Guard and blade disassembly structure
The guard and feather decomposition structure simplifies fan cleaning by allowing easy disassembly and reassembly through a pedestal-mounted motor and interlocking gears, addressing the complexity of conventional fan maintenance.
Patent Information
- Application Number
- JP2024003230U
- Authority / Receiving Office
- JP · JP
- Patent Type
- Utility models
- Current Assignee / Owner
- Filing Date
- 2024-09-27
- Publication Date
- 2025-01-28
- Estimated Expiration
- 2034-09-27
AI Technical Summary
Conventional fans are difficult to clean due to the complexity in disassembling the guard and feather components, making maintenance and cleaning cumbersome.
A guard and feather decomposition structure that allows for easy disassembly by fixing the operating motor on a pedestal, attaching feathers to the motor axis, and utilizing interlocking gears and removable components like the front and rear guards, lock nuts, and penetration holes for seamless detachment.
Facilitates quick and convenient cleaning by enabling easy removal and reassembly of fan components, enhancing user convenience and efficiency.
Smart Images

Figure 0003249975000001_ABST
Abstract
Description
[Technical field]
[0001] This invention relates to the technical field of electric fans, and relates to a guard and blade disassembly structure that allows the blade section, consisting of the guard and the blades, to be completely disassembled from the body of the fan. [Background technology]
[0002] Electric fans, also known as fans, are electrical appliances that use a motor to rotate blades to promote air circulation, mainly used for cooling and ventilation. They are widely used in homes, classrooms, offices, shops, hospitals, hotels and other places. However, after a period of use, dust accumulates on the guards and blades of conventional fans, making it necessary to remove the front and rear guards to clean them. However, because the rear guard is difficult to remove, cleaning is difficult and inconvenient. Summary of the Invention [Problem to be solved by the invention]
[0003] The object of the present invention is to solve the problems raised in the background art above, and to provide a guard / blade disassembly structure that is easy to clean. [Means for solving the problem]
[0004] This invention provides the following technical solution. It is a guard-blade disassembly structure for disassembling the guard and blades from the main body, and is provided with a base to which a support frame is fixedly attached at its tip, a motor body is movably attached to the support frame, blades are attached to the shaft of the motor shaft on the outside of the body, and a front guard and a rear guard are attached to surround the blades. The motor is fixedly attached to the base, a driving gear is fixedly attached to the output shaft side of the motor, and a driven gear is fixedly attached to the rear side of the body, and the driving gear and the driven gear mesh and interlock. The driven gear is oval-shaped and follows an arc-shaped trajectory.
[0005] According to a preferred embodiment, a blade is movably attached to the shaft of the operating motor shaft of the aircraft, a blade head spinner is movably attached to one end of the blade, a lock nut is screwed onto the aircraft, and the lock nut and the blade head spinner are connected at both ends across the blade.
[0006] Furthermore, according to one preferred embodiment, a connecting through hole that fits the shaft of the actuation motor shaft is drilled inside the rear guard. Effect of the Invention
[0007] Compared with the prior art, the present invention discloses a disassembled structure of the guard and the blade, which has the following beneficial effects: 1. The guard and blade disassembly structure disclosed in this invention can be removed by removing the fixing screw of the front guard and turning it to a certain angle. The blade can be removed by turning and removing the spinner of the blade head. The rear guard can be removed by turning and removing the lock nut. After removal, it is very convenient for users to clean. After cleaning, the rear guard can be installed on the aircraft via the lock nut, the blade via the spinner of the blade head, and the front guard via the fixing screw, which is convenient and quick. 2. The guard and blade disassembly structure disclosed in this invention allows the entire fan to swing up and down through the cooperation of the drive gear and driven gear. [Brief description of the drawings]
[0008] The accompanying drawings are structural diagrams used for further understanding of the present invention, which constitute a part of the specification and are used to explain the present invention together with the embodiments of the present invention, but are not intended to limit the present invention. [Figure 1] FIG. 1 is a schematic diagram of the overall three-dimensional assembly of the guard and blade disassembly structure according to the present invention. [Diagram 2] FIG. 2 is a schematic diagram of the assembly of the front and rear guards in the guard / blade disassembly structure of the present invention. [Diagram 3] FIG. 3 is a schematic diagram of the blade assembly of the guard / blade disassembly structure of the present invention. [Figure 4] FIG. 4 is a cross-sectional view of the main body of the guard / blade disassembly structure according to the present invention. DETAILED DESCRIPTION OF THE PREFERRED EMBODIMENTS
[0009] The following will clearly and completely describe the technical solutions in the embodiments of the present invention in conjunction with the drawings of the embodiments of the present invention. Obviously, the described embodiments are not all the embodiments, but only some of the embodiments of the present invention. Based on the embodiments of the present invention, any other embodiments obtained by a person skilled in the art without creative ingenuity are also within the scope of the claims of the present invention.
[0010] Embodiment 1 to 4 show the guard and blade disassembly structure, which includes a base 9 to which a support frame is fixedly attached at its tip, a motor body 6 movably attached to the support frame, a motor shaft having blades 3 attached to the outside of the motor shaft, and a front guard 1 and a rear guard 5 surrounding the blades. The motor is fixedly attached to the base 9, a drive gear 8 is fixedly attached to the output shaft side of the motor, and a driven gear 7 is fixedly attached to the rear side of the motor body 6, with the drive gear 8 and driven gear 7 meshing together to interlock. The driven gear 7 is oval and follows an arc-shaped trajectory.
[0011] The front guard 1 is connected to the rear guard 5 by a fixing screw, so that the front guard can be easily removed from the rear guard 5.
[0012] In this embodiment, the blade 3 is movably attached to the shaft of the operating motor shaft of the airframe 6, the blade head spinner 2 is movably attached to one end of the blade 3, and a lock nut 4 is screwed onto the airframe 6, and the lock nut 4 and the blade head spinner 2 are connected at both ends with the blade 3 in between.
[0013] The lock nut 4 and the rear guard 5 are connected to each other.
[0014] In this embodiment, a connecting through hole that fits the shaft of the actuation motor shaft is drilled inside the rear guard 5 . When the connecting through hole is provided, the rear guard 5 is not interfered with by the shaft of the actuation motor shaft when it is removed from the machine body 6, and the removal of the rear guard 5 becomes easier.
[0015] Working principle of this embodiment: When in use, the front guard 1 can be removed from the rear guard 5 simply by unscrewing the fixing screw of the front guard 1 and turning it to a certain angle. The blade 3 can be removed from the body 6 by turning the spinner 2 of the blade head. The rear guard 5 can be removed from the machine body 6 by turning the lock nut 4. The drive gear 8 is rotated by the operating motor, and when the drive gear 8 rotates, the machine body 6 is driven by the driven gear 7 and rotates around the tip of the support frame. [Explanation of symbols]
[0016] 1. Front guard, 2. Spinner, 3. Blade, 4. Lock nut, 5. Rear guard, 6. Airframe, 7. Driven gear, 8. Driving gear, 9. Base
Claims
1. A base 9 is provided at the tip of which a support frame is fixedly attached, A machine body 6 is movably attached to the tip of the support frame, On the outside of the fuselage 6, a blade 3 is attached to the shaft of an operating motor shaft, The front guard 1 and rear guard 5 are attached around the blade. An operating motor is fixedly attached to the base 9, A drive gear 8 is fixedly attached to the output shaft side of the actuation motor, A driven gear 7 is fixedly attached to the back side of the machine body 6, The driving gear 8 and the driven gear 7 mesh with each other and move in an arc-shaped trajectory. The guard and blade disassembly structure features:
2. The blade 3 is movably attached to the shaft of the operating motor shaft of the machine body 6, A spinner 2 of a blade head is movably attached to one end of the blade 3, A lock nut 4 is screwed onto the machine body 6, The lock nut 4 and the spinner 2 of the blade head are connected at both ends with the blade 3 in between. The guard / blade disassembly structure according to claim 1.
3. Inside the rear guard 5, A connecting through hole that fits the shaft of the operating motor shaft must be drilled. The guard / blade disassembly structure according to claim 1.