Sealing strip, cabin equipment and vehicle

Abstract

The utility model discloses a sealing strip, a cabin structure and a vehicle, the sealing strip is suitable for being installed at the matching position of a first installation piece and a second installation piece, the first installation piece and the second installation piece are installed and matched in the first direction, the sealing strip comprises an insertion matching part and a sealing part, the sealing portion is used for abutting against a second installation piece in a sealed mode, a first deformation cavity is formed in the sealing portion, the inserting matching portion is used for being connected with the first installation piece in an inserting mode in the second direction, and the second direction intersects with the first direction. According to the sealing strip, when the sealing strip is applied to sealing between a cabin body and a cabin door, the sealing strip can be stably matched with the cabin body in a sealing mode through the sealing part, meanwhile, the inserting matching part of the sealing strip can be matched with the cabin door in an inserting mode, and the inserting direction intersects with the opening or closing direction of the cabin door. The situation that the sealing strip falls off in the opening and closing process of the cabin door can be well avoided, and the installation stability of the sealing strip is guaranteed.

Description

TECHNICAL FIELD

[0001] The utility model relates to sealing technical field especially relates to a sealing strip, cabin equipment and vehicle. BACKGROUND

[0002] With the rise and rapid development of new energy vehicles and artificial intelligence, the intelligence, convenience and interesting of vehicles gradually become one of the focuses of competition of major vehicle manufacturers, like some vehicles are equipped with unmanned aerial vehicle cabins to accommodate unmanned aerial vehicles. In the related art, the sealing of the unmanned aerial vehicle cabin is mainly realized by the sealing strip between the cabin door and the cabin body, but the current sealing strip is prone to falling off during the closing or opening process of the cabin door, and there is room for improvement. SUMMARY

[0003] The utility model aims at solving one of the technical problems in the prior art. To this end, the utility model provides a sealing strip, which can well avoid the problem of bulging when applied to a cabin body and a cabin door.

[0004] According to the sealing strip of the utility model embodiment, the sealing strip is suitable for being installed at the matching place of the first mounting piece and the second mounting piece, and the first mounting piece and the second mounting piece are installed and matched along the first direction, the sealing strip comprises a plug-in matching part and a sealing part, the sealing part is used for sealing and pressing against the second mounting piece, a first deformation cavity is formed in the sealing part, the plug-in matching part is used for plug-in matching with the first mounting piece along the second direction, and the second direction intersects with the first direction.

[0005] According to the sealing strip of the utility model embodiment, when the sealing strip is applied to seal between a cabin body and a cabin door, the sealing strip can stably seal and match with the cabin body through the sealing part, at the same time, the plug-in matching part of the sealing strip can plug-in match with the cabin door and the plug-in direction intersects with the direction of opening or closing of the cabin door, which can well avoid the situation that the sealing strip falls off during the opening and closing of the cabin door, and ensure the installation stability of the sealing strip.

[0006] According to the sealing strip of some embodiments of the utility model, the included angle between the first direction and the second direction is less than or equal to 90° and greater than 45°.

[0007] According to the sealing strip of some embodiments of the utility model, the sealing part comprises a first sealing section and a second sealing section, the first sealing section is connected with the plug-in matching part, the second sealing section is connected with the first sealing section and jointly defines a first deformation cavity, and the second sealing section and / or the first sealing section forms a deformation angle.

[0008] According to the sealing strip of some embodiments of the utility model, the first sealing section and the plug-in matching part are made of dense glue;

[0009] And / or, the second sealing section is made of sponge rubber.

[0010] According to the sealing strip of some embodiments of the utility model, the first sealing section is formed with at least one dense rubber deformation angle;

[0011] And / or, the second sealing section is formed with at least one sponge rubber deformation angle.

[0012] According to the sealing strip of some embodiments of the utility model, the dense rubber deformation angle and the sponge rubber deformation angle are distributed in the circumferential direction of the first deformation cavity.

[0013] According to the sealing strip of some embodiments of the utility model, the dense rubber deformation angle and the sponge rubber deformation angle are connected with an intermediate deformation angle.

[0014] According to the sealing strip of some embodiments of the utility model, the dense rubber deformation angle and the sponge rubber deformation angle are both configured to protrude outward relative to the first deformation cavity;

[0015] And / or, the intermediate deformation angle is configured to protrude inward relative to the first deformation cavity.

[0016] According to the sealing strip of some embodiments of the utility model, a second deformation cavity is formed in the plug-in fitting part.

[0017] According to the sealing strip of some embodiments of the utility model, the inner cavity volume of the second deformation cavity is smaller than the inner cavity volume of the first deformation cavity.

[0018] According to the sealing strip of some embodiments of the utility model, the plug-in fitting part is formed with a clamping protruding rib, and the clamping protruding rib is used for clamping connection with the first mounting piece.

[0019] According to the sealing strip of some embodiments of the utility model, the plug-in fitting part is provided with at least one clamping protruding rib on each of two sides facing away from each other.

[0020] The utility model also proposes a cabin equipment.

[0021] The cabin equipment according to the embodiments of the utility model comprises a cabin, a hatch and the sealing strip of any one of the above embodiments, the cabin is formed with a hatchway, the hatch is installed on the cabin, the hatch is suitable for moving along the first direction relative to the cabin to open or close the hatchway, the hatch is provided with a connecting slot, the plug-in fitting part is plugged in and fitted with the connecting slot along the second direction, and the sealing part is sealed and pressed on the cabin.

[0022] According to the cabin equipment of some embodiments of the utility model, the deformation angle is located on the side of the sealing strip towards the cabin.

[0023] The utility model also provides a vehicle.

[0024] The vehicle according to the utility model embodiment comprises the cabin device of any one of the above-mentioned embodiments, and the cabin device is configured as a drone cabin.

[0025] The vehicle, the cabin device and the sealing strip have the same advantages as the prior art, and details are not repeated here.

[0026] The additional aspects and advantages of the utility model will be partially given in the following description, some will become obvious from the following description, or be understood through the practice of the utility model. BRIEF DESCRIPTION OF DRAWINGS

[0027] The above and / or additional aspects and advantages of the utility model will become apparent and more readily understood from the following description, taken in conjunction with the accompanying drawings, in which:

[0028] Figure 1 is the sectional view of the sealing strip of some embodiments of the utility model;

[0029] Figure 2 is the sectional view of the sealing strip installed between the cabin body and the cabin door of some embodiments of the utility model;

[0030] Figure 3 is the sectional view of the sealing strip installed between the cabin body and the cabin door of some embodiments of the utility model (sealing strip deformation);

[0031] Figure 4 is the sectional view of the sealing strip installed between the cabin body and the cabin door of some other embodiments of the utility model;

[0032] Figure 5 is the sectional view of the sealing strip installed between the cabin body and the cabin door of some other embodiments of the utility model (sealing strip deformation);

[0033] Figure 6 is the exploded view of the drone cabin of the utility model embodiment.

[0034] Reference signs:

[0035] Sealing strip 100,

[0036] Plug-in matching part 1, second deformation cavity 11, clamping convex rib 12, sealing part 2, first sealing section 21, second sealing section 22, sealing matching surface 221, dense glue deformation angle 23, sponge glue deformation angle 24, middle deformation angle 25, first deformation cavity 26, fiber wire 3,

[0037] Cabin body 200, hatch 201, cabin door 300, connecting slot 301. DETAILED DESCRIPTION

[0038] The embodiments of the present application will be described below in detail, examples of which are shown in the drawings, wherein the same or similar notations represent the same or similar elements having the same or similar functions throughout. The embodiments described below by reference to the drawings are exemplary only, and are for the purpose of explanation only and are not to be taken as limiting the present application.

[0039] In the description of the present application, it should be understood that the orientation or positional relationship indicated by the terms "center", "longitudinal", "lateral", "length", "width", "thickness", "upper", "lower", "front", "back", "left", "right", "vertical", "horizontal", "top", "bottom", "inner", "outer", "clockwise", "counterclockwise", "axial", "radial", "circumferential" and the like is based on the orientation or positional relationship shown in the drawings, and is only for the convenience of describing the present application and simplifying the description, and does not indicate or imply that the device or element referred to must have a particular orientation, be constructed and operated in a particular orientation, and therefore cannot be understood as a limitation of the present application. In addition, the features defined as "first" and "second" can explicitly or implicitly include one or more of the features. In the description of the present application, unless otherwise specified, the meaning of "a plurality of" is two or more.

[0040] In the description of the present application, it should be noted that, unless otherwise specified and limited, the terms "mounting", "connection", "connection" should be understood broadly, for example, it can be fixedly connected, or it can be detachably connected, or integrally connected; it can be mechanically connected, or it can be electrically connected; it can be directly connected, or it can be indirectly connected through an intermediate medium, or it can be the communication between two elements. For those skilled in the art, the specific meaning of the above terms in the present application can be understood according to the specific circumstances.

[0041] The following will be described with reference to Figures 1-6 The sealing strip 100 according to the embodiments of the present application is described, which is not prone to falling off during the closing or opening process of the cabin door 300 when applied to the cabin body 200 and the cabin door 300 of the unmanned aerial vehicle, and is beneficial to the installation reliability of the sealing strip 100.

[0042] According to one embodiment of the present invention, a sealing strip 100 is adapted to be installed at the mating point of a first mounting member and a second mounting member, wherein the first mounting member and the second mounting member are installed and mated along a first direction. The sealing strip 100 includes an insertion mating portion 1 and a sealing portion 2. The sealing portion 2 is used for sealing and pressing against the second mounting member, and the insertion mating portion 1 is used for inserting and connecting with the first mounting member along a second direction. Thus, during installation, the sealing strip 100 can be relatively fixed to the first mounting member, and the sealing strip 100 and the second mounting member can be sealed and pressed together, thereby achieving a sealing fit between the first mounting member and the second mounting member. Furthermore, the sealing portion 2 can be made of an elastic material so that the sealing portion 2 can elastically press against the second mounting member to achieve a sealing fit.

[0043] Among them, such as Figures 2-5 As shown, the first direction intersects with the second direction, meaning that the first mounting member and the second mounting member can move relative to each other along the first direction to engage or disengage, and structural sealing is achieved through the sealing strip 100 when engaged. By configuring the insertion mating portion 1 of the sealing strip 100 to engage with the first mounting member along the second direction, the movement direction of the first mounting member relative to the second mounting member differs from the insertion direction of the first mounting member and the insertion mating portion 1, forming a certain angle. Therefore, during the opening or closing process of the first mounting member relative to the second mounting member, the sealing strip 100 is less likely to detach from the first mounting member under the interaction force between the first and second mounting members, thus ensuring the installation stability of the sealing strip 100 and guaranteeing sealing performance.

[0044] Specifically, for example, when the sealing strip 100 is applied to the cabin of a drone, such as Figure 5 As shown, the drone cabin includes a cabin body 200 and a door 300, as... Figures 2-5 As shown, the hatch 300 can serve as the first mounting component, and the cabin body 200 can serve as the second mounting component. The sealing strip 100 can be connected to the hatch 300 via the plug-in fitting 1 to be fixed relative to the hatch 300. When the hatch 300 is closed relative to the cabin body 200, the sealing part 2 of the sealing strip 100 presses against the cabin body 200 to achieve a sealed fit between the hatch 300 and the cabin body 200. The first direction can be the direction in which the hatch 300 is opened or closed relative to the cabin body 200. Therefore, the sealing strip 100 is less likely to fall off relative to the hatch 300 during the opening or closing process. It should be noted that the sealing strip 100 in this invention can be installed between the cabin body 200 and the hatch 300 as described above, or between other types of structural components for a sealed fit. That is, the specific mounting body is not limited to the cabin body 200 and the hatch 300 of the UAV cabin, and this invention uses the cabin body 200 and the hatch 300 as examples for description.

[0045] Among them, such asFigures 2-5 As shown, the first deformation cavity 26 is formed in the sealing portion 2, that is, the sealing portion 2 is configured as a hollow structure, so that when the sealing portion 2 is pressed against the cabin body 200, the sealing portion 2 can be elastically deformed towards the first deformation cavity 26, and the outer surface of the sealing portion 2 gradually changes from point contact to surface contact with the cabin body 200, and the contact area gradually increases with the change of elastic deformation, thereby improving the sealing effect.

[0046] According to the sealing strip 100 in the embodiment of the utility model, when the sealing strip 100 is applied to seal between the cabin body 200 and the cabin door 300, the sealing strip 100 can be stably sealed with the cabin body through the sealing portion 2, and the plug-in fitting portion 1 of the sealing strip 100 can be plug-in fitted with the cabin door 300, and the plug-in direction intersects with the opening or closing direction of the cabin door 300, which can well avoid the situation that the sealing strip 300 falls off during the opening and closing of the cabin door 300, and ensures the installation stability of the sealing strip 300.

[0047] In some embodiments, the included angle between the first direction and the second direction is less than or equal to 90° and greater than 45°, that is, the first direction and the second direction can be perpendicular to each other or close to perpendicular, so that the force generated by the movement of the first mounting member relative to the second mounting member on the sealing strip 300 does not easily cause the sealing strip 300 to separate from the first mounting member, and the sealing strip 100 can be prevented from falling off relative to the cabin door 300 during the opening or closing of the cabin door 300 relative to the cabin body 200.

[0048] Specifically, the included angle between the first direction and the second direction can be set to 46°, 48°, 49°, 50°, 52°, 55°, 56°, 58°, 59°, 60°, 62°, 65°, 66°, 68°, 69°, 70°, 72°, 75°, 76°, 78°, 79°, 80°, 81°, 83°, 84°, 87°, 89°, 90°, or other angle values in the interval, which can all prevent the sealing strip 100 from falling off.

[0049] In some embodiments, the sealing portion 2 is formed with at least one deformation angle, which can be configured as a corner protruding from the sealing portion 2. By setting the deformation angle, the deformation direction of the sealing portion 2 can be changed, such as configuring the deformation angle to have a certain degree of anti-deformation effect on the sealing portion 2 during the contact between the sealing portion 2 and the cabin body 200, so as to avoid the sealing portion 2 from forming a bulging structure due to the extrusion and deformation of the cabin door 300 and the cabin body 200 when the cabin door 300 moves relative to the cabin body 200. In other words, setting the deformation angle can strengthen the structure of the sealing portion 2, improve the structural strength of the sealing portion 2 at the deformation angle part, and enable the sealing portion 2 to deform in a directional manner, thereby avoiding the bulging phenomenon while ensuring the sealing performance of the sealing portion 2.

[0050] In practical application, as shown in Figure 2 The plug-in part 1 is fixed relative to the hatch 300, the sealing part 2 is pressed against the cabin body 200, and as the hatch 300 is further closed, as shown in Figure 3 The sealing part 2 deforms in the area outside the deformation angle, achieving effective sealing of the sealing part 2, while the sealing part 2 has a stable shape at the deformation angle, so that the sealing part 2 does not transitionally deform when pressed, i.e. the sealing part 2 is not pressed out of the cabin body 200 and the hatch 300, thereby solving the problem of the sealing part 2 bulging, ensuring sealing performance and improving the appearance of the structure after sealing.

[0051] In some embodiments, the sealing part 2 includes a first sealing section 21 and a second sealing section 22, wherein the first sealing section 21 and the second sealing section 22 can be formed separately and then connected and fixed to form an integral whole.

[0052] The first sealing section 21 is connected to the plug-in part 1, and the second sealing section 22 is connected to the first sealing section 21 and together defines a first deformation cavity 26. As shown in Figure 1 The first sealing section 21 is connected to the second sealing section 22, and as shown in the dashed line in Figure 1 The first sealing section 21 and the plug-in part 1 are fixedly connected or integrally formed, and then the second sealing section 22 is connected to the first sealing section 21; or in actual design, the first sealing section 21 and the plug-in part 1 can be formed of the same material, and the second sealing section 22 can be formed of another material, and then connected and fixed after being formed separately or both materials are formed at the same time.

[0053] The second sealing section 22 and / or the first sealing section 21 forms a deformation angle, i.e. the deformation angle can be provided on the first sealing section 21, or on the second sealing section 22, or on both the first sealing section 21 and the second sealing section 22, so that the deformation angle is provided to enhance the structural state of the first sealing section 21 and the second sealing section 22, avoid excessive deformation of the sealing part 2 when pressed, and prevent the sealing part 2 from bulging.

[0054] It should be noted that the second sealing section 22 is connected to the side of the first sealing section 21 away from the plug-in part 1, i.e. when the sealing strip 100 is installed on the cabin body 200 and the hatch 300, the plug-in part 1 is fixed relative to the hatch 300, and the surface of the second sealing section 22 away from the first sealing section 21 can be in contact with the cabin body 200, so that the deformation angle is provided to prevent the second sealing section 22 from deforming too much and forming a bulge, ensuring the stability of the sealing structure.

[0055] In some embodiments, the first sealing section 21 and the plug-in part 1 are made of dense glue, so that the first sealing section 21 and the plug-in part 1 have a relatively stable structural state. It should be noted that the plug-in part 1 is used to be connected and fixed with the first mounting part, such as the hatch 300, for example, the plug-in part 1 is clamped on the hatch 300. By setting the plug-in part 1 to be made of dense glue, the plug-in part 1 has a certain elasticity and good structural stability, so that the plug-in part 1 has a stable structural state when connected with the hatch 300, thereby ensuring the stability of the installation of the sealing strip 100 on the hatch 300.

[0056] At the same time, the first sealing section 21 is made of dense glue, so that the first sealing section 21 has a stable structural state, that is, when the second sealing section 22 is pressed, the second sealing section 22 can be supported to a certain extent, so as to avoid the second sealing section 22 from being deformed too much and causing the structure to bulge.

[0057] In addition, the second sealing section 22 is made of sponge glue, that is, the second sealing section 22 has a stronger flexible deformation ability than the first sealing section 21 and the plug-in part 1. In this way, when the second sealing section 22 contacts the cabin body 200, the second sealing section 22 can be deformed to a certain extent, so as to ensure that the second sealing section 22 has a larger contact area with the cabin body 200, thereby ensuring the contact stability and the sealing effect.

[0058] In some embodiments, the first sealing section 21 is formed with at least one dense glue deformation corner 23, that is, the dense glue deformation corner 23 can be arranged on the first sealing section 21, and the number of the dense glue deformation corner 23 can be one, two or more. Figures 1-3 As shown in FIG. 6, the first sealing section 21 is provided with one dense glue deformation corner 23. By arranging the dense glue deformation corner 23, the structural strength of the first sealing section 21 can be increased, thereby ensuring the structural stability of the first sealing part 2.

[0059] In addition, the second sealing section 22 is formed with at least one sponge glue deformation corner 24, that is, the sponge glue deformation corner 24 can be arranged on the second sealing section 22, and the number of the sponge glue deformation corner 24 can be one, two or more. Figures 1-3 As shown in FIG. 7, the second sealing section 22 is provided with one sponge glue deformation corner 24. By arranging the sponge glue deformation corner 24, the structural strength of the second sealing section 22 can be increased, thereby ensuring the structural stability of the second sealing part 2.

[0060] Therefore, by arranging the dense glue deformation corner 23 and the sponge glue deformation corner 24, the structural strength of the sealing part 2 can be increased, thereby preventing the sealing part 2 from bulging when the sealing part 2 is sealed between the cabin body 200 and the hatch 300, and improving the stability of the sealing strip 100.

[0061] In some embodiments, the dense rubber deformation angle 23 and the sponge rubber deformation angle 24 are distributed in the circumferential direction of the first deformation cavity 26, so that the dense rubber deformation angle 23 and the sponge rubber deformation angle 24 can be used to structurally reinforce the sealing part 2 at different positions in the circumferential direction, such as the dense rubber deformation angle 23 and the sponge rubber deformation angle 24 being located at the lower side of the first deformation cavity 26 and close to the plug-in fitting part 1. Figure 1

[0062] Therefore, the dense rubber deformation angle 23 and the sponge rubber deformation angle 24 can be used to collectively reinforce the sealing part 2, so that, as shown in FIG. 6, the shape of the sealing part 2 at the dense rubber deformation angle 23 and the sponge rubber deformation angle 24 is relatively stable, the side of the sealing part 2 away from the plug-in fitting part 1 is in contact with the cabin body 200 and forms an effective seal, and the sealing part 2 does not deform to the outside of the fitting position of the cabin door 300 and the cabin body 200, that is, the bulging problem of the sealing strip 100 is well solved. Figure 3

[0063] In some embodiments, the dense rubber deformation angle 23 and the sponge rubber deformation angle 24 are connected by an intermediate deformation angle 25, that is, as shown in FIG. 7, the dense rubber deformation angle 23, the intermediate deformation angle 25, and the sponge rubber deformation angle 24 are sequentially connected in the circumferential direction of the first deformation cavity 26, so that the dense rubber deformation angle 23, the intermediate deformation angle 25, and the sponge rubber deformation angle 24 are collectively used to structurally reinforce the sealing part 2, and as shown in FIG. 8, the intermediate deformation angle 25 can be made of dense rubber, so that the excessive deformation of the sealing part 2 can be more effectively reduced, and the stability of the sealing part 2 is ensured. Figures 1-3 Figure 1

[0064] In further embodiments, the dense rubber deformation angle 23 and the sponge rubber deformation angle 24 are both configured to protrude outward relative to the first deformation cavity 26. As shown in FIG. 9, the dense rubber deformation angle 23 protrudes outward relative to the first deformation cavity 26, the end of the dense rubber deformation angle 23 can be a rounded corner or a right angle, and the included angle between the two parts forming the dense rubber deformation angle 23 can be set to be less than or equal to 90°, so that the dense rubber deformation angle 23 protrudes inward toward the cabin door 300, and the right side of the dense rubber deformation angle 23 is in contact with the cabin door 300, so as to increase the fitting area of the sealing part 2 and the cabin door 300 and improve the structural stability. Figures 1-3 In addition, the sponge rubber deformation angle 24 protrudes outward relative to the first deformation cavity 26, the end of the sponge rubber deformation angle 24 can be a rounded corner or a right angle, and the included angle between the two parts forming the sponge rubber deformation angle 24 can be set to be less than or equal to 90°, so that the sponge rubber deformation angle 24 protrudes inward toward the cabin door 300, and further improves the structural strength of the sealing part 2 together with the dense rubber deformation angle 23.

[0065]

[0066] ​​​​​And / or, the intermediate deformation angle 25 is configured to protrude inwardly relative to the first deformation cavity 26, as shown in Figures 1-3 As shown, the intermediate deformation angle 25 is located between the dense rubber deformation angle 23 and the sponge rubber deformation angle 24, and protrudes in the opposite direction, so that the part of the sealing portion 2 with the deformation angle is configured in a stepped manner, forming a multi-layer structure reinforcement, and as shown in Figure 3 As shown, after the sealing portion 2 is pressed against the cabin body 200, the stepped part can maintain a stable structure state, and the sealing portion 2 will not be excessively deformed to form a bulge.

[0067] In some embodiments, a second deformation cavity 11 is formed in the plug-in fitting portion 1, that is, the plug-in fitting portion 1 is also configured to have a hollow cavity. In other words, when the plug-in fitting portion 1 is installed and fitted with the hatch door 300, the plug-in fitting portion 1 can be quickly installed with the hatch door 300 through structural deformation, which facilitates to improve installation efficiency, and the elastic deformation of the plug-in fitting portion 1 towards the second deformation cavity 11 can be used to maintain the installation stability with the hatch door 300.

[0068] Specifically, as shown in Figure 2 and Figure 3 When actually installed, the hatch door 300 can be formed with a connecting slot 301, and the plug-in fitting portion 1 can be extended into the connecting slot 301 to be tightly fitted with the inner wall of the connecting slot 301, so that the plug-in fitting portion 1 is maintained in the connecting slot 301 to achieve the installation and fixation of the sealing strip 100 with the hatch door 300. Thus, when the plug-in fitting portion 1 is extended into the connecting slot 301, the deformation of the second deformation cavity 11 can be used to quickly enable the plug-in fitting portion 1 to enter the connecting slot 301, and after plugging, the elastic force of the second deformation cavity 11 can be used to maintain the plug-in fitting portion 1 in the connecting slot 301, which is simple in structure and convenient to install.

[0069] In some embodiments, the inner cavity volume of the second deformation cavity 11 is smaller than the inner cavity volume of the first deformation cavity 26, that is, the collapse deformation amount of the sealing portion 2 towards the first deformation cavity 26 is greater than the collapse deformation amount of the plug-in fitting portion 1 towards the first deformation cavity 26. Thus, the sealing portion 2 can generate sufficient deformation to achieve effective sealing with the cabin body 200, increase the sealing area of the two fittings, and improve the sealing performance. At the same time, the plug-in fitting portion 1 can be deformed towards the first deformation cavity 26 to achieve quick installation, and can also avoid excessive deformation of the plug-in fitting portion 1 to prevent the sealing strip 100 from automatically coming out relative to the hatch door 300.

[0070] In some embodiments, the plug-in fitting portion 1 is formed with a clamping protrusion 12, which is used to be clamped and connected with the first mounting member, that is, as shown in Figures 2-5As shown, after the plug-in part 1 is inserted into the connecting slot 301, the clamping protrusions 12 can be abutted with the inner wall of the connecting slot 301 to stably install the plug-in part 1 in the connecting slot 301, and realize the clamping fixation of the sealing strip 100 and the hatch door 300.

[0071] Specifically, as shown in the drawings, Figure 1 the clamping protrusions 12 are arranged on the surface of the plug-in part 1, and as shown in the drawings, Figure 2 and Figure 3 the clamping protrusions 12 are inclined relative to the plug-in direction of the plug-in part 1 to form a barb structure on the surface of the plug-in part 1, thereby increasing the friction force of the plug-in part 1 and improving the connection stability.

[0072] In some embodiments, the plug-in part 1 is provided with at least one clamping protrusion 12 on each of the two sides facing away from each other, that is, the plug-in part 1 is provided with clamping protrusions 12 on both sides in the plug-in direction. Specifically, as shown in the drawings, Figure 2 and Figure 3 the clamping protrusions 12 can be inserted into the connecting slot 301 from the lower left to the upper right in the drawings, and the clamping protrusions 12 are arranged on the upper left side and the lower right side of the plug-in part 1, and the clamping protrusions 12 on each side can be provided as two, so that after the clamping protrusions 12 are clamped into the connecting slot 301, they can be clamped and fixed with the inner walls of the two opposite sides of the connecting slot 301, thereby improving the cooperation stability between the sealing strip 100 and the hatch door 300.

[0073] In some embodiments, the plug-in part 1 can be provided with a fiber line 3 to ensure the structural stability of the sealing strip 100.

[0074] The utility model also provides a cabin equipment.

[0075] According to the cabin equipment provided by the utility model, the cabin equipment comprises a cabin 200, a hatch door 300 and the sealing strip 100 of any one of the above embodiments, the cabin 200 is formed with a hatch opening 201, the hatch door 300 is installed on the cabin 200, the hatch door 300 moves along a first direction relative to the cabin 200 to open or close the hatch opening 201, the plug-in part 1 is connected to the hatch door 300 along a second direction, and the sealing part 2 is abutted and pressed on the cabin 200, the sealing strip 100 can be stably installed on the hatch door 300 and is not prone to falling off. That is, after the sealing strip 100 is applied to the cabin equipment, the sealing strip 100 is fixed relative to the hatch door 300, when the hatch door 300 is closed relative to the cabin 200, the hatch door 300 can be closed relative to the cabin 200, and the sealing strip 100 provided above can not only ensure the sealing effect, but also avoid the bulging phenomenon of the sealing strip 100.

[0076] Specifically, as shown in the drawings, Figures 2-5As shown, the hatch 300 has a connecting slot 301. The insertion and mating part 1 of the sealing strip 100 is inserted and mated with the connecting slot 301 in the second direction, so that the sealing strip 100 is snapped onto the hatch 300. When the hatch 300 is closed relative to the cabin 200, it forms a certain closing angle and is combined with... Figure 2 and Figure 3 As shown, after the hatch 300 is closed relative to the cabin body 200, the sealing part 2 deforms at the position where it mates with the cabin body 200 to achieve a sealing fit. It maintains a stable structural state at both the solid adhesive deformation angle 23 and the sponge adhesive deformation angle 24. The setting of the solid adhesive deformation angle 23 and the sponge adhesive deformation angle 24 ensures that the sealing part 2 does not deform excessively and extend beyond the cabin body 200 and the hatch 300. Thus, it can effectively avoid the formation of sealing bulges on the outside of the cabin body 200 and the hatch 300, improving the aesthetics of the UAV cabin at the hatch 300.

[0077] The hatch 300 has a rectangular plate-like structure, and the hatch 200 has a hatch 201. The hatch 300 is used to seal the hatch 201. The sealing strip 100 extends along the circumference of the hatch 300 and can seal the hatch 300 at various positions along the circumference.

[0078] And, such as Figure 6 As shown, the hatch 201 of the UAV cabin opens upwards, and there are two hatches 300, located on the top sides of the hatch 201, allowing selective opening or closing of both sides of the hatch 201. Simultaneously, two sealing strips 100 are also constructed, and each sealing strip 100 is installed between the two hatches 300 and the cabin body 200, respectively. In actual design, if... Figure 6 As shown, one sealing strip 100 on the left can be constructed as an open ring, and one sealing strip 100 on the right can be constructed as a ring. Under the joint sealing action of the two sealing strips 100, it is beneficial to ensure the airtightness of the hatch 201.

[0079] And such as Figure 2 and Figure 3 As shown, a sealing strip 100 located on the left side can be configured to have a deformation angle, and, as... Figure 4 and Figure 5 As shown, a sealing strip 100 located on the right side can be constructed with no deformation angle, which can meet the requirements of installation and sealing. The structure is simple and the setting is flexible.

[0080] In some embodiments, the deformation angle is located on the side of the sealing strip 100 facing inwards towards the chamber 200, that is, both the solid adhesive deformation angle 23 and the sponge adhesive deformation angle 24 are located on the side of the sealing strip 100 facing inwards towards the chamber 200. Specifically, as Figure 2 and Figure 3As shown, the upper left side of the figure is the outer side of the hatch 300, and the lower right side of the figure is the inner side of the hatch 300, when the hatch 300 is closed relative to the cabin body 200, the cabin body 200 extrudes the sealing part 2 outward, and the sealing part 2 is deformed to form a sealing fit surface 221, the sealing fit surface 221 is pressed and fitted with the cabin body 200, accurate sealing is realized, at the same time, the dense rubber deformation angle 23 and the sponge rubber deformation angle 24 maintain a stable structure state, and can support the sealing part 2 to a certain extent, avoiding the sealing part 2 from protruding outward to the hatch 300 to form a bulge.

[0081] The utility model discloses still propose a kind of vehicle.

[0082] According to the vehicle of the utility model embodiment, the cabin body equipment of any one of the above embodiments is included, and the cabin body equipment is configured as a UAV cabin.

[0083] The sealing strip 100 can be prevented from forming a bulge, and the external structure of the UAV cabin is regular, and the overall appearance is improved.

[0084] In the description of the present specification, the description of the terms "one embodiment", "some embodiments", "illustrative embodiment", "example", "specific example" or "some examples" means that the specific features, structures, materials or characteristics described in conjunction with the embodiment or example are included in at least one embodiment or example of the utility model. In the present specification, the illustrative description of the above terms does not necessarily refer to the same embodiment or example. Moreover, the specific features, structures, materials or characteristics described can be combined in any one or more embodiments or examples in a suitable manner.

[0085] Although the embodiments of the utility model have been shown and described, those skilled in the art can understand that various changes, modifications, replacements and variations can be made to these embodiments without departing from the principles and purposes of the utility model, and the scope of the utility model is defined by the claims and their equivalents.

Claims

1. A weather strip, characterized by The sealing strip is adapted to be mounted at the joint of the first mounting member and the second mounting member, and the first mounting member and the second mounting member are mounted in cooperation along a first direction; The sealing strip comprises a plug-in cooperation part (1) and a sealing part (2), the sealing part (2) is used to be sealed and pressed against the second mounting member, a first deformation cavity (26) is formed in the sealing part (2), the plug-in cooperation part (1) is used to be connected to the first mounting member along a second direction, and the second direction intersects the first direction.

2. The weather strip of claim 1, wherein The included angle between the first direction and the second direction is less than or equal to 90° and greater than 45°.

3. The weather strip of claim 1, wherein The sealing part (2) comprises a first sealing section (21) and a second sealing section (22), the first sealing section (21) is connected to the plug-in cooperation part (1), the second sealing section (22) is connected to the first sealing section (21) and cooperatively defines the first deformation cavity (26), and the second sealing section (22) and / or the first sealing section (21) is formed with a deformation angle.

4. The weather strip of claim 3, wherein The first sealing section (21) and the plug-in cooperation part (1) are made of dense glue; And / or, the second sealing section (22) is made of sponge glue.

5. The weather strip of claim 4, wherein The first sealing section (21) is formed with at least one dense glue deformation angle (23); And / or, the second sealing section (22) is formed with at least one sponge glue deformation angle (24).

6. The weather strip of claim 5, wherein The dense glue deformation angle (23) and the sponge glue deformation angle (24) are distributed in the circumferential direction of the first deformation cavity (26).

7. The weather strip of claim 5 wherein, The dense glue deformation angle (23) and the sponge glue deformation angle (24) are connected with an intermediate deformation angle (25).

8. The weather strip of claim 7, wherein The dense glue deformation angle (23) and the sponge glue deformation angle (24) are both configured to protrude outward relative to the first deformation cavity (26); And / or, the intermediate deformation angle (25) is configured to protrude inward relative to the first deformation cavity (26).

9. The weather strip according to any one of claims 1 to 8, characterized in that The plug-in cooperation part (1) is formed with a second deformation cavity (11).

10. The weather strip of claim 9, wherein The inner cavity volume of the second deformation cavity (11) is less than the inner cavity volume of the first deformation cavity (26).

11. The weather strip according to any one of claims 1 to 8, characterized in that The plug-in cooperation part (1) is formed with a clamping protruding rib (12) used to be clamped and connected to the first mounting member.

12. The weather strip of claim 11, wherein The plug-in cooperation part (1) is provided with at least one clamping protruding rib (12) on each of two mutually opposite sides.

13. A pod apparatus, characterized by, A cabin device comprising a cabin body (200), a cabin door (300) and the sealing strip according to any one of claims 1-12, the cabin body (200) is formed with a hatch (201) therein, the cabin door (300) is mounted to the cabin body (200), and the cabin door (300) is adapted to move relative to the cabin body (200) along the first direction to open or close the hatch (201), the cabin door (300) is provided with a connecting slot (301), the plug-in cooperation part (1) is plugged and cooperated with the connecting slot (301) along the second direction, and the sealing part (2) is sealed and pressed against the cabin body (200).

14. A vehicle characterized by comprising: The cabin device according to claim 13 is configured as a drone cabin.

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