阅读说明：本技术 一种方程式赛车改善前轮绕流的前翼结构 (Front wing structure for improving front wheel streaming of formula car ) 是由 林继铭 周义翔 黎俊杰 于鹏 张勇 于 2021-08-09 设计创作，主要内容包括：本发明公开了一种方程式赛车改善前轮绕流的前翼结构,该前翼结构包括主翼、水平端板、外侧竖直端板、外侧襟翼、中间竖直端板、内侧襟翼和内侧竖直端板；外侧襟翼包括依次连接的襟翼水平段、襟翼折弯段和襟翼竖直段,襟翼水平段与中间竖直端板相固接、襟翼竖直段与水平端板相固接,襟翼水平段与襟翼竖直段之间的夹角呈90度；且,该外侧襟翼在襟翼折弯段产生了扭转,使得该外侧襟翼前缘与后缘之间的连线与xy平面之间的夹角α与该外侧襟翼前缘与后缘之间的连线与xz平面之间的夹角β不相同。该前翼结构简单,可靠性高,成本低,易于制造,具有很好的推广价值。同时,外侧襟翼的特殊结构可减少因轮胎绕流而造成的阻力。(The invention discloses a front wing structure for improving the flow around a front wheel of an equation racing car, which comprises a main wing, a horizontal end plate, an outer side vertical end plate, an outer side flap, a middle vertical end plate, an inner side flap and an inner side vertical end plate; the outer side wing flap comprises a wing flap horizontal section, a wing flap bending section and a wing flap vertical section which are sequentially connected, the wing flap horizontal section is fixedly connected with the middle vertical end plate, the wing flap vertical section is fixedly connected with the horizontal end plate, and an included angle between the wing flap horizontal section and the wing flap vertical section is 90 degrees; and the outer side flap is twisted at the flap bending section, so that an included angle alpha between a connecting line between the leading edge and the trailing edge of the outer side flap and an xy plane is different from an included angle beta between the connecting line between the leading edge and the trailing edge of the outer side flap and an xz plane. The front wing has the advantages of simple structure, high reliability, low cost, easy manufacture and good popularization value. Meanwhile, the special structure of the outboard flap can reduce the resistance caused by the tire flow.)

1. The utility model provides an equation motorcycle race improves front wing structure of front wheel streaming, its rigid coupling is at the automobile body and is located the front side of racing front wheel, its characterized in that: the front wing structure comprises a main wing, a horizontal end plate, an outer side vertical end plate, an outer side flap, a middle vertical end plate, an inner side flap and an inner side vertical end plate;

the end part of the main wing is fixedly connected with the horizontal end plate, the outer side vertical end plate is fixedly connected with the horizontal end plate and is vertically arranged with the horizontal end plate, the two ends of the outer side flap are fixedly connected with the horizontal end plate and the middle vertical end plate respectively, the two ends of the inner side flap are fixedly connected with the middle vertical end plate and the inner side vertical end plate respectively, and the inner side vertical end plate is fixedly connected with the vehicle body;

the outer side wing flap comprises a wing flap horizontal section, a wing flap bending section and a wing flap vertical section which are sequentially connected, the wing flap horizontal section is fixedly connected with the middle vertical end plate, the wing flap vertical section is fixedly connected with the horizontal end plate, and an included angle between the wing flap horizontal section and the wing flap vertical section is 90 degrees; and the outer side flap is twisted at the flap bending section, so that an included angle alpha between a connecting line between the leading edge and the trailing edge of the outer side flap and an xy plane is different from an included angle beta between the connecting line between the leading edge and the trailing edge of the outer side flap and an xz plane.

2. The front wing structure of formula car for improving the flow around the front wheel of claim 1, wherein: the difference between the included angle beta between the connecting line between the leading edge and the trailing edge of the outer flap and the xz plane and the included angle m between the airflow direction and the xz plane is less than 3-7 degrees.

3. The front wing structure of formula car for improving the flow around the front wheel of claim 2, wherein: the difference between the included angle beta between the connecting line between the leading edge and the trailing edge of the outboard flap and the xz plane and the included angle m between the airflow direction and the xz plane is less than 5 degrees.

4. The front wing structure of formula car for improving the flow around the front wheel of claim 1, wherein: the bending radius r of the bending section of the flap is larger than the chord length l of the outboard flap.

5. The front wing structure of formula car for improving the flow around the front wheel of claim 1, wherein: the ratio of the maximum airfoil thickness b of the outboard flap to the chord length l of the outboard flap is less than 10% -15%.

6. The front wing structure of formula car for improving the flow around the front wheel of claim 5, wherein: the ratio of the maximum profile thickness b of the outboard flap to the chord length l of the outboard flap is less than 13%.

7. The front wing structure of formula car for improving the flow around the front wheel of claim 1, wherein: the chord length l of the outboard flap is less than 40-60% of the chord length of the main wing.

8. The front wing structure of formula car of claim 7 for improving the flow around the front wheel, wherein: the chord length l of the outboard flap is less than 50% of the chord length of the main wing.

9. The front wing structure of formula car for improving the flow around the front wheel of claim 1, wherein: the length of the vertical section of the flap is equal to the length of the chord length l of the outboard flap.

10. The front wing structure of formula car for improving the flow around the front wheel of claim 1, wherein: the outside flap is made of resin or nylon materials through 3D printing, the inside of the outside flap is hollow, and the volume of the hollow part of the outside flap is less than or equal to 60% of the volume of the outside flap.

Technical Field

The invention relates to a front wing structure for improving the flow around a front wheel of an equation car.

Background

The race sport originated in 1894 and is a game project of the skill level of the tester and the designer of the race. With the goal of pursuing speed, racing designers have invented racing aerodynamic kits. The aerodynamic effect who produces makes the cycle racing possess the holding down force, and the holding down force that its produced has increased the adhesive force of tire and road surface for the cycle racing is faster in the bend, and brake distance is shorter, accelerates more stably.

The front wing is the main part of the racing car aerodynamic suite, and can generate downward pressure at the front part of the racing car, so that the control effects of reducing steering insufficiency and optimizing steering are achieved. The downward pressure generated by the front wing accounts for 30-50% of the downward pressure of the whole vehicle.

In recent years, front wing designs have become more advanced and mature due to the technological development of computational fluid dynamics. The front wing can generate more downward pressure. The front wing is more utilizing to the air flow and has more negative effect. Since the front wing is mounted at the front of the racing car, the front wing consumes the energy of the airflow, and the airflow can generate turbulence after leaving the front wing, which can have negative effect on the action effect of the aerodynamic feature elements downstream in the airflow direction. Therefore, racing car designers hope that the front wing can reduce negative effects while bringing higher down pressure, and more positive effects are generated, so that the aerodynamic effect of the whole car is optimized, and the controllability of the racing car is improved.

Due to regulatory constraints, the formula car must be an open-tire car and the tire will constantly disturb the air flow during rotation, which is called tire flow. Also, the flow of air over the tire becomes very turbulent due to the rough surface of the tire, so that the tire flow is extremely detrimental to the aerodynamic effect of the racing car. However, due to the regulation, the generation of the tire circumferential flow cannot be reduced by surrounding the tire, and the influence of the tire circumferential flow needs to be solved from other directions.

Disclosure of Invention

The invention provides a front wing structure for improving the circumfluence of a front wheel of an equation car, which overcomes the defects of the prior art. The technical scheme adopted by the invention for solving the technical problems is as follows:

a front wing structure for improving the streaming of a front wheel of an equation racing car is fixedly connected to a car body and positioned on the front side of the front wheel of the racing car, and comprises a main wing, a horizontal end plate, an outer side vertical end plate, an outer side flap, a middle vertical end plate, an inner side flap and an inner side vertical end plate;

the end part of the main wing is fixedly connected with the horizontal end plate, the outer side vertical end plate is fixedly connected with the horizontal end plate and is vertically arranged with the horizontal end plate, the two ends of the outer side flap are fixedly connected with the horizontal end plate and the middle vertical end plate respectively, the two ends of the inner side flap are fixedly connected with the middle vertical end plate and the inner side vertical end plate respectively, and the inner side vertical end plate is fixedly connected with the vehicle body;

the outer side wing flap comprises a wing flap horizontal section, a wing flap bending section and a wing flap vertical section which are sequentially connected, the wing flap horizontal section is fixedly connected with the middle vertical end plate, the wing flap vertical section is fixedly connected with the horizontal end plate, and an included angle between the wing flap horizontal section and the wing flap vertical section is 90 degrees; and the outer side flap is twisted at the flap bending section, so that an included angle alpha between a connecting line between the leading edge and the trailing edge of the outer side flap and an xy plane is different from an included angle beta between the connecting line between the leading edge and the trailing edge of the outer side flap and an xz plane.

In a preferred embodiment: the difference between the included angle beta between the connecting line between the leading edge and the trailing edge of the outer flap and the xz plane and the included angle m between the airflow direction and the xz plane is less than 3-7 degrees.

In a preferred embodiment: the difference between the included angle beta between the connecting line between the leading edge and the trailing edge of the outboard flap and the xz plane and the included angle m between the airflow direction and the xz plane is less than 5 degrees.

In a preferred embodiment: the bending radius r of the bending section of the flap is larger than the chord length l of the outboard flap.

In a preferred embodiment: the ratio of the maximum airfoil thickness b of the outboard flap to the chord length l of the outboard flap is less than 10% -15%.

In a preferred embodiment: the ratio of the maximum profile thickness b of the outboard flap to the chord length l of the outboard flap is less than 13%.

In a preferred embodiment: the chord length l of the outboard flap is less than 40-60% of the chord length of the main wing.

In a preferred embodiment: the chord length l of the outboard flap is less than 50% of the chord length of the main wing.

In a preferred embodiment: the length of the vertical section of the flap is equal to the length of the chord length l of the outboard flap.

In a preferred embodiment: the outside flap is made of resin or nylon materials through 3D printing, the inside of the outside flap is hollow, and the volume of the hollow part of the outside flap is less than or equal to 60% of the volume of the outside flap.

Compared with the background technology, the technical scheme has the following advantages:

1. the front wing has the advantages of simple structure, high reliability, low cost, easy manufacture and good popularization value. Meanwhile, the special structure of the outboard flap can reduce the resistance caused by the tire flow, increase the downforce of the front wing and reduce the downforce loss caused by the tire flow.

2. The difference between the angle beta between the line between the leading edge and the trailing edge of the outboard flap and the xz plane and the angle m between the airflow direction and the xz plane is less than 3-7 degrees, so that the airflows on the xz plane are not separated.

3. The bending radius r of the bending section of the flap is larger than the chord length l of the outboard flap, so that the lower wing surface of the outboard flap is smoother without generating corners.

4. The ratio of the maximum airfoil thickness b of the outboard flap to the chord length l of the outboard flap is less than 10% -15%, so that the airflow near the outboard flap is not easy to separate.

5. The chord length l of the outboard flap is less than 40% -60% of the chord length of the main wing, and airflow near the outboard flap is not easy to separate.

6. The length of the vertical section of the flap is equal to the length of the chord length l of the outboard flap, so that the outboard flap can exert the effect of guiding airflow on the xy plane after being bent.

7. The volume of the hollow part of the outer flap is less than or equal to 60% of the volume of the outer flap, so that the weight of the outer flap can be reduced and the sufficient strength of the outer flap can be ensured.

Drawings

The invention is further illustrated by the following figures and examples.

Fig. 1 is a schematic view illustrating an assembly of the front wing structure and a vehicle body.

Fig. 2 shows a schematic side view of the front wing structure.

Fig. 3 is a schematic perspective view of the front wing structure.

Fig. 4 shows a schematic structure of the front wing structure with the inboard flap and the inboard vertical end plate removed.

FIG. 5 shows an assembly schematic of a horizontal end plate, outboard flap, outboard vertical end plate.

FIG. 6 shows a schematic side view of the outboard flap in the yz direction.

FIG. 7 is a schematic side view of the front wing structure in the xz direction.

Fig. 8 shows an enlarged view of fig. 7 at section i.

Fig. 9 is a schematic top view of the front wing structure in the xy direction.

Fig. 10 shows an enlarged schematic view of fig. 9 at section ii.

FIG. 11 is a schematic view showing the effect of the outboard flap on the air flow at the front wheel of a racing car.

FIG. 12 is a schematic diagram showing the effect of a prior art racing flap on the airflow of the front wheels of a racing car.

Detailed Description

In the claims, the specification and the drawings of the present invention, unless otherwise expressly limited, the terms "first", "second" or "third", etc. are used for distinguishing between different items and not for describing a particular sequence.

In the claims, the specification and the drawings of the present invention, unless otherwise expressly limited, all directional or positional relationships indicated by the terms "center," "lateral," "longitudinal," "horizontal," "vertical," "top," "bottom," "inner," "outer," "upper," "lower," "front," "rear," "left," "right," "clockwise," "counterclockwise," and the like are based on the directional or positional relationships indicated in the drawings and are used for convenience in describing the present invention and for simplicity in description, but do not indicate or imply that the device or element so indicated must have a particular orientation or be constructed and operated in a particular orientation, and therefore should not be construed as limiting the scope of the present invention.

In the claims, the description and the drawings of the present application, unless otherwise expressly limited, the terms "fixedly connected" and "fixedly connected" should be interpreted broadly, that is, any connection between the two that is not in a relative rotational or translational relationship, that is, non-detachably fixed, integrally connected, and fixedly connected by other devices or elements.

In the claims, the specification and the drawings of the present invention, the terms "including", "having", and variations thereof, are intended to be inclusive and not limiting.

Referring to fig. 1 to 12, a preferred embodiment of a front wing structure of an equation type racing car for improving the flow around the front wheel is fixed on the car body 1 and located at the front side of the front wheel 2 of the racing car.

The front wing structure comprises a main wing 10, a horizontal end plate 20, an outboard vertical end plate 30, an outboard flap 40, a middle vertical end plate 50, an inboard flap 60 and an inboard vertical end plate 70.

The main wing 10 is long and is arranged obliquely. The end of the main wing 10 is fixedly connected with the horizontal end plate 20, the outer vertical end plate 30 is fixedly connected with the horizontal end plate 20 and is arranged perpendicular to the horizontal end plate 20, the two ends of the outer flap 40 are fixedly connected with the horizontal end plate 20 and the middle vertical end plate 50 respectively, the two ends of the inner flap 60 are fixedly connected with the middle vertical end plate 50 and the inner vertical end plate 70 respectively, and the inner vertical end plate 70 is fixedly connected with the vehicle body 1.

In this embodiment, the left and right ends of the main wing 10 are symmetrically arranged, that is, the left and right ends of the main wing 10 are both fixedly connected to a horizontal end plate 20; the left horizontal end plate 20 and the right horizontal end plate 20 are fixedly connected with an outer vertical end plate 30 respectively, the left outer vertical end plate 30 and the right outer vertical end plate 30 are fixedly connected with an outer flap 40 respectively, the left outer flap 40 and the right outer flap 40 are fixedly connected with a middle vertical end plate 50 respectively, the left middle vertical end plate 50 and the right middle vertical end plate 50 are fixedly connected with an inner flap 60 respectively, the left inner flap 60 and the right inner flap 60 are fixedly connected with an inner vertical end plate 70 respectively, the two inner vertical end plates 70 are arranged oppositely, and U-shaped lugs 71 are arranged on opposite surfaces of the left middle vertical end plate 50 and the right middle vertical end plate 50 respectively, and the U-shaped lugs 71 are used for being connected with the automobile body 1. As shown in fig. 2, two U-shaped lugs 71 spaced up and down are disposed on the inner side of each inner vertical end plate 70, and the U-shaped lugs 71 are connected with the vehicle body by welding, so that the connection between the U-shaped lugs 71 and the vehicle body is firmer.

Specifically, as shown in fig. 5, the horizontal end plate 20 includes a vertical end plate portion 21, a horizontal end plate portion 22, and an arc-shaped end plate portion 23, which are connected in this order.

The bottom end of the outer vertical end plate 30 is provided with a first lug 31, and the first lug 31 is locked with the horizontal end plate 22 by a first bolt, so that the outer vertical end plate 30 and the horizontal end plate 22 are vertically arranged. As shown in fig. 3, the outer side of the outer vertical end plate 30 is further provided with an end plate wing 80, which can enhance the washing effect of the air flow. The end plate wings 80 are generally arc-shaped, and have a thickness that gradually decreases from the front end to the rear end, and are arranged obliquely.

As shown in FIG. 4, the y-axis is defined along the length of the main wing 10, the x-axis is defined for you by laying down the width of the main wing 10, and the z-axis is defined along the height of the outboard vertical end plate 30.

As shown in fig. 6, the outboard flap 40 includes a flap horizontal section 41, a flap bending section 42, and a flap vertical section 43 connected in series. In this embodiment, two outboard flaps 40 are provided on the left side and two outboard flaps 40 are provided on the right side, and are spaced apart from each other in the fore-and-aft direction.

In this embodiment, as shown in fig. 5, the flap horizontal section 41 is fixedly connected to the middle vertical end plate 50, the flap vertical section 43 is fixedly connected to the horizontal end plate 20, and an included angle k between the flap horizontal section 41 and the flap vertical section 43 is 90 degrees; moreover, the outboard flap 40 is twisted at the flap bending section 42, so that an included angle α between a connecting line between the leading edge and the trailing edge of the outboard flap 40 and an xy plane is different from an included angle β between a connecting line between the leading edge and the trailing edge of the outboard flap 40 and an xz plane. Therefore, the phenomenon that the airflow is separated in the xy plane and the xz plane can be avoided, and the effect is maximized.

In this embodiment, the length of the flap vertical section 43 is equal to the length of the chord length l of the outboard flap 40, so that the outboard flap 40 can exert a sufficient airflow guiding effect on the xy-plane after being bent.

In this embodiment, the bending radius r of the flap bending section 42 is larger than the chord length l of the outboard flap 40.

In the present embodiment, as shown in fig. 8, the ratio of the maximum airfoil thickness b of the outboard flap 40 to the chord length l of the outboard flap 40 is less than 10% -15%. Preferably, the ratio of the maximum airfoil thickness b of the outboard flap 40 to the chord length l of the outboard flap 40 is less than 13%, so that the flow near the outboard flap 40 is not easily separated. If necessary, the ratio of the maximum airfoil thickness b of the outboard flap 40 to the chord length l of the outboard flap 40 may also be less than 10%, or may also be less than 15%, which is not limited thereto.

In this embodiment, the chord length l of the outboard flap 40 is less than 40% -60% of the chord length of the main wing. Preferably, the chord length l of the outboard flap 40 is less than 50% of the chord length of the main wing, which also makes it difficult for the flow near the outboard flap 40 to separate.

In this embodiment, the outboard flap 40 is made of resin or nylon material by 3D printing, and the inside thereof is hollow, and the volume of the hollow portion thereof is equal to or less than 60% of the volume of the outboard flap 40. With the resin, a smoother surface can be achieved; nylon is adopted, so that the strength can be higher; at the same time, a hollow arrangement of 60% ensures sufficient strength while reducing the weight of the outboard flap 40.

In the present embodiment, as shown in FIG. 10, the difference between the angle β between the line connecting the leading edge and the trailing edge of the outboard flap 40 and the xz plane and the angle m between the airflow direction and the xz plane is less than 3-7 °. Preferably, the angle β between the line between the leading and trailing edges of the outboard flap 40 and the xz-plane differs by less than 5 ° from the angle m between the direction of airflow and the xz-plane, so that no separation of the airflow in the xz-plane occurs.

As shown in fig. 5, the bottom end of the vertical flap 43 is provided with a second tab 44, and the second tab 44 and the vertical flap 43 are fixed by welding in actual assembly; a second bolt is further provided, and the second bolt passes through the second lug 44 and is locked to the horizontal end plate portion 22 of the horizontal end plate 20. The left end of the flap horizontal section 41 is welded with a third lug 45, and a third bolt is additionally arranged, passes through the third lug 45 and is locked on the middle vertical end plate 50 through the third bolt, so that the outer flap 40 and the middle vertical end plate 50 are fixed. Similarly, the inboard flap 60 is also secured at both ends to the intermediate vertical end plate 50 and the inboard vertical end plate 70, respectively, in this manner. And, as shown in FIG. 2, the inboard flap 60 is straight; and the number of the left inner side flap 60 and the right inner side flap 60 is two and the two flaps are arranged at intervals. The top end of the middle vertical end plate 50 is square, and the bottom end thereof is triangular. The inboard vertical end plate 70 is generally the same shape as the intermediate vertical end plate 50 and is spaced apart in parallel. The outboard flap rear end is directly opposite the racing front wheel 2 as seen in fig. 1.

The inboard flap 60 and inboard vertical end plate 70 are arranged to further increase the downforce of the front wing. The middle vertical end plate 50 separates the inboard flap 60 from the outboard flap 40, i.e., it interrupts the flow of the outboard flap 40 from the inboard flap 60, preventing the flow near the body from being disturbed by the wash-out flow outside the front wing.

As shown in fig. 11, when the airflow passes through the outboard flap 40, since the outboard flap 40 has a characteristic of changing the direction of the airflow, the airflow will flow toward the outboard side of the front wing in the direction of the deflection of the airfoil, the airflow flowing toward the outboard side of the front wing bypasses the tire, the air pressure in front of the tire is reduced, and the airflow disturbed by the tire is reduced. Meanwhile, the part of airflow has larger energy, can bring the turbulent flow generated by the rotation of the tire away, reduces the front-back pressure difference of the tire, effectively reduces the resistance of the tire and the lifting force caused by the rotation of the tire, optimizes the air flow of the whole vehicle, and improves the aerodynamic effect of the whole vehicle. As shown in fig. 12, the conventional front wing flap structure is adopted, and airflow passes through the flap and then adheres to the end surface of the tire, so that the air pressure in front of the tire is increased, and the airflow disturbed by the tire is increased.

The front wing has the advantages of simple structure, high reliability, low cost, easy manufacture and good popularization value. Meanwhile, the special structure of the outboard flap 40 can reduce the drag caused by the tire bypass, and can increase the downforce of the front wing and reduce the downforce loss caused by the tire bypass.

The above description is only a preferred embodiment of the present invention, and therefore should not be taken as limiting the scope of the invention, which is defined by the appended claims and their equivalents.