CN219220113U - Hinge mounting plate, hinge, cabin joint assembly and vehicle - Google Patents

Hinge mounting plate, hinge, cabin joint assembly and vehicle Download PDF

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Publication number
CN219220113U
CN219220113U CN202320042289.8U CN202320042289U CN219220113U CN 219220113 U CN219220113 U CN 219220113U CN 202320042289 U CN202320042289 U CN 202320042289U CN 219220113 U CN219220113 U CN 219220113U
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China
Prior art keywords
mounting plate
hinge mounting
hinge
cabin
nacelle
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CN202320042289.8U
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Chinese (zh)
Inventor
戴太亮
曾榕
马涛
韩志兵
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Xiaomi Automobile Technology Co Ltd
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Xiaomi Automobile Technology Co Ltd
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    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02EREDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
    • Y02E10/00Energy generation through renewable energy sources
    • Y02E10/70Wind energy
    • Y02E10/72Wind turbines with rotation axis in wind direction

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Abstract

The utility model discloses a hinge mounting plate, a hinge, a cabin joint assembly and a vehicle. The hinge mounting plate can connect a plurality of parts of the engine room into a whole and form a continuous longitudinal connecting structure, has the effect of enhancing the force transmission performance and the structural rigidity of the front part of the vehicle, and further can improve the NVH performance of the whole vehicle.

Description

Hinge mounting plate, hinge, cabin joint assembly and vehicle
Technical Field
The utility model relates to the technical field of vehicles, in particular to a hinge mounting plate, a hinge, a cabin joint assembly and a vehicle.
Background
At present, devices such as an engine or a motor of a vehicle are arranged in a front cabin of the vehicle, and in order to ensure the safety of driving and protect the devices in the cabin, the front part of the vehicle needs to have better force transmission performance and structural strength, but in the related art, the force transmission performance and structural rigidity of the structure of the front part of the vehicle cannot meet the use requirements, and further space for structural optimization and performance improvement is still reserved.
Disclosure of Invention
The present utility model aims to solve at least one of the technical problems in the related art to some extent.
Therefore, the embodiment of the utility model provides the hinge mounting plate, which can connect a plurality of parts of a cabin into a whole and form a continuous longitudinal connecting structure, has the effect of enhancing the force transmission performance and the structural rigidity of the front part of a vehicle, and further can improve the NVH performance of the whole vehicle.
The embodiment of the utility model also provides a hinge comprising the hinge mounting plate.
The embodiment of the utility model also provides a cabin joint assembly comprising the hinge mounting plate.
The embodiment of the utility model also provides a vehicle comprising the cabin joint assembly.
The hinge mounting plate comprises a plate body, wherein the plate body is provided with a first connecting part and a second connecting part which are arranged at intervals in a first direction, the first connecting part is used for being connected with a front vibration reduction tower of a vehicle, and the second connecting part is used for being connected with an A column and/or a cabin roof side rail.
The hinge mounting plate provided by the embodiment of the utility model can connect a plurality of parts of the engine room into a whole and form a continuous longitudinal connecting structure, so that the effect of enhancing the force transmission performance and the structural rigidity of the front part of the vehicle is achieved, and the NVH performance of the whole vehicle can be further improved.
In some embodiments, the thickness dimension of the plate body is 2.5 millimeters to 3 millimeters.
In some embodiments, the plate body is provided with a third connection for connection with the nacelle.
In some embodiments, the first connection is provided with a first hole for a first fastener to pass through;
and/or the second connecting part is provided with at least one second hole for the second fastener to pass through, and the at least one second hole is arranged at intervals in a second direction.
The hinge of the embodiment of the utility model comprises a rotating piece and the hinge mounting plate in any embodiment, wherein the rotating piece is rotatably connected with the hinge mounting plate, and the rotating piece is used for being connected with a cabin cover of a cabin.
In some embodiments, the rotating member includes a first section for connecting to the hatch cover and a second section hinged to the hinge mounting plate, at least a portion of the second section having a U-shaped cross section.
The nacelle joint assembly of an embodiment of the utility model includes a hinge mounting plate as described in any of the embodiments above.
In some embodiments, the nacelle joint assembly includes:
the front vibration damping tower is connected with the first connecting part of the hinge mounting plate;
the A column is connected with the second connecting part of the hinge mounting plate;
and the cabin upper edge beam is connected with the second connecting part of the hinge mounting plate.
In some embodiments, the front vibration-damping tower is provided with a diagonal bracing portion, the diagonal bracing portion is connected with the hinge mounting plate and the cabin roof side rail, the diagonal bracing portion comprises a transverse rib and a diagonal rib, and the transverse rib, the diagonal rib and the cabin roof side rail form a triangular structure.
In some embodiments, the a-pillar includes an a-pillar inner panel and an a-pillar reinforcement panel, the a-pillar reinforcement panel being connected to an outer side of the a-pillar inner panel, the hinge mounting plate being disposed inside the a-pillar and connected to the a-pillar inner panel.
In some embodiments, the cabin roof side rail includes a roof side rail inner panel and a roof side rail outer panel, the roof side rail inner panel is connected to the roof side rail outer panel, and the hinge mounting plate is disposed in the cabin roof side rail and connected to the roof side rail inner panel.
The vehicle of an embodiment of the utility model comprises a cabin joint assembly as described in any of the embodiments above.
Drawings
Fig. 1 is a schematic perspective view of a hinge according to an embodiment of the present utility model.
Fig. 2 is a right side schematic view of the hinge of fig. 1.
FIG. 3 is a right side schematic view of a nacelle joint assembly of an embodiment of the utility model.
FIG. 4 is a left side schematic view of a nacelle joint assembly of an embodiment of the utility model.
FIG. 5 is a schematic bottom view of a nacelle joint assembly of an embodiment of the utility model.
Reference numerals:
a hinge 100;
a hinge mounting plate 1; a first connection portion 11; a first hole 111; a second connecting portion 12; a second hole 121; a third connecting portion 13; a flange 14;
a rotating member 2; a first section 21; a second section 22;
a pivot 3;
front shock absorber 200; a diagonal brace 201; transverse ribs 202; diagonal rib 203;
a column a 300; a column a reinforcing plate 301; a pillar inner panel 302;
a cabin roof side rail 400; a roof side rail outer panel 401; roof side rail inner panel 402.
Detailed Description
Reference will now be made in detail to embodiments of the present utility model, examples of which are illustrated in the accompanying drawings. The embodiments described below by referring to the drawings are illustrative and intended to explain the present utility model and should not be construed as limiting the utility model.
As shown in fig. 1 and 2, the hinge mounting plate 1 according to the embodiment of the present utility model includes a plate body, which may be substantially rectangular, and may be integrally formed by sheet metal stamping. The lower limit value of the thickness dimension of the plate body is not less than a set threshold value, for example, the thickness dimension of the plate body may be not less than 2.5mm (lower limit value), and the specific thickness dimension may be 2.6 mm, 2.8 mm, 3mm, 4 mm, or the like. Therefore, the plate body has higher structural strength, thereby meeting the use requirement.
As shown in fig. 1 and 2, the plate body is provided with first connection portions 11 and second connection portions 12 arranged at intervals in a first direction, wherein the first direction may be a front-rear direction, the first connection portions 11 may be a front-lower portion of the plate body, and the second connection portions 12 may be a rear-lower portion of the plate body. In use, the first connection 11 is used to connect with the front shock tower 200 of the vehicle and the second connection 12 is used to connect with the A-pillar 300 and/or the cabin roof rail 400.
The hinge mounting plate 1 of the embodiment of the utility model can connect a plurality of parts of a cabin (the front vibration-damping tower 200, the A column 300 and the cabin roof side rail 400) into a whole and form a continuous longitudinal connecting structure, thereby playing the role of enhancing the force transmission performance and the structural rigidity of the front part of a vehicle and further improving the NVH performance of the whole vehicle.
In some embodiments, the thickness dimension of the plate body is 2.5 millimeters to 3 millimeters. For example, the thickness dimension of the plate body can be 2.5mm, 2.7 mm, 2.9 mm, 3mm and the like, thereby avoiding material waste and reducing cost while ensuring the structural strength of the plate body.
In some embodiments, the plate body is provided with a third connection 13, the third connection 13 being intended to be connected to the nacelle. For example, as shown in fig. 1, the third connecting portion 13 may be a pin structure, a pin shaft, or the like, and the third connecting portion 13 may be provided at the front upper side of the panel body, and when in use, the third connecting portion 13 may be connected to the nacelle, and the first connecting portion 11, the second connecting portion 12, and the third connecting portion 13 may form a triangle-shaped mounting structure, thereby improving the mounting structure strength and stability of the panel body.
In some embodiments, the first connection portion 11 is provided with a first hole 111, the first hole 111 being for the first fastener to pass through. As shown in fig. 2, the first connection part 11 may be provided with only one first hole 111, and the first hole 111 may be positioned at a front lower corner position of the plate body, and a bolt (first fastener) may be inserted through the first hole 111 and connected to the front shock-absorbing tower 200 when assembled.
In some embodiments, the second connection portion 12 is provided with at least one second hole 121, the second hole 121 being for the second fastener to pass through, and the at least one second hole 121 being spaced apart in the second direction. For example, as shown in fig. 2, two second holes 121 may be provided, and the two second holes 121 may be arranged at intervals in the up-down direction, and when installed, the second holes 121 may also be provided for bolts (second fasteners) to pass through and be connected and fixed with both the a-pillar 300 and the nacelle roof rail 400.
The two second holes 121 may form three apexes of a triangle shape with the first hole 111, so that stability and structural strength of installation of the first and second connection parts 11 and 12 may be improved.
In some embodiments, the flange 14 is provided on the peripheral side of the plate body, the flange 14 may extend along the peripheral direction of the plate body, and the flange 14 may be formed by stamping, so that the structural strength of the plate body may be enhanced, thereby meeting the use requirement.
The hinge 100 of the embodiment of the present utility model is described below.
As shown in fig. 1 and 2, the hinge 100 according to the embodiment of the present utility model includes a rotation member 2 and a hinge mounting plate 1, the hinge mounting plate 1 may be the hinge mounting plate 1 described in any of the above embodiments, the rotation member 2 is rotatably connected to the hinge mounting plate 1, for example, the rotation member 2 and the hinge mounting plate 1 may be rotatably assembled by a pivot shaft 3, the pivot shaft 3 may be provided at a rear upper corner position of the plate body, and the rotation member 2 is used to be connected to a cover of a nacelle. For example, the rotating member 2 may be fixed to a cabin cover of the cabin by a bolt, and the rotating member 2 may be provided with two fitting holes through which the bolts or the like may pass. When the rotary member 2 is used, the rotary member can synchronously swing along with the hatch cover, so that the requirement of the rotation assembly of the hatch cover is met.
In some embodiments, the rotor 2 comprises a first section 21 and a second section 22, the first section 21 being intended to be connected to a hatch, the second section 22 being hinged to the hinge mounting plate 1, and at least part of the second section 22 being U-shaped in cross section.
For example, as shown in fig. 2, the rotating member 2 may be of a unitary structure, for example, the rotating member 2 may be formed by bending a sheet metal, wherein the first section 21 may be located at the front side of the second section 22, the first section 21 may be of a single-layer structure, and the assembly hole may be provided in the first section 21.
The second section 22 is U-shaped groove-shaped, and the upper edge and the lower edge of the second section 22 are turned over and turned over to the right, so that the second section 22 forms a double-layer structure, and the structural strength of the second section 22 can be enhanced, thereby meeting the structural strength requirements of support, torsion resistance and the like of the rotating member 2. The pivot 3 may be disposed at the rear end of the second section 22, and a portion of the pivot 3 may be hidden in a U-shaped groove formed in the second section 22, thereby playing a protective role.
A nacelle joint assembly according to an embodiment of the utility model is described below.
The nacelle joint assembly of the embodiments of the utility model comprises a hinge mounting plate 1, which hinge mounting plate 1 may be the hinge mounting plate 1 described in any of the embodiments described above. The nacelle joint assembly may also include a front shock tower 200, an A-pillar 300, and a nacelle roof rail 400. As shown in fig. 3, the front vibration-damping tower 200 is connected to the first connection portion 11 of the hinge mounting plate 1, the a-pillar 300 is connected to the second connection portion 12 of the hinge mounting plate 1, and the nacelle roof rail 400 is connected to the second connection portion 12 of the hinge mounting plate 1.
Because the front cover hinge mounting plate 1 is thicker (2.5 mm-3 mm) and is mounted between the closed stiffening beam structures formed by the cast aluminum front damping tower 200, the A column 300 and the cabin roof side rail 400 through bolts by means of the high-rigidity structure, structural members with enough rigidity between the two rigid structures (the front damping tower 200, the A column 300 and the cabin roof side rail 400) can be connected.
The hinge mounting plate 1 can just meet the rigidity requirement of the mounting point of the engine cover (hatch cover) hinge 100, and simultaneously, plays a role of connecting the front vibration damping tower 200, the upper side beam and the A column 300 and can form a continuous longitudinal connecting structure. Because the upper side beam is used as the most important force transmission path in the small offset working condition, the front end of the A column 300 can be effectively reinforced through the reinforcing structure, and the structural stability of the front end of the A column 300 is ensured. In addition, as the front end connector of the A column 300 is also a key structure for ensuring the NVH performance of the whole vehicle, the reinforcing structure can effectively improve the dynamic rigidity of the front shock absorber and the mode of the front windshield frame opening.
In some embodiments, the front vibration-damping tower 200 is provided with a diagonal bracing portion 201, the diagonal bracing portion 201 is connected with the hinge mounting plate 1 and the cabin roof side rail 400, the diagonal bracing portion 201 includes a transverse rib 202 and a diagonal rib 203, and the transverse rib 202, the diagonal rib 203 and the cabin roof side rail 400 form a triangular structure.
As shown in fig. 5, the diagonal brace 201 may be integrally formed with the front shock absorber 200, and the diagonal brace 201 is a portion of the front shock absorber 200 extending obliquely and used for lap joint. The bottom of the diagonal brace 201 may be provided with a diagonal rib 203, and the diagonal rib 203 may extend generally in a left front-to-right rear direction, with the diagonal rib 203 extending to the cabin roof rail 400. The bottom of the diagonal brace portion 201 may be further provided with a plurality of lateral ribs 202, the plurality of lateral ribs 202 may be arranged at intervals in the front-rear direction, and each lateral rib 202 may extend in the left-right direction.
The plurality of transverse ribs 202 may be disposed within an angle formed by the diagonal rib 203 and the cabin roof side rail 400, and a length dimension of the plurality of transverse ribs 202 may be gradually increased along a rear-to-front direction, so as to accommodate a change in a distance between the diagonal rib 203 and the cabin roof side rail 400.
Each of the transverse rib 202, the oblique rib 203 and the cabin roof side rail 400 may form a triangle structure, which may play a role in enhancing structural strength on one hand, and may transmit impact load in the Z direction (up-down direction) of the center of the front shock absorber 200 to the rear portion of the cabin roof side rail 400 through multiple paths (the oblique rib 203 and each transverse rib 202) in a dispersed manner, thereby improving durability and reliability of the front shock absorber 200.
In some embodiments, as shown in fig. 3 and 4, the a-pillar 300 includes an a-pillar inner panel 302 and an a-pillar reinforcing panel 301, where the a-pillar reinforcing panel 301 is connected to the outer side of the a-pillar inner panel 302, specifically, may be connected and fixed by bolts, welding, etc., and the hinge mounting plate 1 is disposed inside the a-pillar 300 and connected to the a-pillar inner panel 302. Thereby, the hinge mounting plate 1 can connect more parts as one body, so that a coherent longitudinal connection structure can be formed.
In some embodiments, as shown in fig. 3 and 4, the cabin roof side rail 400 includes a roof side rail inner panel 402 and a roof side rail outer panel 401, where the roof side rail inner panel 402 is connected and fixed in the roof side rail outer panel 401, specifically, may also be connected and fixed by bolts, welding, etc., and the hinge mounting plate 1 is provided in the cabin roof side rail 400 and connected with the roof side rail inner panel 402. Thereby, the hinge mounting plate 1 can connect more parts as one body, so that a coherent longitudinal connection structure can be formed.
A vehicle of an embodiment of the utility model is described below.
The vehicle of an embodiment of the utility model comprises a cabin joint assembly, which may be any of the cabin joint assemblies described in the embodiments above. The vehicle may be an electric vehicle, a bus, an SUV, a pick-up card, etc., but may be other vehicles having cabin joint assemblies.
In some embodiments, the vehicle includes two cabin joint assemblies, and the two cabin joint assemblies are symmetrically arranged in a left-right direction of the vehicle, so that a continuous longitudinal structure can be formed on both left and right sides of a front end of the vehicle, thereby achieving the effect of enhancing force transmission performance and structural rigidity on both left and right sides of a front portion of the vehicle, and further improving NVH performance of the whole vehicle.
In the description of the present utility model, it should be understood that the terms "center", "longitudinal", "lateral", "length", "width", "thickness", "upper", "lower", "front", "rear", "left", "right", "vertical", "horizontal", "top", "bottom", "inner", "outer", "clockwise", "counterclockwise", "axial", "radial", "circumferential", etc. indicate orientations or positional relationships based on the orientations or positional relationships shown in the drawings are merely for convenience in describing the present utility model and simplifying the description, and do not indicate or imply that the device or element being referred to must have a specific orientation, be configured and operated in a specific orientation, and therefore should not be construed as limiting the present utility model.
Furthermore, the terms "first," "second," and the like, are used for descriptive purposes only and are not to be construed as indicating or implying a relative importance or implicitly indicating the number of technical features indicated. Thus, a feature defining "a first" or "a second" may explicitly or implicitly include at least one such feature. In the description of the present utility model, the meaning of "plurality" means at least two, for example, two, three, etc., unless specifically defined otherwise.
In the present utility model, unless explicitly specified and limited otherwise, the terms "mounted," "connected," "secured," and the like are to be construed broadly, and may be, for example, fixedly connected, detachably connected, or integrally formed; may be mechanically connected, may be electrically connected or may be in communication with each other; either directly or indirectly, through intermediaries, or both, may be in communication with each other or in interaction with each other, unless expressly defined otherwise. The specific meaning of the above terms in the present utility model can be understood by those of ordinary skill in the art according to the specific circumstances.
In the present utility model, unless expressly stated or limited otherwise, a first feature "up" or "down" a second feature may be the first and second features in direct contact, or the first and second features in indirect contact via an intervening medium. Moreover, a first feature being "above," "over" and "on" a second feature may be a first feature being directly above or obliquely above the second feature, or simply indicating that the first feature is level higher than the second feature. The first feature being "under", "below" and "beneath" the second feature may be the first feature being directly under or obliquely below the second feature, or simply indicating that the first feature is less level than the second feature.
For purposes of this disclosure, the terms "one embodiment," "some embodiments," "example," "a particular example," or "some examples," etc., mean that a particular feature, structure, material, or characteristic described in connection with the embodiment or example is included in at least one embodiment or example of the utility model. In this specification, schematic representations of the above terms are not necessarily directed to the same embodiment or example. Furthermore, the particular features, structures, materials, or characteristics described may be combined in any suitable manner in any one or more embodiments or examples. Furthermore, the different embodiments or examples described in this specification and the features of the different embodiments or examples may be combined and combined by those skilled in the art without contradiction.
While the above embodiments have been shown and described, it should be understood that the above embodiments are illustrative and not to be construed as limiting the utility model, and that variations, modifications, alternatives, and variations of the above embodiments may be made by those of ordinary skill in the art without departing from the scope of the utility model.

Claims (12)

1. The hinge mounting plate is characterized by comprising a plate body, wherein the plate body is provided with a first connecting part and a second connecting part which are arranged at intervals in a first direction, the first connecting part is used for being connected with a front vibration reduction tower of a vehicle, and the second connecting part is used for being connected with an A column and/or a cabin roof side rail.
2. The hinge mounting plate of claim 1, wherein the thickness dimension of the plate body is 2.5mm to 3 mm.
3. The hinge mounting plate according to claim 1, wherein the plate body is provided with a third connection portion for connection to a nacelle.
4. A hinge mounting plate according to any one of claims 1-3, wherein the first connection portion is provided with a first aperture for passing a first fastener therethrough;
and/or the second connecting part is provided with at least one second hole for the second fastener to pass through, and the at least one second hole is arranged at intervals in a second direction.
5. A hinge comprising a swivel member and a hinge mounting plate according to any one of the preceding claims 1-4, said swivel member being rotatably connected to said hinge mounting plate and said swivel member being adapted to be connected to a hatch of a nacelle.
6. The hinge of claim 5, wherein the swivel member comprises a first section for connection to the hatch and a second section hinged to the hinge mounting plate, and wherein at least a portion of the second section is U-shaped in cross section.
7. Nacelle joint assembly comprising a hinge mounting plate according to any of the claims 1-6.
8. The nacelle joint assembly of claim 7, comprising:
the front vibration damping tower is connected with the first connecting part of the hinge mounting plate;
the A column is connected with the second connecting part of the hinge mounting plate;
and the cabin upper edge beam is connected with the second connecting part of the hinge mounting plate.
9. The nacelle joint assembly of claim 8, wherein the front shock tower is provided with a diagonal brace portion that is coupled to the hinge mounting plate and the nacelle roof rail, the diagonal brace portion including a transverse rib and a diagonal rib, the transverse rib, the diagonal rib, and the nacelle roof rail forming a triangular structure.
10. The cabin joint assembly of claim 8, wherein the a-pillar includes an a-pillar inner panel and an a-pillar reinforcement panel, the a-pillar reinforcement panel being attached to an outer side of the a-pillar inner panel, the hinge mounting plate being disposed inside the a-pillar and being attached to the a-pillar inner panel.
11. The cabin joint assembly of claim 8, wherein the cabin roof rail includes a roof rail inner panel and a roof rail outer panel, the roof rail inner panel being connected within the roof rail outer panel, the hinge mounting plate being disposed within the cabin roof rail and connected with the roof rail inner panel.
12. A vehicle comprising a nacelle joint assembly according to any one of claims 7-11.
CN202320042289.8U 2023-01-06 2023-01-06 Hinge mounting plate, hinge, cabin joint assembly and vehicle Active CN219220113U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN202320042289.8U CN219220113U (en) 2023-01-06 2023-01-06 Hinge mounting plate, hinge, cabin joint assembly and vehicle

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN202320042289.8U CN219220113U (en) 2023-01-06 2023-01-06 Hinge mounting plate, hinge, cabin joint assembly and vehicle

Publications (1)

Publication Number Publication Date
CN219220113U true CN219220113U (en) 2023-06-20

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Family Applications (1)

Application Number Title Priority Date Filing Date
CN202320042289.8U Active CN219220113U (en) 2023-01-06 2023-01-06 Hinge mounting plate, hinge, cabin joint assembly and vehicle

Country Status (1)

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CN (1) CN219220113U (en)

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