufacturing period of the rotor structure is decreased.
Further, the rotor structure of the present invention comprises waterproof structure, so the rotor structure can prevent the inner components of the fan from rust.
An sealing can be formed between the securing structure and the case to provide the airtight connection for preventing.
Further, an electrocoating coating process to form an electrocoating layer can be performed after assembly of the rotor structure so that the electrocoating layer is not damaged. The electrocoating layer can cover the clearance in the connection area and to prevent the inner component of the fan from rust.
A detailed description is given in the following embodiments with reference to the accompanying drawings.
The present invention can be more fully understood by reading the subsequent detailed description and examples with references made to the accompanying drawings, wherein:
The rotor structure 200 comprises a case 202, a securing structure 216, and a shaft 204 fixed to the case 202 by the securing structure 216.
The case 202 is the body of the rotor structure 200 and has a tubular shape. An opening 226 is disposed in an axle center on the bottom of the case 202 to enclose the securing structure 216. Specifically, a cross-section of the tubular shape can be circular, polygonal, or other similar shapes, and the opening 226 can be circular, polygonal, regular-patterned or irregular-patterned. The case 202 can be fabricated by punching or integral forming, and the material of the case 202 is metal, plastic or alloy.
When the rotor structure 200 is applied to a fan or other similar device, a fan blade 212 can be disposed surrounding periphery of the case 202. The fan blade 212 can be an axial-flow fan blade, a centrifugal fan blade, a flat fan blade, or a blower fan blade. The material of the fan blade 212 is metal, plastic or alloy.
The securing structure 216 can comprise a single linking structure 206. The linking structure 206 comprises a threaded portion 224 and a fixing portion 222. A maximum radius of the threaded portion 224 is shorter than a minimum radius of the fixing portion 222. Further, the maximum radius of the threaded portion 224 is slightly shorter than or equal to a radius of the opening 226, and the minimum radius of the fixing portion 222 is longer than the radius of the opening 226. In this case, when threads of the opening 226 correspond to the threaded portion 224, the threaded portion 224 is screwed into the opening 226 to fix to the case 202. It is preferable that a screwing direction between the threaded portion 224 and the opening 226 is opposite to a rotating direction of the rotor structure 200. Thus, the securing structure 216 does not loose when the rotor structure 200 is in operation.
In
Further, the threaded portion 224 of the linking structure 206 can be inner threads, and the linking structure 208 has an outer threads corresponding to the inner threads. The shaft 204 is connected to the linking structure 208 by embedding, dying or engaging. Specifically, the linking structures 206 and 208 can be a set of screw and nut.
A hole 220 is disposed in the axle center of the linking structure 206 for fixing the shaft 204. The hole 220 can be either a through hole as shown in
A buffer structure 214 is provided in the rotor structure 200, connected to the securing structure 216. Specifically, the opening of the linking structure 208 comprises two ends, with a radius of the end near the fixing portion 222 shorter than a radius of the end away from the fixing portion 222. Thus, a space is formed at the bottom of the linking structure 208 for securing the buffer structure 214. The outer periphery of the linking structures 206, 208 or 216 can be a circle, polygon, polyhedron, ellipse, or a sliced circle. The buffer structure 214 connects the housing to the stator structure or the shaft protection structure seamlessly. The buffer structure 214 can be a spring or an elastic member.
An sealing 210 can be disposed between the linking structure 206 and the case 202 by integral forming or direct forming. The sealing 210 can be an oil ring, a silicon spacer, an elastic pad, a seal, or a rubber sealing. When the sealing 210 is directly formed between the linking structure 206 and the case 202, an indentation 212a is formed on the linking structure 206 and the case 202 to fill in the sealing 210. The indentation 212a can be formed on the linking structure 206 or the case 202 or both. Further, the sealing 210 can be circular, ring-shaped, star-shaped, polygonal, or an enclosed shape. It is applicable to form a plurality of individual sealings to secure the airtight connection. The sealings are disposed separately or crossing with each other.
In
In assembly of the rotor structure 200, an electrocoating layer is coated on the rotor structure 200 to prevent from rust. Since the electrocoating layer is applied after assembly of the rotor structure 200, there is no need to perform a pre-coating process for the individual elements of the rotor structure. Thus, assembly of the rotor structure is simplified, and manufacturing time and cost are reduced.
In the rotor structure, the case and the shaft can be combined by at least one linking structure. Thus, combination and the airtight connection between the case, the shaft and the linking structure are increased. Additionally, the manufacturing process of the rotor structure is simplified, and the manufacturing period of the rotor structure is decreased.
Further, the rotor structure of the present invention comprises waterproof structure, so the rotor structure can prevent the inner components of the fan from rust.
A sealing can be formed between the linking structure and the case to provide the airtight connection for preventing.
Further, an electrocoating coating process to form an electrocoating layer can be performed after assembly of the rotor structure so that the electrocoating layer is not damaged. The electrocoating layer can cover the clearance in the connection area and to prevent the inner component of the fan from rust.
As well, the rotor structure of the invention can be employed in a fan or a motor. Because the shaft is screwed to the housing, the lifetime of the fan or the motor can be extended by renewing the shaft.
While the invention has been described by way of example and in terms of preferred embodiment, it is to be understood that the invention is not limited thereto. To the contrary, it is intended to cover various modifications and similar arrangements (as would be apparent to those skilled in the art). Therefore, the scope of the appended claims should be accorded the broadest interpretation so as to encompass all such modifications and similar arrangements.
Number | Date | Country | Kind |
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92132496 | Nov 2003 | TW | national |