CN216659477U - Top cover structure and flying car - Google Patents

Abstract

The application relates to a top cap structure and hovercar. The top cover structure comprises a plurality of beam bodies and a plurality of columns which are integrally formed; the beam bodies comprise horn mounting beams and top cover mounting beams connected with the horn mounting beams, a plurality of columns are arranged at the bottoms of the top cover mounting beams, and the columns are used for being connected with the body of a flying automobile; the both ends of horn installation roof beam are equipped with the horn installation department, the horn installation roof beam with be formed with the cavity region that is used for installing windshield part between the top cap installation roof beam. The scheme that this application provided can simplify the structure and the connection of each part, and can weight reduction, satisfies hovercar's lightweight demand.

Description

Top cover structure and flying car

Technical Field

The application relates to the technical field of vehicles, in particular to a top cover structure and a flying automobile.

Background

The automobile roof is a cover plate of the top of an automobile compartment, is a key part for forming a cab, and is an important part related to the safety of a driver and passengers.

In the related art, the roof of the flying car is generally used as the roof of the ordinary car. The top cover of the common automobile is formed by welding, bonding or bolting a plurality of parts, needs to be connected into smaller assemblies through the parts, is connected into a larger assembly through each smaller assembly, and is assembled to the larger assembly to realize assembly.

SUMMERY OF THE UTILITY MODEL

For solving or partly solving the problem that exists among the correlation technique, this application provides a top cap structure and hovercar, and this top cap structure can simplify the structure and the connection of each part, and can lighten weight, satisfies hovercar's lightweight demand.

The present application provides in a first aspect a roof structure comprising:

a plurality of beam bodies and a plurality of columns which are integrally formed;

the beam bodies comprise horn mounting beams and top cover mounting beams connected with the horn mounting beams, a plurality of columns are arranged at the bottoms of the top cover mounting beams, and the columns are used for being connected with the body of a flying automobile;

the both ends of horn installation roof beam are equipped with the horn installation department, the horn installation roof beam with be formed with the cavity region that is used for installing windshield part between the top cap installation roof beam.

In an implementation mode, the robot arm installation beam further comprises edge beams connected between the two ends of the robot arm installation beam and the top cover installation beam, the robot arm installation beam is arranged above the top cover installation beam, and the edge beams are connected between the robot arm installation beam and the top cover installation beam in an inclined mode.

In one embodiment, the top cover mounting beam comprises a front beam, a rear beam, a left beam and a right beam, the front beam, the rear beam, the left beam and the right beam enclose a frame, the horn mounting beam is connected to the front beam, and the four corners of the frame are respectively provided with the cylinders;

and the front cross beam, the rear cross beam, the left cross beam and the right cross beam are used for arranging cover plates in the area enclosed by the front cross beam, the rear cross beam, the left cross beam and the right cross beam.

In one embodiment, the horn mounting beam is provided as a hollowed structure.

In one embodiment, the horn installation beam is provided with a first reinforcing structure, the first reinforcing structure comprises a plurality of first reinforcing ribs arranged at intervals along the length direction of the horn installation beam, and the first reinforcing ribs are vertically supported on the upper side and the lower side of the horn installation beam.

In one embodiment, the columns include two first columns disposed proximate to a front portion of the vehicle body, two second columns disposed proximate to a rear portion of the vehicle body;

the first cylinder is arranged corresponding to the left side and the right side of the front portion of the vehicle body, and the second cylinder is arranged corresponding to the left side and the right side of the rear portion of the vehicle body.

In one embodiment, the roof mounting rail is provided with an attachment tab for attachment to the body of the flying automobile on a side thereof adjacent the rear portion of the body.

In one embodiment, the top cover mounting beam is provided with a second reinforcing structure, and the second reinforcing structure comprises a plurality of second reinforcing ribs arranged at intervals along the length direction of the front cross beam, the rear cross beam, the left cross beam and the right cross beam; and/or the presence of a gas in the gas,

the cylinder is provided with a third reinforcing structure, and the third reinforcing structure comprises a plurality of third reinforcing ribs arranged at intervals along the length direction of the first cylinder and/or the second cylinder.

In one embodiment, a fourth reinforcing structure is provided around the hollow area for mounting the windshield component;

the fourth reinforcing structure comprises a plurality of fourth reinforcing ribs; the fourth reinforcing ribs are arranged between the horn mounting beam and the edge beam; and/or a plurality of fourth reinforcing ribs are arranged between the edge beam and the first column body.

The present application provides in a second aspect a flying automobile comprising: a roof construction as described above.

The technical scheme provided by the application can comprise the following beneficial effects: the roof structure provided by the application comprises a plurality of beam bodies and a plurality of columns which are integrally formed; the beam bodies comprise horn mounting beams and top cover mounting beams connected with the horn mounting beams, a plurality of columns are arranged at the bottoms of the top cover mounting beams, and the columns are used for being connected with the body of a flying automobile; the both ends of horn installation roof beam are equipped with the horn installation department, the horn installation roof beam with be formed with the cavity region that is used for installing windshield part between the top cap installation roof beam. The beam bodies and the columns are integrally formed, and all parts of the top cover structure are not required to be connected through connecting parts, so that the number of parts of the top cover structure can be reduced, the structure and connection of all parts are simplified, and the weight of the top cover structure is reduced; and set up the cavity region between top cap installation roof beam and horn installation roof beam, be favorable to installing the windscreen part, also can reduce the weight of top cap structure through the fretwork design to be favorable to realizing hovercar's lightweight.

It is to be understood that both the foregoing general description and the following detailed description are exemplary and explanatory only and are not restrictive of the application.

Drawings

The foregoing and other objects, features and advantages of the application will be apparent from the following more particular descriptions of exemplary embodiments of the application as illustrated in the accompanying drawings wherein like reference numbers generally represent like parts throughout the exemplary embodiments of the application.

FIG. 1 is a schematic structural diagram of a top cover structure shown in an embodiment of the present application;

FIG. 2 is a schematic top view of a top cover structure according to an embodiment of the present disclosure;

FIG. 3 is a schematic structural view of the top cover structure shown in FIG. 2, taken in cross-section at A-A;

FIG. 4 is a schematic structural view of the top cover structure shown in FIG. 2, taken in cross-section at B-B;

fig. 5 is an assembly structure diagram of a reinforcing structure of a top cover structure according to an embodiment of the present application.

Reference numerals: a beam body 10; a hollow region 100; a horn-mounting beam 11; a horn attachment portion 111; a hollowed-out area 112; a roof mounting rail 12; a front cross member 121; a rear cross member 122; a left cross member 123; a right cross member 124; the edge beam 13; a cover plate 14; a connection joint 15; a column 20; a first cylinder 21; a second cylinder 22; a first reinforcing structure 31; a second reinforcing structure 32; a third reinforcing structure 33; a fourth reinforcing structure 34.

Detailed Description

Embodiments of the present application will be described in more detail below with reference to the accompanying drawings. While embodiments of the present application are illustrated in the accompanying drawings, it should be understood that the present application may be embodied in various forms and should not be limited to the embodiments set forth herein. Rather, these embodiments are provided so that this disclosure will be thorough and complete, and will fully convey the scope of the disclosure to those skilled in the art.

The terminology used herein is for the purpose of describing particular embodiments only and is not intended to be limiting of the application. As used in this application and the appended claims, the singular forms "a", "an", and "the" are intended to include the plural forms as well, unless the context clearly indicates otherwise. It should also be understood that the term "and/or" as used herein refers to and encompasses any and all possible combinations of one or more of the associated listed items.

It should be understood that although the terms "first," "second," "third," etc. may be used herein to describe various information, these information should not be limited to these terms. These terms are only used to distinguish one type of information from another. For example, first information may also be referred to as second information, and similarly, second information may also be referred to as first information, without departing from the scope of the present application. Thus, a feature defined as "first" or "second" may explicitly or implicitly include one or more of that feature. In the description of the present application, "a plurality" means two or more unless specifically limited otherwise.

In the related art, the roof of the flying car is generally used as the roof of the ordinary car. The top cover of the common automobile is formed by welding, bonding or bolting a plurality of parts, needs to be connected into smaller assemblies through the parts, is connected into a larger assembly through each smaller assembly, and is assembled to the larger assembly to realize assembly.

The technical solutions of the embodiments of the present application are described in detail below with reference to the accompanying drawings.

Referring to fig. 1, the present embodiment provides a roof structure including a plurality of beams 10 and a plurality of columns 20 formed as one body; the plurality of beam bodies 10 comprise horn mounting beams 11 and top cover mounting beams 12 connected with the horn mounting beams 11, a plurality of columns 20 are arranged at the bottoms of the top cover mounting beams 12, and the columns 20 are used for being connected with the body of a flying automobile; the arm mounting beam 11 has arm mounting portions 111 at both ends thereof, and a hollow area 100 for mounting a windshield member is formed between the arm mounting beam 11 and the roof mounting beam 12.

The plurality of beams 10 may include beams extending in a front-rear direction of the hovercar, such as longitudinal beams, and beams extending in a left-right direction of the hovercar, such as transverse beams, and the plurality of columns 20 are connected to different portions of the plurality of beams 10, and may form at least parts of a column a and a column B of the hovercar, and the plurality of beams 10 and the plurality of columns 20 constitute a main structure of the top of the hovercar.

In this embodiment, the plurality of beams 10 and the plurality of columns 20 are integrally formed, so that the condition that the plurality of beams and the plurality of columns are integrally assembled by using connecting parts, such as bolts and buckles, in the related art is avoided, and therefore, the number of parts of the top cover structure can be reduced, the structural strength is increased, the weight can be reduced, and the lightweight of the hovercar is facilitated.

In this embodiment, the horn installation beams 11 are disposed along the left and right direction of the hovercar, and both ends thereof are located at the left and right sides of the hovercar, wherein the left and right direction of the hovercar is the Y direction in fig. 1 of this embodiment, and the front and rear direction of the body of the hovercar is the X direction of this embodiment; the vehicle body vertical direction of the hovercar is the Z direction of the present embodiment. The horn mounting portions 111 may be provided at both sides of the horn mounting beam 11 for connection with a horn of a flying car. The horn installation beam 11 is provided on the roof installation beam on the side near the front part of the vehicle body, and a plurality of columns 20 are provided on the lower side of the roof installation beam for constituting at least parts of the a-column and the B-column of the hovercar. For example, a plurality of columns may form the upper sections of the A and B columns for connection to the lower sections of the A and B columns of the body arrangement to secure the roof structure to the body of the hovercar.

In the present exemplary embodiment, the roof mounting bar 12 is arranged at a distance from the arm mounting bar 11 in the longitudinal direction X and in the vertical direction Z of the flying vehicle, so as to form a hollow area 100 corresponding to the longitudinal direction of the flying vehicle, which hollow area 100 is used, on the one hand, for mounting a windshield component, which may be, for example, a windshield of the flying vehicle. On the other hand can reduce the weight of top cap structure through fretwork design to be favorable to realizing hovercar's lightweight.

This embodiment is through establishing a plurality of roof beam bodies 10 and a plurality of cylinder 20 into integrated into one piece, has simplified the connection form of roof structure and hovercar's automobile body side wall, can promote roof structure and hovercar's integration degree, and when hovercar's rotor passed through the horn and transmitted moment to hovercar's automobile body, the transmission efficiency of moment was higher, has not only promoted hovercar's structural strength, has strengthened hovercar's operating stability moreover.

In one of them embodiment, the roof structure can be by carbon fiber material integrated into one piece, and it is better to use carbon fiber material integrated into one piece part structural strength, can further reduce the weight of roof structure moreover, satisfies hovercar's lightweight demand.

In one embodiment, the roof structure may be further integrally formed by an aluminum alloy material, for example, integrally formed and cast by a high-pressure vacuum die casting process, so that the plurality of beams 10 and the plurality of columns 20 form an integral structure, and the overall material thickness may be distributed within a predetermined size interval according to the strength and functional requirements of the roof structure, for example, the predetermined size interval may be 3mm to 10mm, thereby realizing integration of a plurality of parts into one integral part, achieving a weight reduction effect on the premise of meeting the strength and safety performance, and achieving a weight reduction effect of 25% compared with the roof of the related art, which has an obvious weight reduction effect.

In one embodiment, the roof structure further includes an edge beam 13 connected between two ends of the horn installation beam 11 and the roof installation beam 12, the horn installation beam 11 is disposed above the roof installation beam 12, and the edge beam 13 is connected between the horn installation beam 11 and the roof installation beam 12 in an oblique direction, for example, between the horn installation beam 11 and the roof installation beam 12 in the front-back direction X and the up-down direction Z of the hovercar.

In one implementation, the edge beam 13 is integrally formed with the horn mounting beam 11 and the cap mounting beam 12. Here, a plurality of, for example, two edge beams 13 may be provided, and are respectively provided at both ends of the arm mounting beam 11. The horn mounting beam 11 is connected to the roof mounting beam 12 by two boundary beams 13, which together define a hollow area 100 formed between the horn mounting beam 11 and the roof mounting beam 12, it being understood that the distance between the horn mounting beam 11 and the roof mounting beam 12 may be set according to the length of the boundary beams 13. For easy understanding, referring to fig. 1, the horn-mounting beam 11 is disposed above the Z-direction of the top cover-mounting beam 12, the beam body 10 of the horn-mounting beam 11 extends in the Y-direction, one end of the side beam 13 is connected to both sides of the horn-mounting beam 11 in the Y-direction, and extends obliquely from the horn-mounting beam 11 to the top cover-mounting beam 12 at an angle to the X-direction and the Z-direction. Since the side beams 13 on both sides have a space in the Y direction, the horn installation beam 11 and the roof installation beam 12 have a space in the X direction, thereby forming a hollow area 100.

Referring to fig. 2, in one embodiment, the roof mounting beam 12 includes a front beam 121, a rear beam 122, a left beam 123 and a right beam 124, the front beam 121, the rear beam 122, the left beam 123 and the right beam 124 enclose a frame, and the frame may be rectangular. The horn installation beam 11 is connected to the front cross beam 121, and the four corners of the frame body are respectively provided with a column 20; the front cross member 121, the rear cross member 122, the left cross member 123 and the right cross member 124 are used for arranging the cover plate 14 in a region enclosed by the two cross members.

Wherein, front beam 121 and rear beam 122 can extend the setting along the Y direction, and left crossbeam 123 and right crossbeam 124 can extend the setting along the X direction, and front beam 121 and rear beam 122 are connected respectively at left crossbeam 123 and right crossbeam 124 both ends to enclose and close and injecing the framework, apron 14 can set up in the middle part of framework, and four sides of apron 14 are connected with front beam 121, rear beam 122, left crossbeam 123 and right crossbeam 124 respectively. The front cross member 121, the rear cross member 122, the left cross member 123, and the right cross member 124 may be formed integrally, and the front cross member 121, the arm mounting member 11, the cover plate 14, and the frame may be formed integrally.

In the present embodiment, the frame body formed by enclosing the front cross member 121, the rear cross member 122, the left cross member 123, and the right cross member 124 is provided, so that the cover plate 14 can be provided through the frame body, and when the roof structure is coupled to the body of the hovercar, the cover plate 14 can be fitted to the hovercar.

Referring to fig. 1 and 4, in one embodiment, the horn installation beam 11 is a hollow structure.

Wherein, hollow out construction can include a plurality of hollow out regions 112, and hollow out region 112 can be seted up in horn installation roof beam 11 along the X direction, can include recess or shrinkage pool etc. through setting up horn installation roof beam 11 into hollow out construction, can alleviate the weight of horn installation roof beam 11, is favorable to realizing hovercar's lightweight.

Wherein, because the horn installation department 111 of horn installation roof beam 11 needs the installation horn, horn installation department 111 includes the platelike structure as an organic whole with horn installation roof beam 11 shaping, platelike structure has preset thickness in flying automobile's fore-and-aft direction X, for guaranteeing installation performance and flight performance, can establish the platelike structure's of horn installation department 111 thickness to be greater than 10mm, it is corresponding, because horn installation roof beam 11 needs load horn installation department 111, the material thickness of its roof beam body in the X direction can be established to be greater than 5mm to improve structural strength.

It is to be understood that the above dimensions are merely exemplary, and the present application does not specifically limit the thickness of the plate-like structure of the horn attachment section 111.

The horn installation beam 11 may be an i-beam, and is "i" shaped in the Y direction, for example, the "i" shaped beam may have two transverse plates extending in the Y direction, and both sides of the transverse plates have a predetermined width dimension in the X direction, and one vertical plate extending in the Y direction, and having a predetermined height dimension in the Z direction, and the upper and lower ends of the vertical plate in the Z direction are respectively connected to the transverse plates to form an i-beam, so that the horn installation beam 11 forms a plurality of through regions which are spaced apart from each other and are through in the X direction, thereby forming a hollow structure. In other embodiments, the horn-mounting beam 11 may also be configured as a U-beam. The size and shape of the horn-mounting beam 11 are exemplified above, but not specifically limited thereto.

Referring to fig. 4, in order to improve the structural strength of the horn installation beam 11, in one embodiment, the horn installation beam 11 is provided with a first reinforcing structure 31, and the first reinforcing structure 31 includes a plurality of first reinforcing ribs arranged at intervals along the length direction of the horn installation beam 11, and the first reinforcing ribs are supported between two transverse plates on the upper and lower sides of the horn installation beam 11 along the vertical direction Z.

This embodiment sets up the first additional strengthening 31 that has first strengthening rib on horn installation roof beam 11, and first strengthening rib is along vertical, and the Z direction supports between the horizontal board of the upper and lower both sides of horn installation roof beam 11 promptly, can improve the structural strength of horn installation roof beam 11, compares in prior art, and horn installation roof beam 11 establishes to hollow out construction and sets up first additional strengthening 31 after, when guaranteeing structural strength, has still satisfied the lightweight demand. In one embodiment, the first reinforcing rib may have a size in the Y direction and the Z direction smaller than a preset size, for example, 190mm × 100mm, and a preset thickness in the X direction, for example, 3mm to 5mm, and may be, for example, a square rib structure with a side length of 5mm, where the square rib structure is uniformly arranged on the inner sides of the two transverse plates of the horn installation beam 11 to reinforce the two transverse plates.

Referring to fig. 1, in one embodiment, the column 20 includes two first columns 21 disposed near the front of the vehicle body, two second columns 22 disposed near the rear of the vehicle body; two first columns 21 are provided corresponding to left and right sides of a front portion of the vehicle body, and two second columns 22 are provided corresponding to left and right sides of a rear portion of the vehicle body. The first column may be at least part of an a-column and the second column may be at least part of a B-column. The column A is a connecting column for connecting the roof and the front cabin on the front left and the front right, and the column B is a connecting column for connecting the rear left and the rear right between the front seat and the rear seat of the cockpit.

In the present embodiment, the first column 21 and the second column 22 are disposed on two sides of the bottom of the roof mounting beam 12 in the X direction, so that the two first columns 21 and the two second columns 22 are respectively coupled with the body of the hovercar in the Y direction. For example, the first column body 21 may include a left first column body 21 and a right first column body 21, the left first column body 21 and the right first column body 21 are integrated to replace an upper part of an a-column reinforcement of a conventional automobile roof, and can be connected with a side wall inner plate and a side wall outer plate of a body of a flying automobile in at least one of a screw joint, a riveting and a glue joint manner. Because a cavity is formed between the side wall inner plate and the side wall outer plate of the aerocar, the left first column body 21 and the right first column body 21 can be respectively contained in the cavity formed by the side wall coaming and the side wall outer plate and connected with the aerocar body, so that the cavity space is more effectively utilized. It will be appreciated that the second column 22 may be provided by the connection of the first column 21, and may be shaped and sized according to the structure of the body of the hovercar, so as to be coupled with the rear part of the body of the hovercar.

Referring to fig. 1 and 2, in one embodiment, the roof mounting beam 12 is provided with a connection joint 15 for connecting with the body on a side close to the rear part of the body of the hovercar, and the connection joint 15 and the roof structure are integrally formed.

For example, when the roof mounting rail 12 includes the front rail 121, the rear rail 122, the left rail 123, and the right rail 124, the connection joint 15 may be provided on the rear rail 122 and extend from the left rail 123 and the right rail 124 in the X direction toward the rear of the vehicle body, thereby achieving connection with the rear of the vehicle body.

Referring to fig. 1, 2 and 5, in order to improve the structural strength of the roof structure and improve the flight performance of the hovercar, in one embodiment, the roof mounting rail 12 is provided with a second reinforcing structure 32, and the second reinforcing structure 32 includes a plurality of second reinforcing ribs arranged at intervals along the length direction of the front cross member 121, the rear cross member 122, the left cross member 123 and the right cross member 124; and/or, the column body 20 is provided with a third reinforcing structure 33, and the third reinforcing structure comprises a plurality of third reinforcing ribs which are arranged at intervals along the length direction of the first column body 21 and/or the second column body 22.

The second reinforcing ribs may be disposed outside the front cross member 121, the rear cross member 122, the left cross member 123, and the right cross member 124, and are used to protect and reinforce the structure of the roof mounting beam 12. The length direction of the column 20 may be a direction extending from the roof mounting beam 12 toward the vehicle body, for example, the direction may be a Z direction or a direction forming a certain included angle with the Z direction, and the third reinforcing rib is disposed on the first column 21 and/or the second column 22, for example, the inner side of the first column 21 and/or the second column 22, and is disposed at an interval in the length direction of the first column 21 and/or the second column 22, so that the structural strength of the first column 21 and/or the second column 22 may be improved, thereby enhancing the connection reliability of the first column 21 and/or the second column 22 with the vehicle body, and further improving the safety of the hovercar.

In one embodiment, the third reinforcing rib may include an a-pillar third reinforcing rib disposed inside the first pillar 21 and a B-pillar third reinforcing rib disposed inside the second pillar 22, the a-pillar third reinforcing rib may have a predetermined size in the Y direction and the Z direction, for example, set to be less than 95mm by 40mm, and have a predetermined thickness in the X direction, for example, set to be a square rib structure of 3mm to 5mm, and the square rib structure penetrates through the left first pillar 21 and extends to the right first pillar 21, and is integrated with the side beams 13 on both sides. Correspondingly, the B-pillar third reinforcing rib may have a predetermined size in the Y direction and the Z direction, for example, less than 80mm by 60mm, and a predetermined thickness in the X direction, for example, a square rib structure of 3mm to 5mm, where the square rib structure penetrates from the left-side second pillar 22 to the right-side second pillar 22, and is set as an integrated structure with the second pillar 22. Through with A post third strengthening rib and/or B post third strengthening rib equipartition at the cylinder 20 inboard, can play first cylinder 21 and second cylinder 22 lightweight and reinforcing effect.

In one embodiment, the B-pillar third reinforcing rib is further integrated with the rear cross member 122, the left cross member 123 and the right cross member 124, so that the rear cross member 122, the left cross member 123, the right cross member 124 and the second pillar 22 are reinforced by the B-pillar third reinforcing rib to improve the overall structural strength of the hovercar.

Referring to fig. 5, in one embodiment, a hollow area 100 for mounting a windshield component is surrounded by a fourth reinforcing structure 34; the fourth reinforcing structure 34 includes a plurality of fourth reinforcing beads; the fourth reinforcing ribs are arranged between the horn installation beam 11 and the edge beam 13; and/or a plurality of fourth reinforcing ribs are provided between the edge beam 13 and the first column 21.

The windshield member is disposed in the hollow area 100, and is used for providing a wind shielding effect during the flight of the hovercar, and in order to improve the performance of the windshield, the fourth reinforcing structure 34 is installed in the embodiment, and the fourth reinforcing structure 34 may include a plurality of fourth reinforcing ribs. For convenience of illustration, for example, the horn installation beam 11, the side beam 13 and the first column 21 are sequentially arranged from top to bottom in the Z direction, a hollow area 100 for installing the windshield member is formed between the horn installation beam 11 and the roof installation beam 12, and a fourth reinforcing rib may be provided between the horn installation beam 11 and the side beam 13; since the windshield member is disposed close to the roof rail 12, the fourth reinforcing rib may be disposed between the side rail 13 and the first cylinder 21, thereby improving the structural strength of the windshield member.

In one embodiment, the fourth rib may have a predetermined dimension in the Y direction and the Z direction, for example, less than 140mm by 190mm, and a predetermined thickness in the X direction, for example, 3mm to 5mm, so as to improve the structural strength of the windshield member, and the size of the fourth rib is set to facilitate the installation of the windshield member.

Corresponding to the above-mentioned top cover structure embodiment, this application still provides a hovercar and corresponding embodiment.

The present embodiment provides a flying automobile comprising a roof structure as described in any of the above embodiments. The flying automobile comprises an automobile body and a horn, wherein a top cover structure is respectively connected with the automobile body and wings. By arranging the integrally formed top cover structure, the number of parts can be reduced, the weight of the flying automobile is reduced, and the light weight is favorably realized; and the force transmission path of the flying automobile is simpler, and the improvement of the structural strength is facilitated.

Having described embodiments of the present application, the foregoing description is intended to be exemplary, not exhaustive, and not limited to the disclosed embodiments. Many modifications and variations will be apparent to those of ordinary skill in the art without departing from the scope and spirit of the described embodiments. The terminology used herein was chosen in order to best explain the principles of the embodiments, the practical application, or improvements to the technology in the marketplace, or to enable others of ordinary skill in the art to understand the embodiments disclosed herein.

Claims (10)

1. A roof structure, comprising:

a plurality of beam bodies and a plurality of columns which are integrally formed;

the beam bodies comprise horn mounting beams and top cover mounting beams connected with the horn mounting beams, a plurality of columns are arranged at the bottoms of the top cover mounting beams, and the columns are used for being connected with the body of a flying automobile;

the both ends of horn installation roof beam are equipped with the horn installation department, the horn installation roof beam with be formed with the cavity region that is used for installing windshield part between the top cap installation roof beam.

2. The roof structure of claim 1, wherein:

still including connect in the both ends of horn installation roof beam with boundary beam between the top cap installation roof beam, horn installation roof beam is located the top of top cap installation roof beam, the boundary beam along the slant connect in horn installation roof beam with between the top cap installation roof beam.

3. The roof structure of claim 2, wherein:

the top cover mounting beam comprises a front cross beam, a rear cross beam, a left cross beam and a right cross beam, the front cross beam, the rear cross beam, the left cross beam and the right cross beam enclose to form a frame body, the horn mounting beam is connected to the front cross beam, and the columns are arranged at four corners of the frame body respectively;

the front cross beam, the rear cross beam, the left cross beam and the right cross beam are used for arranging a cover plate in a surrounding area.

4. The roof structure of claim 1, wherein:

the horn installation roof beam is established to hollow out construction.

5. The roof structure of claim 4, wherein:

the horn installation roof beam is equipped with first additional strengthening, first additional strengthening includes the edge a plurality of first strengthening ribs of the length direction interval arrangement of horn installation roof beam, first strengthening rib along vertical support in the upper and lower both sides of horn installation roof beam.

6. The roof structure of claim 3, wherein:

the cylinders comprise two first cylinders arranged close to the front part of the vehicle body and two second cylinders arranged close to the rear part of the vehicle body;

the first cylinder is arranged corresponding to the left side and the right side of the front portion of the vehicle body, and the second cylinder is arranged corresponding to the left side and the right side of the rear portion of the vehicle body.

7. The roof structure of claim 1, wherein:

and one side of the top cover mounting beam close to the rear part of the body of the flying automobile is provided with a connecting joint for connecting with the body.

8. The roof structure of claim 6, wherein:

the top cover mounting beam is provided with a second reinforcing structure, and the second reinforcing structure comprises a plurality of second reinforcing ribs which are arranged at intervals along the length directions of the front cross beam, the rear cross beam, the left cross beam and the right cross beam; and/or the presence of a gas in the gas,

the cylinder is equipped with third additional strengthening, third additional strengthening includes along the length direction interval arrangement of first cylinder and/or the second cylinder a plurality of third strengthening ribs.

9. The capping structure of claim 6 wherein:

a fourth reinforcing structure is arranged around the hollow area for mounting the windshield component;

the fourth reinforcing structure comprises a plurality of fourth reinforcing ribs; the fourth reinforcing ribs are arranged between the horn mounting beam and the edge beam; and/or a plurality of fourth reinforcing ribs are arranged between the edge beam and the first column body.

10. A flying automobile, comprising: the roof structure of any of claims 1-9.

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