Lightweight fairing assembly structure

Abstract

The utility model discloses a light weight fairing assembly structure which comprises a fairing shell, the fairing shell is a streamline cavity shell, a supporting framework is arranged in the fairing shell, the supporting framework is attached to the inner wall of the fairing shell, and a stable connecting structure is arranged on the supporting framework. According to the light weight fairing, the fairing shell and the supporting framework form a composite anti-bending system through the multidirectional rib plate network, and the I-shaped main beam is combined with the gradient transverse rib plates to improve the load transmission efficiency; threaded locking of the inserting rod and the connecting base in the stable connecting structure is matched with the hollow vibration reduction design of the stabilizing rod, multi-point dynamic anchoring is achieved, high-speed wind resistance is effectively dispersed, tremor is restrained, the triangular reinforcing plate strengthens the transverse bearing force of the connecting body, and the problems that the structural rigidity is insufficient and connection is prone to damage are comprehensively solved on the premise of light weight.

Description

Technical Field

[0001] This utility model relates to the field of fairing technology, specifically to a lightweight fairing assembly structure. Background Technology

[0002] Fairings are a common component in modern automotive systems, widely used in the main structure of automobiles to reduce wind resistance and assist in heat dissipation. Therefore, most current automotive fairings have a streamlined structure. In order to maximize the effectiveness of fairings, their structure mainly uses lightweight materials, such as engineering plastics and lightweight aluminum alloys.

[0003] The fairing structure is mainly connected to the main body of the car using a fixed frame. However, due to the use of lightweight materials in the current fairing, the fairing's ability to resist external impacts is reduced. At the same time, the fairing is subject to greater air resistance at high speeds. Because of its light weight, the fairing is very prone to vibration, which increases the car's wind resistance and may cause breakage at the connection points, affecting driving safety. In view of this, in-depth research was conducted on the above problems, which led to this case. Utility Model Content

[0004] To address the shortcomings of existing technologies, this utility model provides a lightweight fairing assembly structure, which solves the existing background technology problems.

[0005] To achieve the above objectives, this utility model is implemented through the following technical solution: a lightweight fairing assembly structure, including a fairing shell, the fairing shell being a streamlined cavity shell, a support frame being provided inside the fairing shell, the support frame being fitted to the inner wall of the fairing shell, and a stable connection structure being provided on the support frame;

[0006] The stable connection structure includes a connector, which is mounted on the vehicle body. The connector is provided with at least one pair of stabilizer bars, a pair of control slots are provided on the pair of stabilizer bars, and a pair of connecting seats are provided on the pair of control slots.

[0007] The stable connection structure also includes at least one pair of insert rods. A pair of insert rods are provided on one side of the support frame. The pair of insert rods are inserted into corresponding control slots. The pair of insert rods are connected to a pair of connecting seats. A pair of movable slots are provided on the support frame. The pair of insert rods are movably installed on the pair of movable slots.

[0008] Preferably, a pair of triangular reinforcing plates are provided on both sides of the stabilizer bar and connected to the connecting body.

[0009] Preferably, the front end of the rectifier housing is provided with a plurality of positioning holes, and the front end of the connector is provided with a plurality of fixing holes corresponding to the plurality of positioning holes, and a plurality of fixing bolts are inserted into the plurality of positioning holes and threadedly connected to the plurality of fixing holes.

[0010] Preferably, the support frame is fitted to the inner side of the rectifier housing, and a pair of the movable slots penetrate the top of the rectifier housing.

[0011] Preferably, the connecting seat has an internal thread structure, and the connecting seat is threadedly connected to the end of the insert rod.

[0012] Preferably, the top end of the insertion rod penetrates the top of the rectifier housing, and a rotating seat is provided at the top end of the insertion rod. The rotating seat has a hexagonal rotating groove, and a ring-shaped shock-absorbing pad is provided below the rotating seat. The shock-absorbing pad matches the rotating groove. Beneficial effects

[0013] This utility model provides a lightweight fairing assembly structure. It offers the following advantages: the lightweight fairing's shell and supporting frame form a composite bending-resistant system through a multi-directional stiffener network; the I-beam main beam combined with gradient transverse stiffeners improves load transfer efficiency; the threaded locking of the insert rod and connecting seat in the stable connection structure, along with the hollow vibration-damping design of the stabilizer rod, achieves multi-point dynamic anchoring, effectively dispersing high-speed wind resistance and suppressing vibration; and the triangular reinforcing plate strengthens the transverse load-bearing capacity of the connecting body. Under the premise of lightweight design, it comprehensively solves the problems of insufficient structural rigidity and easy connection damage. Attached Figure Description

[0014] Figure 1 This is a three-dimensional structural diagram of a lightweight fairing assembly according to the present invention.

[0015] Figure 2 This is a bottom view of the lightweight fairing assembly structure described in this utility model.

[0016] Figure 3 This is a three-dimensional explosive structure diagram of a lightweight fairing assembly structure described in this utility model.

[0017] In the diagram: 1. Fairing housing; 2. Support frame; 3. Connector; 4. Stabilizer bar; 5. Control slot; 6. Insert rod; 7. Movable slot; 8. Reinforcing plate; 9. Positioning hole; 10. Fixing bolt; 11. Rotating seat. Detailed Implementation

[0018] The technical solutions of the present utility model will be clearly and completely described below with reference to the accompanying drawings of the embodiments. Obviously, the described embodiments are only some embodiments of the present utility model, and not all embodiments. Based on the embodiments of the present utility model, all other embodiments obtained by those of ordinary skill in the art without creative effort are within the protection scope of the present utility model.

[0019] Please see Figure 1-3 This utility model provides an implementation scheme: the current fairing material adopts a lightweight structure, which reduces the fairing's ability to resist external impacts. At the same time, the fairing suffers greater air resistance at high speeds. Because of its light weight, the fairing is very prone to vibration, which increases the vehicle's wind resistance and causes breakage at connection points, affecting driving safety.

[0020] According to the instruction manual Figure 1-3 As can be seen, in order to ensure the structural stability of the lightweight fairing and reduce the vibration problem caused by wind resistance during high-speed driving, this application discloses a lightweight fairing assembly structure, including a fairing shell 1. The fairing shell 1 is a streamlined cavity shell, which forms a composite bending resistance system with the support frame 2. The support frame 2 is set in close contact with the inner wall of the fairing shell 1 and adopts a multi-directional stiffener network structure. The main beam section is I-shaped and the transverse stiffener spacing is gradient distributed to achieve uniform load transfer.

[0021] To ensure the stability of the diffuser at high speeds, this application also discloses a stable connection structure. The connector 3 of the stable connection structure is rigidly connected to the vehicle body by high-strength bolts. The connector 3 adopts an aluminum alloy frame, which has the characteristics of high structural strength and light weight. The stabilizer bar 4 adopts a hollow vibration damping design. The control groove 5 inside the stabilizer bar 4 has a built-in connector seat. During installation, the plug rod 6 is inserted into the stabilizer bar 4 and threadedly connected to the connector seat. On the one hand, the connector 3 is connected to the fairing shell 1 through the plug rod 6. On the other hand, the multi-point plug rod 6 structure can ensure more stable installation of the fairing shell.

[0022] As a preferred option, triangular reinforcing plates 8 are provided on both sides of the stabilizer bar 4 and welded to the connector 3 to form a triangular support structure, which significantly improves the lateral load-bearing capacity. The front end of the fairing is provided with positioning holes 9, which are precisely matched with the fixing holes of the connector 3 through anti-loosening bolts to ensure installation stability.

[0023] As a preferred option, the pair of movable slots 7 of the supporting frame 2 extend through the top of the rectifier housing, and a rotating seat 11 with a shock-absorbing pad is set at the top of the insert rod 6. The hexagonal rotating slot design facilitates installation and adjustment. The insert rod 6 and the connecting seat are connected by a threaded locking connection, and with the guiding structure of the movable slots 7, dynamic displacement compensation is achieved to avoid stress concentration.

[0024] As a preferred option, the connection between the stabilizer bar 4 and the connecting body 3 is further strengthened by multiple sets of reinforcing plates 8 to disperse vibration energy, and an elastic buffer layer is provided on the contact surface between the support frame 2 and the fairing shell 1 to absorb local deformation stress.

[0025] As a preferred option, the shock-absorbing pad at the end of the insertion rod 6 adopts a ring-shaped multi-layer composite structure, which fits with the movable groove 7 with a gap. This can suppress high-frequency vibration and allow low-speed deformation displacement, thereby improving the durability of the connection part.

[0026] As a preferred option, the streamlined cavity of the fairing 1 and the supporting frame 2 form a synergistic wind resistance structure. The aerodynamic shape is optimized to reduce air turbulence, while the internal frame network is used to enhance bending resistance, thus comprehensively solving the contradiction between lightweight and structural rigidity.

[0027] In summary, this lightweight fairing, with its fairing shell 1 and supporting frame 2 forming a composite bending resistance system through a multi-directional stiffener network, and its I-beam main beam combined with gradient transverse stiffeners to improve load transfer efficiency, and its stable connection structure with the threaded locking of the insert rod 6 and the connecting seat, and the hollow vibration reduction design of the stabilizer rod 4 to achieve multi-point dynamic anchoring, effectively disperses high-speed wind resistance and suppresses vibration, and the triangular reinforcing plate 8 strengthens the transverse bearing capacity of the connecting body 3, comprehensively solving the problems of insufficient structural rigidity and easy connection damage under the premise of lightweight design.

[0028] Although embodiments of the present invention have been shown and described, it will be understood by those skilled in the art that various changes, modifications, substitutions and alterations can be made to these embodiments without departing from the principles and spirit of the present invention, the scope of which is defined by the appended claims and their equivalents.

Claims

1. A lightweight fairing assembly structure, comprising a fairing shell (1), wherein the fairing shell (1) is a streamlined cavity shell, and a support frame (2) is provided inside the fairing shell (1), characterized in that, The support frame (2) is fitted to the inner wall of the rectifier shell (1), and a stable connection structure is provided on the support frame (2); The stable connection structure includes a connector (3), which is mounted on the vehicle body. At least one pair of stabilizer bars (4) are provided on the connector (3). A pair of control slots (5) are provided on the pair of stabilizer bars (4), and a pair of connecting seats are provided on the pair of control slots (5). The stable connection structure also includes at least one pair of insert rods (6). A pair of insert rods (6) are provided on one side of the support frame (2). The pair of insert rods (6) are inserted into the corresponding control slots (5). The pair of insert rods (6) are connected to a pair of connecting seats. A pair of movable slots (7) are provided on the support frame (2). The pair of insert rods (6) are movably installed on the pair of movable slots (7).

2. The lightweight fairing assembly structure according to claim 1, characterized in that, The stabilizer bar (4) has a pair of triangular reinforcing plates (8) on both sides that are connected to the connector (3).

3. The lightweight fairing assembly structure according to claim 2, characterized in that, The front end of the rectifier cover is provided with a number of positioning holes (9), and the front end of the connector (3) is provided with a number of fixing holes corresponding to the number of positioning holes (9). A number of fixing bolts (10) are inserted into the number of positioning holes (9) and threadedly connected to the number of fixing holes.

4. The lightweight fairing assembly structure according to claim 3, characterized in that, The support frame (2) is attached to the inner side of the rectifier housing, and a pair of movable slots (7) penetrate the top of the rectifier housing.

5. The lightweight fairing assembly structure according to claim 4, characterized in that, The connecting seat has an internal thread structure and is threaded to the end of the insert rod (6).

6. The lightweight fairing assembly structure according to claim 5, characterized in that, The top of the insert (6) penetrates the top of the rectifier housing. A rotating seat (11) is provided at the top of the insert (6). A hexagonal rotating groove is provided on the rotating seat (11). A ring-shaped shock-absorbing pad is provided below the rotating seat (11). The shock-absorbing pad matches the movable groove (7).

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