Electric empennage lifting mechanism, automobile electric empennage and automobile thereof

Abstract

The utility model relates to the technical field of vehicles, in particular to an electric empennage lifting mechanism, an electric empennage and an automobile with the electric empennage. An electric empennage lifting mechanism comprises a supporting seat; a support plate; the lifting unit is mounted on the supporting seat and connected with the supporting plate, and the lifting unit has a folded state and an unfolded state; wherein the supporting seat is provided with a first limiting point, a second limiting point and a third limiting point, and the supporting plate is provided with a fourth limiting point and a fifth limiting point; when the lifting unit is in a folded state, the lifting unit is limited and propped against the first limiting point and the second limiting point respectively; when the lifting unit is in the unfolded state, the lifting unit abuts against the third limiting point, the fourth limiting point and the fifth limiting point for limiting. The method is better in stability.

Description

Technical Field

[0001] The present application relates to the field of vehicle technology, and in particular to an electric tail wing lifting mechanism, an electric tail wing of a car, and a car thereof. Background Art

[0002] The main function of the electric rear wing is to increase downforce. When the vehicle reaches a certain speed, the electric rear wing opens, thereby generating downforce in the rear wing area, allowing the car to have greater grip and effectively reducing the air resistance generated by the car during high-speed driving.

[0003] The electric tail generally includes a tail and a lifting structure, which is connected to the tail to drive the tail to do lifting motion, so as to realize the expansion or folding of the tail. However, the existing electric tail has poor stability whether in the expanded state or the folded state. Utility Model Content

[0004] Based on this, it is necessary to provide an electric tail wing lifting mechanism with good stability, an automobile electric tail wing and an automobile thereof.

[0005] In order to solve the above technical problems, this application provides the following technical solutions:

[0006] 1. The electric tail lifting mechanism of claim 1, wherein the electric tail lifting mechanism comprises: a support seat; a support plate for supporting the tail plate of the electric tail; a lifting unit, which is installed on the support seat and connected to the support plate, and the lifting unit has a folded state and an unfolded state, and the lifting unit can switch between the folded state and the unfolded state in response to an external force to drive the support plate to perform a lifting / lowering movement relative to the support seat; wherein a first limit point, a second limit point and a third limit point are arranged on the support seat, and a fourth limit point and a fifth limit point are arranged on the support plate; when the lifting unit is in the folded state, the lifting unit is limited and abutted against the first limit point and the second limit point respectively; when the lifting unit is in the unfolded state, the lifting unit is limited and abutted against the third limit point, the fourth limit point and the fifth limit point respectively.

[0007] In one embodiment, the lifting unit includes an active rod, a first rod, a second rod, a third rod, a fourth rod and a fifth rod; one end of the active rod is hinged to the support seat, and the other end is provided with a first abutment point; one end of the first rod is hinged to the support seat, and the other end is provided with a second abutment point and a third abutment point; one end of the second rod is hinged to the active rod, and the other end is hinged to the first rod; one end of the third rod is hinged to the first rod, and the other end is hinged to the support plate; the fourth rod is hinged to the support seat, the fifth rod is rotatably connected to the second rod and one end of the fifth rod is hinged to the fourth rod, and the other end is hinged to the support plate, and a fourth abutment point is provided on the fourth rod and / or the fifth rod; wherein, when the lifting unit is in a folded state, the first abutment point forms an abutment limit with the first limit point, and the fourth abutment point forms an abutment limit with the second limit point;

[0008] When the lifting unit is in an unfolded state, the first abutting point abuts against the third limiting point for limiting position, the second abutting point abuts against the fourth limiting point for limiting position, and the third abutting point abuts against the fifth limiting point.

[0009] In one embodiment, the support seat is provided with a receiving groove having an opening, and the folded lifting unit can be at least partially accommodated in the receiving groove through the opening; the first limit point and the second limit point are arranged in the receiving groove, and the third limit point is arranged at the opening.

[0010] In one of the embodiments, two convex portions are arranged at intervals on the groove wall at the opening of the receiving groove, and a limiting groove is formed between the two convex portions, and the third limiting point is located in the limiting groove.

[0011] In one of the embodiments, a first convex column and a first flexible member are disposed at the bottom of the receiving groove, and the first flexible member is disposed on the first convex column to form the second limiting point.

[0012] In one of the embodiments, a second flexible member is sleeved on one end of the active rod away from the support seat.

[0013] In one of the embodiments, the support seat is provided with a third flexible member at the fourth limit point and the fifth limit point.

[0014] In one embodiment, the connection between the first rod and the support seat is configured as a transition fit; and / or, the connection between the second rod and the active rod and the first rod is configured as a transition fit; the connection between the third rod and the first rod and the support plate is configured as a transition fit; the connection between the fourth rod and the support seat is configured as a transition fit; the connection between the fifth rod and the second rod, the fourth rod and the support plate is configured as a transition fit.

[0015] This application also provides the following technical solutions:

[0016] An electric rear wing for an automobile comprises the electric rear wing lifting mechanism described in any one of the above embodiments.

[0017] This application also provides the following technical solutions:

[0018] A car comprises the electric rear wing described in any one of the above embodiments.

[0019] Compared with the prior art, the electric tail wing lifting mechanism is provided with a first limit point, a second limit point, a third limit point, a fourth limit point and a fifth limit point; when the lifting unit is in a folded state, the lifting unit is respectively limited and abutted against the first limit point and the second limit point; when the lifting unit is in an unfolded state, the lifting unit is respectively abutted against the third limit point, the fourth limit point and the fifth limit point. In this way, no matter the lifting unit is in an unfolded state or a folded state, it can be effectively limited, avoiding the lifting unit from shaking, and effectively improving the stability of the electric tail wing. BRIEF DESCRIPTION OF THE DRAWINGS

[0020] In order to more clearly illustrate the technical solutions in the embodiments of the present application or the conventional technology, the drawings required for use in the embodiments or the conventional technology descriptions are briefly introduced below. Obviously, the drawings described below are only some embodiments of the present application. For ordinary technicians in this field, other drawings can be obtained based on these drawings without creative work.

[0021] Figure 1 This is a schematic diagram of the three-dimensional structure of the electric rear wing of a car provided in this application in a folded state.

[0022] Figure 2 This is a schematic diagram of the three-dimensional structure of the electric rear wing of a car provided in this application when it is unfolded.

[0023] Figure 3 This is a one-view stereoscopic structural schematic diagram of the electric tail wing lifting mechanism provided in the present application in a folded state.

[0024] Figure 4This is a schematic diagram of the three-dimensional structure from another perspective of the electric tail wing lifting mechanism provided in the present application in the folded state.

[0025] Figure 5 A one-view stereoscopic structural schematic diagram of the electric tail wing lifting mechanism provided in the present application in the unfolded state.

[0026] Figure 6 This is a schematic diagram of the three-dimensional structure from another perspective of the electric tail wing lifting mechanism provided in this application in the unfolded state.

[0027] The reference numerals of the components are as follows:

[0028] 100. Electric tail wing lifting mechanism; 10. Support seat; 11. First limiting point; 12. Second limiting point; 13. Third limiting point; 14. Receiving groove; 141. Opening; 142. First boss; 143. First flexible member; 15. Protrusion; 16. Limiting groove; 20. Support plate; 21. Fourth limiting point; 22. Fifth limiting point; 23. Third flexible member; 24. Boss; 30. Lifting unit; 31. Active rod; 311. First abutment point; 312. Second flexible member; 32. First rod; 321. Second abutment point; 322. Third abutment point; 33. Second rod; 34. Third rod; 35. Fourth rod; 351. Fourth abutment point; 36. Fifth rod; 200. Automobile electric tail wing; 201. Tail wing plate; 202. Driving mechanism; 203. Motor; 204. Driving shaft. DETAILED DESCRIPTION

[0029] In order to make the above-mentioned purposes, features and advantages of the present application more obvious and easy to understand, the specific implementation methods of the present application are described in detail below in conjunction with the accompanying drawings. In the following description, many specific details are set forth to facilitate a full understanding of the present application. However, the present application can be implemented in many other ways different from those described herein, and those skilled in the art can make similar improvements without violating the connotation of the present application, so the present application is not limited by the specific embodiments disclosed below.

[0030] It should be noted that when a component is referred to as being "fixed to" or "disposed on" another component, it may be directly on the other component or there may also be a central component. When a component is considered to be "connected to" another component, it may be directly connected to the other component or there may be a central component at the same time. The terms "vertical", "horizontal", "upper", "lower", "left", "right" and similar expressions used in the specification of this application are for illustrative purposes only and do not represent the only implementation method.

[0031] 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.

[0032] In the present application, unless otherwise clearly specified and limited, a first feature being “above” or “below” a second feature may mean that the first feature is directly in contact with the second feature, or the first feature and the second feature are in contact indirectly through an intermediate medium. Moreover, a first feature being “above”, “above”, or “above” a second feature may mean that the first feature is directly above or obliquely above the second feature, or simply means that the first feature is higher in level than the second feature. A first feature being “below”, “below”, or “below” a second feature may mean that the first feature is directly below or obliquely below the second feature, or simply means that the first feature is lower in level than the second feature.

[0033] Unless otherwise defined, all technical and scientific terms used in the specification of this application have the same meaning as those commonly understood by those skilled in the art to which this application belongs. The terms used in the specification of this application are only for the purpose of describing specific embodiments and are not intended to limit this application. The term "and / or" used in the specification of this application includes any and all combinations of one or more related listed items.

[0034] like Figure 1 and Figure 2 As shown, the present application provides an electric rear wing 200 for an automobile, which is installed at a rear position in the length direction x of the automobile, such as a trunk lid or a rear door.

[0035] For details, please continue to refer to Figure 1 and Figure 2 The electric rear wing 200 of the automobile includes a rear wing panel 201, an electric rear wing lifting mechanism 100 and a driving mechanism 202. The rear wing panel 201 is installed on the electric rear wing lifting mechanism 100, and the driving mechanism 202 is connected to the driving mechanism 202 to drive the electric rear wing lifting mechanism 100 to perform an ascending / descending movement in the vertical direction z of the automobile, thereby driving the rear wing panel 201 to fold or unfold.

[0036] Here, the driving mechanism 202 includes a motor 203 and a driving shaft 204, the driving shaft 204 is connected to the motor 203, and the electric tail lifting mechanism 100 is connected to the driving shaft. In this way, under the drive of the motor 203, the driving shaft 204 drives the electric tail lifting mechanism 100 to rise / fall.

[0037] In one embodiment, if Figures 2 to 6 As shown, the electric tail wing lifting mechanism 100 includes a support base 10, a support plate 20 and a lifting unit 30. The support base 10 is used as a base for carrying and installing various components. The support plate 20 is used to support the tail wing plate 201; the lifting unit 30 is installed on the support base 10 and connected to the support plate 20, and the lifting unit 30 has a folded state (refer to Figure 3 ) and expanded state (reference Figure 5 ), the lifting unit 30 can switch between the folded state and the unfolded state in response to external force, so as to drive the support plate 20 to move up / down relative to the support seat 10, thereby realizing the folding or unfolding of the tail wing panel 201.

[0038] Furthermore, if Figures 3 to 6 As shown, the support seat 10 is provided with a first limiting point 11, a second limiting point 12 and a third limiting point 13, and the support plate 20 is provided with a fourth limiting point 21 and a fifth limiting point 22; when the lifting unit 30 is in the folded state, the lifting unit 30 is respectively limited and abutted against the first limiting point 11 and the second limiting point 12; when the lifting unit 30 is in the unfolded state, the lifting unit 30 is respectively limited and abutted against the third limiting point 13, the fourth limiting point 21 and the fifth limiting point 22. In this way, no matter whether the lifting unit 30 is in the folded state or the unfolded state, it can be limited by the limiting points, thereby avoiding the shaking of the lifting unit 30, and effectively improving the stability of the tail wing plate 201. Here, the lifting unit 30 responds to the external force action, that is, the lifting unit 30 is driven by the driving shaft 204, and switches between the folded state and the unfolded state.

[0039] like Figure 3 and Figure 4 As shown, the support base 10 is provided with a receiving groove 14 having an opening 141, and the folded lifting unit 30 can be partially accommodated in the receiving groove 14 through the opening 141. The first limiting point 11 and the second limiting point 12 are arranged in the receiving groove 14, and the third limiting point 13 is arranged at the opening 141. That is, when the lifting unit 30 is in the folded state, it can be accommodated in the receiving groove 14, thereby reducing the space occupied by the lifting unit 30 and making the overall structure more compact.

[0040] Preferably, the first limiting point 11 and the second limiting point 12 are both located at the bottom of the receiving groove 14 .

[0041] In one embodiment, if Figure 3 As shown, the first limiting point 11 is the bottom of the receiving groove 14. Of course, the first limiting point 11 is not limited to the bottom of the receiving groove 14 itself, and a protrusion can also be set at the bottom of the receiving groove 14 for abutment and limiting.

[0042] Furthermore, a first flexible member 143 is disposed at the bottom of the receiving groove 14, and the first flexible member 143 forms the second limiting point 12. Here, the first flexible member 143 is configured as a relatively soft member such as rubber or silicone. Thus, when the second limiting point 12 is limited and abutted, the first flexible member 143 can buffer the extrusion during the abutment process, and avoid abnormal noise, etc.

[0043] Furthermore, if Figure 4 As shown, two convex portions 15 are arranged at intervals on the groove wall at the opening 141 of the receiving groove 14, and a limiting groove 16 is formed between the two convex portions 15, and the third limiting point 13 is located in the limiting groove 16. That is, the limiting groove 16 can further realize the limiting, thereby improving the reliability of the limiting.

[0044] In one embodiment, if Figure 5 and Figure 6 As shown, the support plate 20 is provided with a third flexible member 23 at the fourth limit point 21 and the fifth limit point 22. Thus, when the lifting unit 30 is abutted and limited at the fourth limit point 21 and the fifth limit point 22, the third flexible member 23 can buffer the extrusion during the abutment process, and avoid abnormal noise and the like.

[0045] Here, the third flexible member 23 is configured as a relatively soft member such as rubber or silica gel.

[0046] Preferably, a convex column 24 is provided on the support plate 20 , and the third flexible member 23 is sleeved on the convex column 24 , so as to form a fourth limiting point 21 .

[0047] like Figure 5 and Figure 6 As shown, in one embodiment, the lifting unit 30 includes an active rod 31, a first rod 32, a second rod 33, a third rod 34, a fourth rod 35 and a fifth rod 36; one end of the active rod 31 is hinged to the support seat 10, and the other end is provided with a first abutment point 311; one end of the first rod 32 is hinged to the support seat 10, and the other end is provided with a second abutment point 321 and a third abutment point 322; one end of the second rod 33 is hinged to the active rod 31, and the other end is hinged to the first rod 32; one end of the third rod 34 is hinged to the first rod 32, and the other end is hinged to the support plate 20; the fourth rod 35 is hinged to the support seat 10, the fifth rod 36 is rotatably connected to the second rod 33 and one end of the fifth rod 36 is hinged to the fourth rod 35, and the other end is hinged to the support plate 20, and a fourth abutment point 351 is provided on the fourth rod 35 and / or the fifth rod 36; wherein, with reference to Figure 3 and Figure 4 When the lifting unit 30 is in the folded state, the first abutting point 311 forms an abutting limit with the first limiting point 11, and the fourth abutting point 351 forms an abutting limit with the second limiting point 12. Figure 5 and Figure 6 When the lifting unit 30 is in the unfolded state, the first abutting point 311 abuts against the third limiting point 13, the second abutting point 321 abuts against the fourth limiting point 21, and the third abutting point 322 abuts against the fifth limiting point 22. In this way, the lifting unit 30 is limited in the unfolded state or the folded state through the first abutting point 311, the second abutting point 321, the third abutting point 322 and the fourth abutting point 351.

[0048] Furthermore, a second flexible member 312 is sleeved on one end of the active rod 31 away from the support seat 10. The second flexible member 312 is used to limit and flexibly abut against the first abutment point 311. In this way, the impact force during the abutment process is reduced, thereby reducing abnormal noise and improving the comfort of use.

[0049] like Figure 5 and Figure 6 As shown, the connection between the first rod 32 and the support seat 10 is configured as a transition fit; the connection between the second rod 33 and the active rod 31 and the first rod 32 is configured as a transition fit; the connection between the third rod 34 and the first rod 32 and the support plate 20 is configured as a transition fit; the connection between the fourth rod 35 and the support seat 10 is configured as a transition fit; the connection between the fifth rod 36 and the second rod 33, the fourth rod 35 and the support plate 20 is configured as a transition fit.

[0050] It should be explained that transition fit means that the tolerance zone of the hole overlaps the tolerance zone of the shaft. That is, in the lifting unit 30, the matching clearance between the rod and the support seat, the rod and the support plate, and the rods can be minimized through transition fit, thereby reducing looseness and further improving the stability of the lifting unit 30.

[0051] The present application also provides a car, which includes the car electric rear wing 200 in any of the above embodiments.

[0052] The technical features of the above-described embodiments may be arbitrarily combined. To make the description concise, not all possible combinations of the technical features in the above-described embodiments are described. However, as long as there is no contradiction in the combination of these technical features, they should be considered to be within the scope of this specification.

[0053] The above-described embodiments only express several implementation methods of the present application, and the descriptions thereof are relatively specific and detailed, but they cannot be understood as limiting the scope of the patent application. It should be pointed out that, for a person of ordinary skill in the art, several variations and improvements can be made without departing from the concept of the present application, and these all belong to the protection scope of the present application. Therefore, the scope of patent protection of the present application shall be subject to the attached claims.

Claims

1. An electric tail lifting mechanism, characterized in that: The electric tail lifting mechanism comprises: Support seat (10); A support plate (20) for supporting a tail wing plate (201) of an electric tail wing; A lifting unit (30) is installed on the support base (10) and connected to the support plate (20), and the lifting unit (30) has a folded state and an unfolded state. The lifting unit (30) can switch between the folded state and the unfolded state in response to an external force, so as to drive the support plate (20) to perform an ascending / descending movement relative to the support base (10); The support seat (10) is provided with a first limit point (11), a second limit point (12) and a third limit point (13), and the support plate (20) is provided with a fourth limit point (21) and a fifth limit point (22); when the lifting unit (30) is in a folded state, the lifting unit (30) is respectively abutted against the first limit point (11) and the second limit point (12) for limit; when the lifting unit (30) is in an unfolded state, the lifting unit (30) is respectively abutted against the third limit point (13), the fourth limit point (21) and the fifth limit point (22) for limit.

2. The electric tail wing lifting mechanism according to claim 1, characterized in that: The lifting unit (30) comprises an active rod (31), a first rod (32), a second rod (33), a third rod (34), a fourth rod (35) and a fifth rod (36); one end of the active rod (31) is hinged to the support seat (10), and the other end is provided with a first abutment point (311); One end of the first rod (32) is hinged to the support seat (10), and the other end is provided with a second abutment point (321) and a third abutment point (322); one end of the second rod (33) is hinged to the active rod (31), and the other end is hinged to the first rod (32); one end of the third rod (34) is hinged to the first rod (32), and the other end is hinged to the support plate (20); the fourth rod (35) is hinged to the support seat (10), the fifth rod (36) is rotatably connected to the second rod (33), one end of the fifth rod (36) is hinged to the fourth rod (35), and the other end is hinged to the support plate (20), and a fourth abutment point (351) is provided on the fourth rod (35) and / or the fifth rod (36); Wherein, when the lifting unit (30) is in a folded state, the first abutting point (311) and the first limiting point (11) form an abutting limit, and the fourth abutting point (351) and the second limiting point (12) form an abutting limit; When the lifting unit (30) is in an unfolded state, the first abutment point (311) abuts against the third limit point (13) for limit, the second abutment point (321) abuts against the fourth limit point (21) for limit, and the third abutment point (322) abuts against the fifth limit point (22).

3. The electric tail wing lifting mechanism according to claim 2, characterized in that: The support seat (10) is provided with a receiving groove (14) having an opening (141), and the folded lifting unit (30) can be at least partially accommodated in the receiving groove (14) through the opening (141); The first limiting point (11) and the second limiting point (12) are arranged in the receiving groove (14), and the third limiting point (13) is arranged at the opening (141).

4. The electric tail wing lifting mechanism according to claim 3, characterized in that: Two convex portions (15) are arranged at intervals on the groove wall at the opening (141) of the receiving groove (14), and a limiting groove (16) is formed between the two convex portions (15), and the third limiting point (13) is located in the limiting groove (16).

5. The electric tail wing lifting mechanism according to claim 3, characterized in that: A first convex column (142) and a first flexible member (143) are provided at the bottom of the receiving groove (14); the first flexible member (143) is arranged on the first convex column (142) and forms the second limiting point (12).

6. The electric tail wing lifting mechanism according to claim 2, characterized in that: A second flexible member (312) is sleeved on one end of the active rod (31) away from the support seat (10).

7. The electric tail wing lifting mechanism according to claim 2, characterized in that: The support seat (10) is provided with a third flexible member (23) at the positions of the fourth limiting point (21) and the fifth limiting point (22).

8. The electric tail wing lifting mechanism according to claim 2, characterized in that: The connection between the first rod (32) and the support seat (10) is configured as a transition fit; and / or the connection between the second rod (33) and the active rod (31) and the first rod (32) is configured as a transition fit; the connection between the third rod (34) and the first rod (32) and the support plate (20) is configured as a transition fit; the connection between the fourth rod (35) and the support seat (10) is configured as a transition fit; the connection between the fifth rod (36) and the second rod (33), the fourth rod (35) and the support plate (20) is configured as a transition fit.

9. An electric rear wing for a car, characterized in that: It comprises the electric tail lifting mechanism as described in any one of claims 1 to 8.

10. An automobile, characterized in that: The electric rear wing of an automobile comprises the electric rear wing of claim 9.

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