Electric empennage driving system, electric empennage system and vehicle
By designing the transmission mechanism and elastic components connected to the coupling in the electric tail drive system to apply positive pressure, the problem of insufficient grip during high speed driving is solved, the system accuracy and self-locking ability are improved, and the vehicle handling is enhanced.
Patent Information
- Application Number
- CN202421923797.8
- Authority / Receiving Office
- CN · China
- Patent Type
- Utility models(China)
- Current Assignee / Owner
- Filing Date
- 2024-08-09
- Publication Date
- 2025-05-02
- Estimated Expiration
- 2034-08-09
AI Technical Summary
The existing electric tail drive system has accuracy errors when used, resulting in insufficient grip when driving at high speed, reduced handling, and may even lead to out-of-control accidents.
An electric tail drive system is designed, including a driving device, a first transmission member, a second transmission member, an output shaft and an elastic member. The drive device is connected to the first transmission member through a coupling, and the second transmission member is driven by the first transmission member, and the second transmission member is driven to the output shaft. The elastic member applies elastic force to the second transmission member to ensure that there is a positive pressure between the second transmission member and the output shaft, reduces side suction, and improves self-locking.
By reducing the side clearance of the transmission mechanism, the accuracy and self-locking of the electric tail drive system are improved, the grip of the vehicle when driving at high speed is enhanced, the handling is improved, and the risk of out-of-control accidents is reduced.
Smart Images
Figure CN222820166U_ABST
Abstract
Description
Technical Field
[0001] The present invention relates to an electric tail wing driving system, an electric tail wing system and a vehicle, belonging to the technical field of vehicle tail wing. Background Art
[0002] With the increasingly widespread application of vehicle lightweight technology, the weight of the entire vehicle is getting lighter and lighter, resulting in insufficient grip when the vehicle is driving at high speed, which reduces the vehicle's handling. In severe cases, it may cause the vehicle to lose control and cause a traffic accident.
[0003] To this end, electric rear wing systems that can automatically adjust their position according to vehicle speed are becoming more and more widely used.
[0004] For example, Chinese utility model patent publication CN214689805U discloses an electric tail wing drive system, in which there is a multi-stage transmission mechanism. Due to factors such as manufacturing and installation errors, there will be gaps in the transmission mechanism, and the electric tail wing drive system will have certain precision errors when in use. Utility Model Content
[0005] In order to solve one of the above technical problems, the present disclosure provides an electric tail wing drive system, an electric tail wing system and a vehicle.
[0006] According to one aspect of the present disclosure, there is provided an electric tail wing drive system, comprising:
[0007] A driving device, the driving device is used to generate a driving force;
[0008] A first transmission component, wherein the driving device is used to drive the first transmission component to rotate;
[0009] A second transmission component, wherein the first transmission component cooperates with the second transmission component, and the first transmission component drives the second transmission component to rotate;
[0010] an output shaft, the second transmission component being in driving connection with the output shaft, and the second transmission component driving the output shaft to rotate; and
[0011] An elastic component is used to apply an elastic force to the second transmission component, and the elastic force causes a positive pressure to exist between the second transmission component and the output shaft.
[0012] According to the electric tail wing drive system of at least one embodiment of the present disclosure, the first transmission component is a first worm gear, and the first transmission component and the drive device have the same rotation axis.
[0013] According to the electric tail wing drive system of at least one embodiment of the present disclosure, the drive device is connected to the first transmission component via a coupling.
[0014] According to the electric tail drive system of at least one embodiment of the present disclosure, the second transmission component includes a first end, wherein a first worm gear is formed on an outer surface of the second transmission component, and the first worm gear is close to the first end of the second transmission component, wherein the first worm gear is connected to the first worm gear.
[0015] According to the electric tail drive system of at least one embodiment of the present disclosure, the second transmission component includes a second end, and the second transmission component includes a second worm, and the second worm is arranged close to the second end of the second transmission component.
[0016] According to the electric tail drive system of at least one embodiment of the present disclosure, the elastic component is disposed close to the second end of the second transmission component, and the force application point of the elastic component to the second transmission component is close to the second end of the second transmission component.
[0017] According to the electric tail wing drive system of at least one embodiment of the present disclosure, a bearing is provided at the second end of the second transmission component, and the elastic component is in contact with the bearing and can apply an elastic force to the bearing.
[0018] According to the electric tail wing drive system of at least one embodiment of the present disclosure, a second worm gear is provided on the output shaft, and the second worm gear cooperates with the second worm gear.
[0019] According to the electric tail wing drive system of at least one embodiment of the present disclosure, the elastic component includes:
[0020] a base having a first end and a second end;
[0021] A first elastic part and a second elastic part, wherein the first elastic part is arranged at the first end of the base, and the second elastic part is located at the second end of the base, and elastic force is applied to the second transmission component through elastic deformation of the first elastic part and the second elastic part.
[0022] According to the electric tail wing drive system of at least one embodiment of the present disclosure, the first elastic portion is the same as the second elastic portion, and both include a first bending portion and a second bending portion, wherein one end of the first bending portion is arranged at one end of the base, one end of the second bending portion is connected to the other end of the first bending portion, and the other end of the second bending portion is arranged close to the base.
[0023] According to at least one embodiment of the electric tail wing drive system of the present disclosure, it also includes a shell and a cover body, wherein the cover body is arranged on the shell, and an accommodating space is formed between the shell and the cover body, and the drive device, the first transmission component, the second transmission component and the elastic component are arranged in the accommodating space.
[0024] According to the electric tail drive system of at least one embodiment of the present disclosure, the shell has a first end face facing the cover body, and the cover body has a second end face facing the shell, wherein a groove is formed on one of the first end face and the second end face, and a protrusion is formed on the other of the first end face and the second end face, and when the shell and the cover body are installed together, at least a portion of the protrusion is located in the groove.
[0025] According to the electric tail wing drive system of at least one embodiment of the present disclosure, a sealing component is disposed in the groove, and the protrusion causes the sealing component to be deformed.
[0026] According to the electric tail wing driving system of at least one embodiment of the present disclosure, the sealing component includes a rubber ring.
[0027] According to the electric tail drive system of at least one embodiment of the present disclosure, a first transmission ratio is provided between the first transmission component and the second transmission component, a second transmission ratio is provided between the second transmission component and the output shaft, and the first transmission ratio is the same as the second transmission ratio.
[0028] According to another aspect of the present disclosure, an electric tail system is provided, which includes the above-mentioned electric tail drive system.
[0029] According to another aspect of the present disclosure, a vehicle is provided, which includes the above-mentioned electric tail wing system. BRIEF DESCRIPTION OF THE DRAWINGS
[0030] The accompanying drawings illustrate exemplary embodiments of the present disclosure and together with the description serve to explain the principles of the present disclosure. These drawings are included to provide a further understanding of the present disclosure and are incorporated in and constitute a part of this specification.
[0031] Figure 1 is a schematic structural diagram of an electric tail wing drive system according to an embodiment of the present disclosure.
[0032] Figure 2 is a transmission principle diagram of an electric tail wing drive system according to one embodiment of the present disclosure.
[0033] Figure 3 is a schematic diagram of an exploded structure of an electric tail wing drive system according to one embodiment of the present disclosure.
[0034] Figure 4 It is a schematic cross-sectional view of a portion of the structure of an electric tail wing drive system according to one embodiment of the present disclosure.
[0035] Figure 5 It is a partial structural schematic diagram of an electric tail wing drive system according to one embodiment of the present disclosure.
[0036] Figure 6 is a schematic structural diagram of an elastic component according to an embodiment of the present disclosure.
[0037] The specific reference numerals in the figure are:
[0038] 100 Shell
[0039] 200 cover
[0040] 300 drive unit
[0041] 301 shock absorbing parts
[0042] 302 coupling
[0043] 400 first transmission component
[0044] 500 Second transmission component
[0045] 600 elastic parts
[0046] 610 base
[0047] 620 first elastic portion
[0048] 621 first bending portion
[0049] 622 second bending portion
[0050] 630 second elastic portion
[0051] 700 output shaft
[0052] 701 second worm gear
[0053] 900 sealing components. DETAILED DESCRIPTION
[0054] The present disclosure is further described in detail below in conjunction with the accompanying drawings and implementations. It is understood that the specific implementations described herein are only used to explain the relevant content, rather than to limit the present disclosure. It should also be noted that, for ease of description, only the parts related to the present disclosure are shown in the accompanying drawings.
[0055] It should be noted that, in the absence of conflict, the embodiments and features of the embodiments in the present disclosure can be combined with each other. The technical solution of the present disclosure will be described in detail below with reference to the accompanying drawings and in combination with the embodiments.
[0056] Unless otherwise specified, the exemplary embodiments / embodiments shown will be understood as providing exemplary features of various details of some ways in which the technical concept of the present disclosure can be implemented in practice. Therefore, unless otherwise specified, the features of the various embodiments / embodiments can be combined, separated, interchanged and / or rearranged without departing from the technical concept of the present disclosure.
[0057] The use of cross-hatching and / or shading in the accompanying drawings is generally used to make the boundaries between adjacent components clear. As such, unless otherwise specified, the presence or absence of cross-hatching or shading does not convey or indicate any preference or requirement for the specific materials, material properties, dimensions, proportions, commonalities between the components shown, and / or any other characteristics, attributes, properties, etc. of the components. In addition, in the accompanying drawings, the sizes and relative sizes of the components may be exaggerated for clarity and / or descriptive purposes. When the exemplary embodiments can be implemented differently, the specific process sequence can be performed in a different order than described. For example, two successively described processes can be performed substantially simultaneously or in an order opposite to the described order. In addition, the same figure numbers represent the same components.
[0058] When a component is referred to as being "on" or "over," "connected to," or "coupled to" another component, the component may be directly on, directly connected to, or directly coupled to the other component, or intervening components may be present. However, when a component is referred to as being "directly on," "directly connected to," or "directly coupled to" another component, there are no intervening components. For this purpose, the term "connected" may refer to a physical connection, an electrical connection, etc., with or without intervening components.
[0059] For descriptive purposes, the present disclosure may use spatially relative terms such as "under," "beneath," "under," "down," "over," "upper," "above," "higher," and "side (e.g., as in "sidewall")," to describe the relationship of one component to another (other) component as shown in the accompanying drawings. The spatially relative terms are intended to encompass different orientations of the device in use, operation, and / or manufacture in addition to the orientation depicted in the accompanying drawings. For example, if the device in the accompanying drawings is turned over, components described as "under" or "beneath" other components or features would subsequently be positioned "over" the other components or features. Thus, the exemplary term "under" can encompass both the "above" and "below" orientations. Furthermore, the device may be otherwise oriented (e.g., rotated 90 degrees or at other orientations), and the spatially relative descriptors used herein should be interpreted accordingly.
[0060] The terms used here are for the purpose of describing specific embodiments, and are not intended to be restrictive. As used here, unless the context clearly indicates otherwise, the singular forms "one (kind, person)" and "said (the)" are also intended to include plural forms. In addition, when the terms "comprise" and / or "include" and their variations are used in this specification, it is explained that there are stated features, integral bodies, steps, operations, parts, assemblies and / or their groups, but it is not excluded that there are or add one or more other features, integral bodies, steps, operations, parts, assemblies and / or their groups. It should also be noted that, as used here, the terms "substantially", "approximately" and other similar terms are used as approximate terms and not as degree terms, so that they are used to explain the inherent deviations of the measured values, calculated values and / or the values provided that will be recognized by those of ordinary skill in the art.
[0061] Figure 1 is a schematic structural diagram of an electric tail wing drive system according to an embodiment of the present disclosure. Figure 2 is a transmission principle diagram of an electric tail wing drive system according to one embodiment of the present disclosure. Figure 3 is a schematic diagram of an exploded structure of an electric tail wing drive system according to one embodiment of the present disclosure.
[0062] like Figure 1 , Figure 2 and Figure 3 As shown, the electric tail wing drive system of the present disclosure may include components such as a housing 100 and a cover 200. In actual use, the cover 200 is disposed on the housing 100, so that the housing 100 and the cover 200 can be fixed together, and then the housing 100 or the cover 200 can be fixed to the vehicle body, so that the electric tail wing drive system of the present disclosure can be fixed to the vehicle body.
[0063] In a specific embodiment, an accommodation space is formed between the housing 100 and the cover 200 , and the driving device 300 , the first transmission component 400 , the second transmission component 500 , and the elastic component 600 are disposed in the accommodation space.
[0064] More specifically, the housing 100 has a first cavity opening upward, and the housing 100 has a first end surface facing the cover 200. In the present disclosure, the first end surface is the peripheral area of the first cavity. On the other hand, the cover 200 has a second cavity opening downward, and the cover 200 has a second end surface facing the housing 100. The second end surface is the peripheral area of the second cavity.
[0065] In the present disclosure, a groove is formed on one of the first end face and the second end face, and a protrusion is formed on the other of the first end face and the second end face. When the shell 100 and the cover body 200 are installed together, at least a portion of the protrusion is located in the groove, thereby forming a sealed connection between the shell 100 and the cover body 200.
[0066] Figure 4 It is a schematic cross-sectional view of a portion of the structure of an electric tail wing drive system according to one embodiment of the present disclosure.
[0067] In a specific embodiment, Figure 4 As shown, the protrusion is formed on the first end surface of the shell 100, and the groove is formed on the second end surface of the cover body 200.
[0068] More preferably, a sealing component 900 is disposed in the groove, and the protrusion causes the sealing component 900 to deform, thereby achieving better sealing performance between the housing 100 and the cover 200. In a specific embodiment, the sealing component 900 can be a component made of a deformable material such as a rubber ring or a silicone ring.
[0069] Refer to Figure 1 and Figure 3 In the present disclosure, the driving device 300 may be a motor, such as a DC motor or other device capable of generating power, thereby, the driving device 300 can generate driving force. In one embodiment, a shock absorbing component 301 may be provided at at least one end of the driving device 300, thereby, the motor is not directly supported by the housing 100 and the cover 200, but is indirectly supported by the housing 100 and the cover 200 through the shock absorbing component 301, and the provision of the shock absorbing component 301 can reduce the vibration transmitted by the motor to the housing 100 and the cover 200, so that the electric tail wing driving system of the present disclosure can have less noise and vibration as a whole.
[0070] The driving device 300 is used to drive the first transmission component 400 to rotate; specifically, the first transmission component 400 is a first worm, and the first transmission component 400 and the driving device 300 have the same rotation axis.
[0071] In the present disclosure, the driving device 300 is connected to the first transmission component 400 via a coupling 302. More preferably, the coupling 302 may be an elastic coupling, so that the vibration outputted by the motor to the first transmission component 400 is reduced by the setting of the elastic coupling, so that the transmission of the electric tail drive system of the present disclosure is more stable.
[0072] In a specific embodiment, one end of the first transmission component 400 is connected to the driving device 300 through a coupling 302, and the other end of the first transmission component 400 can be rotatably supported by the housing 100 and the cover 200 through a bearing.
[0073] The first transmission component 400 cooperates with the second transmission component 500 , and the first transmission component 400 drives the second transmission component 500 to rotate; in the present disclosure, the rotation axis of the second transmission component 500 may be perpendicular or substantially perpendicular to the rotation axis of the first transmission component 400 .
[0074] Figure 5 It is a partial structural schematic diagram of an electric tail wing drive system according to one embodiment of the present disclosure.
[0075] In a specific embodiment, Figure 5 As shown, the second transmission component 500 includes a first end and a second end, and a first worm gear is formed on the outer surface of the second transmission component 500 (or, the second transmission component 500 includes a first worm gear), and the first worm gear is close to the first end of the second transmission component 500, wherein the first worm gear is connected to the first worm gear, thereby, the first transmission component 400 can drive the second transmission component 500 to rotate.
[0076] Furthermore, the second transmission component 500 includes a second worm gear, and the second worm gear is disposed close to the second end of the second transmission component 500 .
[0077] In a preferred embodiment, bearings are provided at both ends of the second transmission component 500 , and the bearings at both ends of the second transmission component 500 can be supported by the housing 100 and / or the cover 200 .
[0078] The second transmission component 500 is in transmission connection with the output shaft 700, and the second transmission component 500 drives the output shaft 700 to rotate; in a preferred embodiment, a second worm gear 701 is provided on the output shaft 700, and the second worm cooperates with the second worm gear 701, so that when the second transmission component 500 rotates, it can drive the output shaft 700 to rotate, and accordingly, power is output outwardly through the output shaft 700.
[0079] In the present disclosure, the second worm gear and a portion of the output shaft 700 are disposed in the accommodation space, that is, both ends of the output shaft 700 are located outside the housing 100 and the cover 200 .
[0080] like Figure 5As shown, the elastic component 600 is used to apply elastic force to the second transmission component 500, and the elastic force will cause positive pressure to exist between the second transmission component 500 and the output shaft 700. In addition, through the arrangement of the elastic component 600, the center distance between the second transmission component 500 (second worm) and the output shaft 700 (second worm wheel) can be reduced, thereby reducing side suction and improving the self-locking property of the electric tail wing drive system disclosed in the present invention.
[0081] More preferably, the elastic component 600 is provided only at the second end of the second transmission component 500, so that in a stationary state, the elastic component 600 can lift up the second end of the second transmission component 500. At this time, the second transmission component 500 will swing slightly with its first end as a fixed point, and the center distance between the second worm and the second worm wheel can be reduced, thereby reducing the side clearance and improving the self-locking property.
[0082] In the present disclosure, bearings are provided at both ends of the second transmission component 500, and the bearings can be supported on the housing 100 or the cover 200, and enable the second transmission component 500 to rotate. Accordingly, the elastic component 600 is arranged to contact the bearing provided at the second end of the second transmission component 500, and can apply elastic force to the bearing, thereby, the elastic component 600 is arranged close to the second end of the second transmission component 500, and the force application point of the elastic component 600 to the second transmission component 500 is close to the second end of the second transmission component 500.
[0083] In a preferred embodiment, the bearing can be selected as a deep groove ball bearing, an angular contact ball bearing, an angular contact roller bearing or the like.
[0084] Figure 6 is a schematic structural diagram of an elastic component according to an embodiment of the present disclosure.
[0085] like Figure 6 As shown, in the present disclosure, the elastic component 600 includes: a base 610, a first elastic part 620, and a second elastic part 630; wherein the base 610, the first elastic part 620 and the second elastic part 630 can be integrally formed, for example, by stamping or bending processes.
[0086] The base 610 is substantially in the shape of a thin sheet and includes a first end and a second end, wherein the first end and the second end may be the first end and the second end in the length direction of the base 610 .
[0087] The first elastic portion 620 is disposed at a first end of the base 610 , and the second elastic portion 630 is located at a second end of the base 610 . The elastic force is applied to the second transmission component 500 through elastic deformation of the first elastic portion 620 and the second elastic portion 630 .
[0088] Specifically, the first elastic portion 620 is the same as the second elastic portion 630, and the first elastic portion 620 is taken as an example for description below. The first elastic portion 620 includes a first bending portion 621 and a second bending portion 622, wherein one end of the first bending portion 621 is disposed at one end of the base 610, and the other end of the first bending portion 621 is disposed away from the base 610. In a preferred embodiment, the first bending portion 621 is disposed perpendicular or substantially perpendicular to the base 610.
[0089] One end of the second bending portion 622 is connected to the other end of the first bending portion 621, and the other end of the second bending portion 622 is arranged close to the base 610. That is, the second bending portion 622 can extend from the other end of the first bending portion 621 toward the direction close to the base 610, and the second bending portion 622, the first bending portion 621 and part of the base 610 together form a roughly triangular shape.
[0090] At this time, a portion of the outer surface of the second bent portion 622 can contact the bearing, so that an elastic force is applied to the bearing through the second bent portion 622. In a preferred embodiment, the elastic component 600 can be made of materials such as spring steel.
[0091] In the present disclosure, a first transmission ratio is defined between the first transmission component 400 and the second transmission component 500, and a second transmission ratio is defined between the second transmission component 500 and the output shaft 700. The first transmission ratio is the same as the second transmission ratio. In a preferred embodiment, the first transmission ratio and the second transmission ratio may both be 14, thereby enabling high torque output to be achieved through a low-power motor.
[0092] According to another aspect of the present disclosure, an electric tail system is provided, which includes the above-mentioned electric tail drive system.
[0093] According to another aspect of the present disclosure, a vehicle is provided, which includes the above-mentioned electric tail wing system.
[0094] In the description of this specification, the description with reference to the terms "one embodiment / method", "some embodiments / methods", "example", "specific example", or "some examples" etc. means that the specific features, structures, materials or characteristics described in conjunction with the embodiment / method or example are included in at least one embodiment / method or example of the present application. In this specification, the schematic representations of the above terms do not necessarily refer to the same embodiment / method or example. Moreover, the specific features, structures, materials or characteristics described may be combined in any one or more embodiments / methods or examples in a suitable manner. In addition, those skilled in the art may combine and combine the different embodiments / methods or examples described in this specification and the features of the different embodiments / methods or examples, unless they are contradictory.
[0095] In addition, the terms "first" and "second" are used for descriptive purposes only and should not be understood as indicating or implying relative importance or implicitly indicating the number of the indicated technical features. Therefore, the features defined as "first" and "second" may explicitly or implicitly include at least one of the features. In the description of this application, the meaning of "plurality" is at least two, such as two, three, etc., unless otherwise clearly and specifically defined.
[0096] Those skilled in the art should understand that the above embodiments are only for the purpose of clearly illustrating the present disclosure, and are not intended to limit the scope of the present disclosure. For those skilled in the art, other changes or modifications may be made based on the above disclosure, and these changes or modifications are still within the scope of the present disclosure.
Claims
1. An electric tail wing drive system, characterized in that: include: A driving device, the driving device is used to generate a driving force; A first transmission component, wherein the driving device is used to drive the first transmission component to rotate; A second transmission component, wherein the first transmission component cooperates with the second transmission component, and the first transmission component drives the second transmission component to rotate; An output shaft, wherein the second transmission component is in transmission connection with the output shaft, and the second transmission component drives the output shaft to rotate; as well as An elastic component is used to apply an elastic force to the second transmission component, and the elastic force causes a positive pressure to exist between the second transmission component and the output shaft.
2. The electric tail wing drive system according to claim 1, characterized in that: The first transmission component is a first worm, and the first transmission component and the driving device have the same rotation axis.
3. The electric tail wing drive system according to claim 2, characterized in that: The driving device is connected to the first transmission component via a coupling.
4. The electric tail wing drive system according to claim 1, characterized in that: The second transmission member includes a first end, wherein A first worm gear is formed on the outer surface of the second transmission component, and the first worm gear is close to the first end of the second transmission component, wherein the first worm gear is drivingly connected to the first worm.
5. The electric tail wing drive system according to claim 4, characterized in that: The second transmission component includes a second end, and the second transmission component includes a second worm, and the second worm is arranged near the second end of the second transmission component.
6. The electric tail wing drive system according to claim 5, characterized in that: The elastic component is arranged close to the second end of the second transmission component, and the force application point of the elastic component to the second transmission component is close to the second end of the second transmission component.
7. The electric tail wing drive system according to claim 6, characterized in that: A bearing is disposed at the second end of the second transmission component, and the elastic component is in contact with the bearing and can apply elastic force to the bearing.
8. The electric tail wing drive system according to claim 7, characterized in that: The output shaft is provided with a second worm gear, and the second worm is matched with the second worm gear.
9. The electric tail wing drive system according to claim 7, characterized in that: The elastic component comprises: a base having a first end and a second end; A first elastic part and a second elastic part, wherein the first elastic part is arranged at the first end of the base, and the second elastic part is located at the second end of the base, and elastic force is applied to the second transmission component through elastic deformation of the first elastic part and the second elastic part.
10. The electric tail wing drive system according to claim 9, characterized in that: The first elastic portion is the same as the second elastic portion, and both include a first bending portion and a second bending portion, wherein one end of the first bending portion is arranged at one end of the base, one end of the second bending portion is connected to the other end of the first bending portion, and the other end of the second bending portion is arranged close to the base.
11. The electric tail wing drive system according to claim 1, characterized in that: It also includes a shell and a cover body, wherein the cover body is arranged on the shell, and an accommodating space is formed between the shell and the cover body, and the driving device, the first transmission component, the second transmission component and the elastic component are arranged in the accommodating space.
12. The electric tail wing drive system according to claim 11, characterized in that: The shell has a first end face facing the cover body, and the cover body has a second end face facing the shell, wherein a groove is formed on one of the first end face and the second end face, and a protrusion is formed on the other of the first end face and the second end face, and when the shell and the cover body are installed together, at least a part of the protrusion is located in the groove.
13. The electric tail wing drive system according to claim 12, characterized in that: A sealing component is arranged in the groove, and the protrusion causes the sealing component to be deformed.
14. The electric tail wing drive system according to claim 13, characterized in that: The sealing component includes a rubber ring.
15. The electric tail wing drive system according to claim 1, characterized in that: A first transmission ratio is defined between the first transmission component and the second transmission component, a second transmission ratio is defined between the second transmission component and the output shaft, and the first transmission ratio is the same as the second transmission ratio.
16. An electric tail system, characterized in that: An electric tail wing drive system comprising any one of claims 1-15.
17. A vehicle, characterized in that: Includes the electric tail system as described in claim 16.
Citation Information
Patent Citations
Electric empennage driving device, electric empennage system and automobile
CN214689805U