Unmanned aerial vehicle propeller gasket and unmanned aerial vehicle propeller base
By adopting snap-on connections and high wear-resistant materials, the existing gaskets are easily loose and not wear-resistant, achieving higher wear resistance and stability, avoiding the problem of stuck during high-speed operation.
Patent Information
- Application Number
- CN202421873528.5
- Authority / Receiving Office
- CN · China
- Patent Type
- Utility models(China)
- Current Assignee / Owner
- Filing Date
- 2024-08-05
- Publication Date
- 2025-04-25
- Estimated Expiration
- 2034-08-05
AI Technical Summary
The materials of existing drone propeller spacers are easy to loosen and not wear-resistant, and they tend to turn black when running at high speed, causing the blade to get stuck.
The upper and lower covers with snap-on connections are used, and the pad core is clamped. Teflon and fibrous Teflon materials are used to ensure that the gasket is not easy to displace and wear-resistant during high-speed operation.
It improves the wear resistance and stability of the propeller spacer, avoids the problem of blade stuck due to the blackening of the spacer during high-speed operation, and is more environmentally friendly.
Smart Images

Figure CN222793840U_ABST
Abstract
Description
Technical Field
[0001] The utility model relates to the technical field of unmanned aerial vehicles, and in particular to a propeller gasket for an unmanned aerial vehicle and a propeller base for an unmanned aerial vehicle. Background Art
[0002] The rotorcraft comprises a fuselage, an arm, a driving device and a propeller assembly fixed to the driving device, wherein the driving device drives the propeller assembly to provide lift for the aircraft to fly. In the prior art, the propeller assembly is a foldable propeller assembly for easy storage of the rotorcraft.
[0003] When installing the propeller assembly, it is usually necessary to use gaskets to reduce vibration and prevent wear. The original blade gaskets currently used are made of 3M adhesive, which is easy to loosen and shift, and are not wear-resistant. When the blades are running at high speed, the inside of the gaskets tends to turn black, causing the blades to get stuck. Utility Model Content
[0004] In order to make up for the deficiencies in the prior art, the utility model provides a propeller gasket for a drone, which has the advantages of being wear-resistant, not easy to shift, not turning black when running at high speed, and being green and environmentally friendly.
[0005] In order to achieve the above purpose, the technical solution adopted by the utility model is as follows:
[0006] A propeller gasket for a drone comprises an upper cover and a lower cover connected in a snap-on manner, a gasket core is sandwiched between the upper cover and the lower cover, and a through hole for connecting a propeller base is provided as a whole after the upper cover, the gasket core and the lower cover are connected.
[0007] Furthermore, the bottom surface of the upper cover is provided with a plurality of connecting columns, the top surface of the lower cover is provided with a plurality of embedded hole columns corresponding to the connecting columns, the embedded hole columns are provided with countersunk holes, the countersunk holes are interference fit with the connecting columns, and the cushion core is provided with through holes for the embedded hole columns to pass through.
[0008] Furthermore, the upper cover and the lower cover are both made of Teflon, and the cushion core is made of fiber-reinforced Teflon.
[0009] The utility model also provides a UAV propeller base, comprising the UAV propeller gasket.
[0010] Furthermore, the UAV propeller base also includes a base, on which a connecting shaft is provided, and the connecting shaft is sequentially sleeved with the UAV propeller gasket, the blade, the UAV propeller gasket, and the propeller clamp from bottom to top.
[0011] Compared with the prior art, the utility model has the following beneficial technical effects:
[0012] Compared with the existing gasket, the utility model has higher wear resistance, is not easy to shift during use, does not contain glue, is more environmentally friendly, and the gasket will not turn black inside when running at high speed, thus avoiding the blade from getting stuck. BRIEF DESCRIPTION OF THE DRAWINGS
[0013] Figure 1 The utility model is an exploded view of a propeller gasket of a UAV.
[0014] Figure 2 The utility model is a structural diagram of an upper cover of a propeller gasket of a drone.
[0015] Figure 3 The utility model is a structural diagram of a propeller base of an unmanned aerial vehicle.
[0016] Among them: 100, UAV propeller gasket; 1, upper cover; 11, connecting column; 2, gasket core; 21, through hole; 3, lower cover; 31, embedded hole column; 4, through hole; 31, embedded hole column; 200, base; 300, connecting shaft; 400, blade; 500, propeller clamp. DETAILED DESCRIPTION
[0017] Many specific details are described in the following description to facilitate a full understanding of the present invention. However, the present invention can be implemented in many other ways different from the description, and those skilled in the art can make similar generalizations without violating the connotation of the present invention. Therefore, the present invention is not limited to the specific embodiments disclosed below.
[0018] Example 1
[0019] like Figure 1 , 2 As shown, a drone propeller gasket 100 includes an upper cover 1, a gasket core 2 and a lower cover 3. The bottom surface of the upper cover 1 is provided with a plurality of connecting columns 11, and the top surface of the lower cover 3 is provided with a plurality of embedded hole columns 31 corresponding to the connecting columns 11. The embedded hole columns 31 are provided with countersunk holes, and the countersunk holes are interference fit with the connecting columns 11, so as to realize the snap-on connection between the upper cover 1 and the lower cover 3. The gasket core 2 is sandwiched between the upper cover 1 and the lower cover 3, and the gasket core 2 is provided with a through hole 21 for the embedded hole columns 31 to pass through. The upper cover 1, the gasket core 2 and the lower cover 3 are connected as a whole and are provided with a through hole 4 for connecting the propeller base. Preferably, the upper cover 1 and the lower cover 3 are made of Teflon, and the gasket core 2 is made of fiber-reinforced Teflon, which is more wear-resistant than the existing gaskets.
[0020] like Figure 3 As shown, a UAV propeller base includes a base 200, on which a connecting shaft 300 is provided, and the connecting shaft 300 is sequentially sleeved with a UAV propeller gasket 100, a blade 400, a UAV propeller gasket 100, and a propeller clamp 500 from bottom to top.
[0021] The above are only preferred embodiments of the present invention and are not intended to limit the present invention. Although the present invention has been described in detail with reference to the embodiments, those skilled in the art can still modify the technical solutions described in the aforementioned embodiments or make equivalent substitutions for some of the technical features therein. However, any modifications, equivalent substitutions, improvements, etc. made within the spirit and principles of the present invention should be included in the protection scope of the present invention.
Claims
1. A UAV propeller gasket, characterized in that: It comprises an upper cover and a lower cover connected in a snap-fit manner, a cushion core is sandwiched between the upper cover and the lower cover, and a through hole for connecting a propeller seat is provided as a whole after the upper cover, the cushion core and the lower cover are connected.
2. The UAV propeller gasket according to claim 1, characterized in that: The bottom surface of the upper cover is provided with a plurality of connecting columns, the top surface of the lower cover is provided with a plurality of embedded hole columns corresponding to the connecting columns, the embedded hole columns are provided with countersunk holes, the countersunk holes are interference fit with the connecting columns, and the cushion core is provided with through holes for the embedded hole columns to pass through.
3. The UAV propeller gasket according to claim 2, characterized in that: The upper cover and the lower cover are both made of Teflon, and the cushion core is made of fiber-reinforced Teflon.
4. A propeller base for an unmanned aerial vehicle, characterized in that: It comprises a drone propeller gasket as described in any one of claims 1 to 3.
5. The propeller base of the unmanned aerial vehicle according to claim 4, characterized in that: It also includes a machine base, on which a connecting shaft is provided, and the connecting shaft is sleeved with the UAV propeller gasket, the blade, the UAV propeller gasket, and the propeller clamp in sequence from bottom to top.