Machine body frame and clothes treating equipment

Abstract

The utility model is suitable for the technical field of household appliances, and provides a machine body frame and clothes treatment equipment. The machine body frame comprises a front door plate, a front supporting piece, a connecting piece and a rear back plate, and the front door plate, the front supporting piece and the rear back plate are sequentially arranged in the first direction; the front door plate is connected with the front supporting piece; the connecting piece is connected between the front supporting piece and the rear back plate in the first direction. The arranged front supporting piece serves as a middle connecting part of the front door plate and the rear back plate, the connecting effect is achieved, meanwhile, stress can be dispersed, and large pressure and pulling force can be borne, so that it is guaranteed that the shape and the structure of the fuselage frame are kept stable, and the rigidity of the overall structure of the fuselage frame is effectively improved. The arranged connecting pieces have the connecting and reinforcing effects, the whole fuselage frame can work cooperatively, and the connecting pieces are cooperatively matched with the front supporting pieces and the rear back plate, so that the structural strength and stability of the fuselage frame are effectively enhanced.

Description

TECHNICAL FIELD

[0001] The present application belongs to the technical field of household appliances, and more particularly relates to a machine body frame and a clothes processing device. BACKGROUND

[0002] The clothes processing device is a device for performing various processing operations on clothes. In the related art, the clothes processing device includes a machine body frame and various components installed inside the machine body frame, wherein the machine body frame includes a front door plate, a rear support plate, and a connecting piece, the front door plate and the rear support plate are arranged at intervals, and are connected through the connecting piece.

[0003] However, the above-mentioned machine body frame has certain defects, and the structural strength is insufficient. This defect in strength can cause the machine body frame to deform during the operation of the clothes processing device, thereby affecting the normal operation of the clothes processing device. UTILITY MODEL CONTENT

[0004] The purpose of the embodiments of the present application is to provide a machine body frame and a clothes processing device, aiming to solve the technical problem of insufficient structural strength of the machine body frame in the related art.

[0005] To achieve the above-mentioned purpose, according to one aspect of the present application, a machine body frame is provided, comprising a front door plate, a front support piece, a connecting piece, and a rear back plate, wherein the front door plate, the front support piece, and the rear back plate are arranged in sequence along a first direction; the front door plate is connected with the front support piece; the connecting piece is connected between the front support piece and the rear back plate along the first direction.

[0006] Optionally, the connecting piece is connected with the front support piece and / or the rear back plate through a fastener.

[0007] Optionally, one of the connecting piece and the front support piece is provided with a first limiting block, and the other is provided with a first limiting slot; the connecting piece is limited on the front support piece by being threaded into the first limiting slot through the first limiting block.

[0008] Optionally, the first limiting block is arranged on the front support piece, and the first limiting slot is arranged on the connecting piece; the first limiting block has two first limiting surfaces arranged at intervals along a second direction, the first limiting surfaces block the movement of the connecting piece along the second direction by contacting the slot wall of the first limiting slot; the first limiting block further has a second limiting surface, the direction from the first limiting surface to the second limiting surface is a third direction, and the first direction, the second direction, and the third direction are perpendicular to each other; the second limiting surface blocks the movement of the connecting piece along the third direction by contacting the slot bottom of the first limiting slot.

[0009] Optionally, a second limiting block is further arranged on the front support piece, and the second limiting block is located on one side of the first limiting block in the third direction; the connecting piece is clamped between the first limiting block and the second limiting block in the third direction.

[0010] Optionally, the second limiting block comprises two limiting protrusions, which are arranged at intervals along the second direction.

[0011] Optionally, one of the connecting member and the back plate is provided with a third limiting block, and the other is provided with a second limiting slot; the connecting member is limited on the back plate by being inserted into the second limiting slot through the third limiting block.

[0012] Optionally, the third limiting block is arranged on the connecting member, and the second limiting slot is arranged on the back plate; the back plate has a mounting plate, part of the structure on the mounting plate is arranged protruding towards the front support along the first direction, and a limiting gap is formed between the surface of the mounting plate close to the front support; the third limiting block can be inserted into the limiting gap along the third direction, and the surface of the mounting plate away from the front support blocks the third limiting block from moving along the second direction by contacting the third limiting block; the limiting gap is formed as the second limiting slot.

[0013] Optionally, the machine body frame further comprises a base, a side plate and a top plate, the base, the side plate, the top plate, the front door plate and the back plate enclose to form a cuboid structure of the machine body frame.

[0014] Optionally, one of the side plate and the base is provided with a fourth limiting block, and the other is provided with a third limiting slot; the side plate is limited on the base by being inserted into the third limiting slot through the fourth limiting block.

[0015] Optionally, the machine body frame further comprises a reinforcing member, which extends along the third direction and is connected with the front door plate, the front support and the side plate.

[0016] According to another aspect of the present application, a laundry treating apparatus is provided, comprising a drum and the above-mentioned machine body frame, the drum being installed in the machine body frame, and the drum being provided with a connecting member at least on one side along the third direction.

[0017] Optionally, the drum has a middle section perpendicular to the second direction, and the connecting member is located above the middle section.

[0018] The fuselage frame provided by the application has the beneficial effects that in the application, the front support and the rear back plate are used in cooperation to resist external force, thereby preventing the fuselage frame from deforming. The front support arranged as an intermediate connecting component of the front door plate and the rear back plate not only plays a connecting role, but also can disperse stress and bear greater pressure and tension, thereby ensuring that the shape and structure of the fuselage frame remain stable and effectively improving the rigidity of the overall structure of the fuselage frame. The connecting component not only plays a connecting and reinforcing role, but also enables the entire fuselage frame to work in cooperation, and cooperates with the front support and the rear back plate to effectively enhance the structural strength and stability of the fuselage frame. Meanwhile, when the fuselage frame is subjected to uneven force (such as greater pressure at one end), the connecting component can effectively disperse the force to each component, thereby avoiding that a single component bears excessive stress and effectively improving the anti-deformation capability of the fuselage frame. BRIEF DESCRIPTION OF DRAWINGS

[0019] In order to more clearly illustrate the technical solutions in the embodiments of the present application, the drawings needed to be used in the embodiments or prior art description will be briefly introduced. Obviously, the drawings in the following description are only some embodiments of the present application, and other drawings can be obtained by those skilled in the art without creative labor.

[0020] Figure 1 The structural schematic diagram of the laundry treating apparatus provided by the embodiment of the present application is shown in the figure.

[0021] Figure 2 The structural schematic diagram of the fuselage frame provided by the embodiment of the present application is shown in the figure.

[0022] Figure 3 The structural schematic diagram of the fuselage frame provided by the embodiment of the present application is shown in the figure. Figure 2 The enlarged schematic diagram of A in the figure.

[0023] Figure 4 The structural schematic diagram of the fuselage frame provided by the embodiment of the present application is shown in the figure.

[0024] Figure 5 The structural schematic diagram of the fuselage frame provided by the embodiment of the present application is shown in the figure. Figure 4 The enlarged schematic diagram of C in the figure.

[0025] Figure 6 The structural schematic diagram of the fuselage frame provided by the embodiment of the present application is shown in the figure.

[0026] Figure 7 The structural schematic diagram of the fuselage frame provided by the embodiment of the present application is shown in the figure. Figure 6 The enlarged schematic diagram of D in the figure.

[0027] Figure 8 The structural schematic diagram of the fuselage frame provided by the embodiment of the present application is shown in the figure. Figure 6 The enlarged schematic diagram of E in the figure.

[0028] Figure 9 A structure schematic view of a top plate hidden behind a body frame with a roller in a first perspective view is provided for the embodiment of the present application.

[0029] Figure 10 A structure schematic view of a top plate hidden behind a body frame with a roller in a second perspective view is provided for the embodiment of the present application.

[0030] Figure 11 A structure schematic view of a side plate is provided for the embodiment of the present application. Figure 2 An enlarged schematic view of the middle B.

[0031] Figure 12 A structure schematic view of a top plate is provided for the embodiment of the present application.

[0032] The label details involved in the above-mentioned drawings are as follows:

[0033] 100, front door plate; 200, front support; 210, first limiting block; 211, first limiting surface; 212, second limiting surface; 220, second limiting block; 221, limiting protrusion;

[0034] 300, connecting piece; 310, first limiting groove; 320, third limiting block; 400, back plate; 410, mounting plate; 411, second limiting groove;

[0035] 500, base; 510, fourth limiting block; 600, side plate; 610, third limiting groove; 700, top plate; 800, reinforcing piece; 900, roller. DETAILED DESCRIPTION

[0036] In order to make the technical problems to be solved by the present application, the technical solutions and beneficial effects more clearly understood, the present application will be further described in detail below with reference to the drawings and embodiments. It should be understood that the specific embodiments described herein are only used to explain the present application and not used to limit the present application.

[0037] It should be noted that when an element is referred to as being "fixed to" or "disposed on" another element, it can be directly on the other element or indirectly on the other element. When an element is referred to as being "connected to" another element, it can be directly connected to the other element or indirectly connected to the other element. The embodiments in the present application and the features in the embodiments can be combined with each other without conflict. The present application will be described in detail below with reference to the drawings and in combination with the embodiments.

[0038] It should be understood that the terms "length", "width", "upper", "lower", "front", "back", "left", "right", "vertical", "horizontal", "top", "bottom", "inner", "outer" and the like indicate directions or positions based on the directions or positions shown in the drawings, and are used only for the purpose of facilitating this application and simplifying the description, and do 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 limiting the application.

[0039] In addition, the terms "first", "second" are only for descriptive purposes and cannot be understood as indicating or implying relative importance or implicitly indicating the number of the technical features indicated. Therefore, the features defined as "first", "second" can explicitly or implicitly include one or more of the features. In the description of the application, the meaning of "multiple" is more than two, unless otherwise explicitly and specifically limited.

[0040] As described in the background, the laundry treating apparatus is an apparatus for performing various treating operations on laundry. In the related art, the laundry treating apparatus includes a body frame and various components installed inside the body frame, wherein the body frame includes a front door panel, a rear support panel, and a connection member, the front door panel and the rear support panel are spaced apart and connected by the connection member. However, the above-mentioned body frame has certain defects, and the structural strength is insufficient. This defect in strength can cause the body frame to deform during the operation of the laundry treating apparatus, thereby affecting the normal operation of the laundry treating apparatus.

[0041] Referring to Figure 1 and Figure 2 , in order to solve the above-mentioned problems, according to one aspect of the present application, the embodiments of the present application provide a body frame, which includes a front door panel 100, a front support member 200, a connection member 300, and a rear back panel 400, wherein the front door panel 100, the front support member 200, and the rear back panel 400 are sequentially arranged along a first direction; the front door panel 100 is connected with the front support member 200; the connection member 300 is connected between the front support member 200 and the rear back panel 400 along the first direction.

[0042] In the embodiments of the present application, the body frame is used in a laundry treating apparatus. The front door panel 100 is provided with an openable and closable door; the front support member 200 is a support frame or a support frame, which is fixedly connected with the front door panel 100; the rear back panel is a support member located at the last end in the body frame. The connection member 300 is a connection strip, which is fixedly connected with the front support member 200 and the rear back panel 400; the first direction is parallel to the length direction of the body frame; in other embodiments, the first direction can also be parallel to the width direction or the height direction of the body frame.

[0043] In the present application, the front support 200 and the rear back plate 400 are used in cooperation to resist external force, thereby preventing the deformation of the fuselage frame. The front support 200 is arranged as an intermediate connecting component of the front door plate 100 and the rear back plate 400, which not only plays a connecting role, but also can disperse stress and bear greater pressure and tension, thereby ensuring that the shape and structure of the fuselage frame remain stable and effectively improving the rigidity of the overall structure of the fuselage frame. The connecting component 300 not only plays a connecting and reinforcing role, enabling the entire fuselage frame to work in cooperation, but also cooperates with the front support 200 and the rear back plate 400 to effectively enhance the structural strength and stability of the fuselage frame; at the same time, when the fuselage frame is subjected to uneven force (such as greater pressure at one end), the connecting component 300 can effectively disperse the force to each component, avoiding that a single component bears excessive stress, thereby effectively improving the anti-deformation ability of the fuselage frame.

[0044] With reference to Figure 2 and Figure 3 In an embodiment, the connecting component 300 is connected with the front support 200 through a fastener. In the present embodiment, the fastener is a fastening screw, a fastening bolt or a fastening pin; the above-mentioned connecting mode reduces the assembly difficulty and cost of the connecting component 300 and the front support 200. In other embodiments, the connecting component 300 and the front support 200 can also be fixedly connected through a welding mode, a plug-in mode or a clamping mode.

[0045] With reference to Figure 4 and Figure 5 In an embodiment, the connecting component 300 is connected with the rear back plate 400 through a fastener. In the present embodiment, the fastener is a fastening screw, a fastening bolt or a fastening pin; the above-mentioned connecting mode reduces the assembly difficulty and cost of the connecting component 300 and the rear back plate 400. In other embodiments, the connecting component 300 and the rear back plate 400 can also be fixedly connected through a welding mode, a plug-in mode or a clamping mode.

[0046] With reference to Figure 2 , Figure 3 , Figure 6 and Figure 7 In an embodiment, one of the connecting component 300 and the front support 200 is provided with a first limiting block 210, and the other is provided with a first limiting groove 310; the connecting component 300 is limited on the front support 200 by being inserted into the first limiting groove 310 through the first limiting block 210.

[0047] In the embodiment, the first limiting block 210 can be arranged on the front support 200, and the first limiting slot 310 can be arranged on the connecting piece 300. The first limiting block 210 and the first limiting slot 310 used in cooperation in the application not only have a limiting effect, but also can limit the relative displacement of the connecting piece 300 and the front support 200, thereby ensuring the stability of the connection between the connecting piece 300 and the front support 200. Meanwhile, the first limiting block 210 and the first limiting slot 310 can also realize accurate positioning between the connecting piece 300 and the front support 200. Specifically, during the assembly of the fuselage frame, the operator can quickly and accurately determine the relative position of the connecting piece 300 and the front support 200 by inserting the first limiting block 210 into the first limiting slot 310, and then the connecting piece 300 and the front support 200 can be smoothly and conveniently connected by using fasteners, thereby greatly improving the assembly efficiency. In addition, the first limiting block 210 and the first limiting slot 310 used in cooperation are also convenient to operate and reduce the operation difficulty.

[0048] With reference to Figure 2 , Figure 3 , Figure 6 and Figure 7 , in an embodiment, the first limiting block 210 is arranged on the front support 200, and the first limiting slot 310 is arranged on the connecting piece 300; the first limiting block 210 has two first limiting surfaces 211 arranged at intervals in the second direction, and the first limiting surface 211 blocks the movement of the connecting piece 300 in the second direction by contacting the slot wall of the first limiting slot 310.

[0049] The first limiting block 210 also has a second limiting surface 212, the direction of the first limiting surface 211 to the second limiting surface 212 is a third direction, and the first direction, the second direction and the third direction are perpendicular to each other; the second limiting surface 212 blocks the movement of the connecting piece 300 in the third direction by contacting the slot bottom of the first limiting slot 310.

[0050] In the embodiment, the first limiting block 210 and the front support 200 are an integral piece; in other embodiments, the first limiting block 210 can also be an integral piece with the connecting piece 300, and at this time the first limiting slot 310 should be arranged on the front support 200. The second direction is parallel to the height direction of the fuselage frame, and the third direction is parallel to the length direction of the fuselage frame; in other embodiments, the second direction can also be parallel to the width direction or the length direction of the fuselage frame, and the third direction can also be parallel to the height direction or the width direction of the fuselage frame.

[0051] The number of the groove walls of the first limiting groove 310 is two, the two groove walls of the first limiting groove 310 are arranged in the second direction, and the two first limiting surfaces 211 are respectively arranged corresponding to the two groove walls of the first limiting groove 310. The second limiting surface 212 is arranged adjacent to the two first limiting surfaces 211, and the groove bottom of the first limiting groove 310 is arranged adjacent to the two groove walls of the first limiting groove 310; this design facilitates the first limiting block 210 to be arranged in the first limiting groove 310 in the third direction, and improves the convenience of operation.

[0052] The two first limiting surfaces 211 used in combination in the application and the groove walls of the two first limiting grooves 310 together limit the reciprocating movement of the connecting piece 300 on the front support 200 in the second direction; at the same time, the second limiting surface 212 used in combination and the groove bottom of the first limiting groove 310 limit the one-way movement of the connecting piece 300 on the front support 200 in the third direction. In addition, based on the design that the connecting piece 300 is connected between the front support 200 and the back plate 400 in the first direction, the connecting piece 300 is also limited to reciprocate on the front support 200 in the first direction. By adopting the above design, the relative displacement of the connecting piece 300 and the front support 200 in multiple directions can be limited, so that the connecting piece 300 can be stably limited on the front support 200, thereby ensuring the overall stability of the fuselage frame.

[0053] Referring to Figure 2 , Figure 3 and Figure 6 to Figure 8 In an embodiment, the front support 200 is also provided with a second limiting block 220, the second limiting block 220 is located on one side of the first limiting block 210 in the third direction; and the connecting piece 300 is clamped between the first limiting block 210 and the second limiting block 220 in the third direction.

[0054] In the embodiment, the second limiting block 220 is an integral part of the front support 200. The first limiting block 210 and the second limiting block 220 used in combination in the application together limit the reciprocating movement of the connecting piece 300 on the front support 200 in the third direction, which effectively prevents the connecting piece 300 from moving out of control in the third direction, and further enhances the stability of the connection between the connecting piece 300 and the front support 200. In addition, in order to ensure that the first limiting block 210 can be smoothly arranged in the first limiting groove 310, the first limiting groove 310 is a through groove arranged in the first direction.

[0055] Referring to Figure 7 and Figure 8In an embodiment, the second limiting block 220 comprises two limiting protrusions 221 which are arranged at intervals along the second direction. The two limiting protrusions 221 used in cooperation in the present application not only have the effect of double limiting, effectively preventing the connecting piece 300 from deviating along the third direction, but also reduce the manufacturing difficulty and cost. In addition, this design can also better disperse the stress, reduce local stress concentration, and improve the durability and service life of the limiting protrusion 221.

[0056] With reference to Figure 5 In an embodiment, one of the connecting piece 300 and the back plate 400 is provided with the third limiting block 320, and the other is provided with the second limiting slot 411; the connecting piece 300 is limited on the back plate 400 by the third limiting block 320 penetrating into the second limiting slot 411.

[0057] In the present embodiment, the third limiting block 320 can be arranged on the connecting piece 300, and the second limiting slot 411 can be arranged on the back plate 400. The third limiting block 320 and the second limiting slot 411 used in cooperation in the present application not only have the effect of limiting, which can limit the relative displacement of the connecting piece 300 and the back plate 400, thereby ensuring the stability of the connection between the connecting piece 300 and the back plate 400, but also can realize the precise positioning between the connecting piece 300 and the back plate 400; specifically, during the assembly of the fuselage frame, the operator can quickly and accurately determine the relative position of the connecting piece 300 and the back plate 400 by inserting the third limiting block 320 into the second limiting slot 411, and then the connecting piece 300 and the back plate 400 can be connected smoothly and conveniently by using fasteners, greatly improving the assembly efficiency. In addition, the third limiting block 320 and the second limiting slot 411 used in cooperation are also convenient to operate, reducing the operation difficulty.

[0058] With reference to Figure 5 In an embodiment, the third limiting block 320 is arranged on the connecting piece 300, and the second limiting slot 411 is arranged on the back plate 400; the back plate 400 has a mounting plate 410, and part of the structure on the mounting plate 410 is arranged protruding towards the front support 200 along the first direction, and forms a limiting gap with the surface of the mounting plate 410 close to the front support 200.

[0059] The third limiting block 320 can be inserted into the limiting gap along the third direction, and the surface of the mounting plate 410 away from the front support 200 blocks the third limiting block 320 from moving along the second direction by contacting the third limiting block 320; the limiting gap is formed as the second limiting slot 411.

[0060] In the embodiment, the third limiting block 320 is an integral part of the connecting piece 300; in other embodiments, the third limiting block 320 can also be an integral part of the rear back plate 400, in which case the second limiting slot 411 should be provided on the connecting piece 300. The third limiting block 320 and the second limiting slot 411 used in combination in the application jointly limit the reciprocating movement of the connecting piece 300 along the second direction and the one-way movement of the connecting piece 300 along the third direction on the rear back plate 400; in addition, based on the design that the connecting piece 300 is connected between the front support 200 and the rear back plate 400 along the first direction, the connecting piece 300 will also be limited to reciprocate along the first direction on the rear back plate 400. By adopting the above design, the relative displacement of the connecting piece 300 and the rear back plate 400 in multiple directions can be limited, so that the connecting piece 300 can be stably limited on the rear back plate 400, thereby ensuring the overall stability of the fuselage frame.

[0061] Referring to Figure 1 , Figure 9 and Figure 10 , in an embodiment, the fuselage frame further comprises a base 500, a side plate 600 and a top plate 700, and the base 500, the side plate 600, the top plate 700, the front door plate 100 and the rear back plate 400 enclose to form a cuboid structure of the fuselage frame.

[0062] In the embodiment, the base 500 is connected with the front door plate 100, the front support 200 and the rear back plate 400 through fasteners (such as fastening screws, fastening bolts or fastening pins); this design not only helps to form a stable connection system and improve the anti-deformation ability of the fuselage frame, but also facilitates installation and disassembly, thereby improving production efficiency and maintenance efficiency.

[0063] The number of side plates 600 is two, and the two side plates 600 are arranged in the third direction; the side plate 600 is connected with the front support 200, the rear back plate 400 and the base 500 through fasteners (such as fastening screws, fastening bolts or fastening pins); this design not only helps to form a stable connection system and improve the anti-deformation ability of the fuselage frame, but also facilitates installation and disassembly, thereby improving production efficiency and maintenance efficiency.

[0064] The top plate 700 and the base 500 are arranged in the second direction; the top plate 700 is connected with the reinforcing piece 800, the side plate 600 and the rear back plate 400 through fasteners (such as fastening screws, fastening bolts or fastening pins); this design not only helps to form a stable connection system and improve the anti-deformation ability of the fuselage frame, but also facilitates installation and disassembly, thereby improving production efficiency and maintenance efficiency. In addition, the base 500, the side plate 600, the top plate 700, the front door plate 100 and the rear back plate 400 enclose to form a closed three-dimensional structure.

[0065] The base 500, the side plate 600, the top plate 700, the front door plate 100 and the back plate 400 in the present application enclose a cuboid structure of the fuselage frame, and each component cooperates with each other to provide support and constraint from multiple directions. For example, when subjected to external impact force, the base 500 can stably support the weight of the entire fuselage frame and disperse the impact force, the side plate 600 resists the collision force from the side, the top plate 700 prevents the pressure from above from damaging the internal structure, and the front door plate 100 and the back plate 400 also participate in the overall force distribution, so that the fuselage frame can effectively resist external forces in various directions and maintain the stability of the structure. At the same time, the cuboid structure design makes the fuselage frame have balanced structural strength and good anti-deformation ability in three-dimensional space. In addition, the cuboid structure fuselage frame forms a regular space inside, which is convenient for reasonable arrangement and installation of various internal components. This regular space makes the layout of internal components more orderly, which is conducive to improving the space utilization rate.

[0066] Referring to Figure 1 , Figure 2 and Figure 9 to Figure 12 , in an embodiment, one of the side plate 600 and the base 500 is provided with the fourth limiting block 510, and the other is provided with the third limiting groove 610; the side plate 600 is limited on the base 500 by the fourth limiting block 510 penetrating into the third limiting groove 610.

[0067] In the present embodiment, the fourth limiting block 510 is an integral part of the base 500; in other embodiments, the fourth limiting block 510 can also be an integral part of the side plate 600, and at this time the third limiting groove 610 should be provided on the base 500. The fourth limiting block 510 and the third limiting groove 610 used in cooperation in the present application not only have a limiting effect, but also can limit the relative displacement of the side plate 600 and the base 500, thereby ensuring the stability of the connection between the side plate 600 and the base 500; at the same time, it can also realize the precise positioning between the side plate 600 and the base 500; specifically, during the assembly process of the fuselage frame, the operator can quickly and accurately determine the relative position of the side plate 600 and the base 500 by inserting the fourth limiting block 510 into the third limiting groove 610; then the side plate 600 and the base 500 can be smoothly and conveniently connected by using fasteners, greatly improving the assembly efficiency. In addition, the fourth limiting block 510 and the third limiting groove 610 used in cooperation are also convenient to operate, reducing the operation difficulty.

[0068] In addition, in order to ensure that the side plate 600 can be stably limited on the base 500, the number of the fourth limiting block 510 is multiple, and the multiple fourth limiting blocks 510 are arranged at intervals along the first direction; the number of the third limiting groove 610 is the same as that of the fourth limiting block 510, and the multiple fourth limiting blocks 510 are respectively arranged in one-to-one correspondence with the multiple third limiting grooves 610.

[0069] Referring to Figure 9 and Figure 10 In an embodiment, the body frame further comprises a reinforcing member 800, which extends along the third direction and is connected with the front door plate 100, the front support member 200 and the side plate 600.

[0070] In the embodiment, the reinforcing member 800 is located between the front door plate 100 and the back plate 400 and above the front support member 200. The reinforcing member 800 is connected with the front door plate 100, the front support member 200 and the side plate 600 by fasteners (such as fastening screws, fastening bolts or fastening pins).

[0071] When the body frame is subjected to external force in the third direction (such as impact from the side, vibration of internal components in the third direction, etc.), the reinforcing member 800 can effectively resist deformation; at the same time, the above-mentioned connection mode tightly combines multiple key components, greatly enhancing the overall rigidity of the body frame. In addition, as a connecting component, the reinforcing member 800 can effectively transmit the action force between the internal components of the body frame and the force from the outside, and can change the transmission path of the force, dispersing the stress to a larger area, thereby making the stress distribution more uniform.

[0072] Referring to Figure 1 to Figure 12 According to another aspect of the present application, the embodiments of the present application also provide a laundry treating apparatus, which comprises a drum 900 and the above-mentioned body frame, the drum 900 being installed in the body frame, and the drum 900 being provided with a connecting member 300 on at least one side along the third direction.

[0073] In the embodiments of the present application, the laundry treating apparatus is a clothes dryer; in other embodiments, the laundry treating apparatus can also be a washing machine or a dryer, etc. The connecting member 300 not only plays a connecting and reinforcing role, enabling the entire body frame to work cooperatively, but also cooperates with the front support member 200 and the back plate 400, effectively enhancing the structural strength and stability of the body frame; at the same time, it also plays a role of limiting the drum 900 from shaking randomly in the body frame, improving the stability of the drum 900 in the body frame; in addition, the connecting member 300 can also serve as a positioning point for installing the drum 900, and the operator can quickly and accurately install the drum 900 into the body frame by cooperating the connecting member 300 with the corresponding connecting part on the body frame; at the same time, when the drum 900 needs to be maintained (such as repairing the bearings, heating devices, etc. in the drum 900) or replaced, the presence of the connecting member 300 makes it more convenient to disassemble the drum 900.

[0074] In addition, in order to strengthen the connection, reinforcement and limiting, etc., the drum 900 is provided with a connecting member 300 on both sides along the third direction.

[0075] Referring to Figure 4 In an embodiment, the drum 900 has a middle section perpendicular to the second direction, and the connecting pieces 300 are located above the middle section. The above design helps to reduce the volume of the body frame in the third direction, thereby helping to reduce the overall volume of the body frame. In addition, for ease of disassembly, the two connecting pieces 300 are symmetrically arranged along the axis of the drum 900.

[0076] In summary, the body frame and the clothes processing apparatus provided by the embodiment have at least the following beneficial technical effects: In the present application, the front support 200 and the back plate 400 are used in cooperation to resist external force, thereby preventing the body frame from deforming. The front support 200 is arranged as an intermediate connecting component of the front door plate 100 and the back plate 400, which not only plays a connecting role, but also can disperse stress and bear greater pressure and tension, thereby ensuring that the shape and structure of the body frame remain stable, effectively improving the rigidity of the overall structure of the body frame. The connecting piece 300 not only plays a connecting and reinforcing role, enabling the entire body frame to work in cooperation, but also cooperates with the front support 200 and the back plate 400 to effectively enhance the structural strength and stability of the body frame; at the same time, when the body frame is subjected to uneven force (such as greater pressure at one end), the connecting piece 300 can effectively disperse the force to each component, avoiding that a single component bears excessive stress, thereby effectively improving the anti-deformation ability of the body frame.

[0077] The above is only a preferred embodiment of the present application and is not intended to limit the present application. Any modifications, equivalent replacements and improvements made within the spirit and principles of the present application shall be included in the protection scope of the present application.

Claims

1. A fuselage frame, characterized in that The door includes a front door plate (100), a front support (200), a connecting piece (300) and a back plate (400), wherein the front door plate (100), the front support (200) and the back plate (400) are sequentially arranged along a first direction; the front door plate (100) is connected with the front support (200); the connecting piece (300) is connected between the front support (200) and the back plate (400) along the first direction.

2. The fuselage frame of claim 1, wherein, The connecting piece (300) is connected with the front support (200) and / or the back plate (400) through a fastener.

3. The fuselage frame of claim 2, wherein, One of the connecting piece (300) and the front support (200) is provided with a first limiting block (210), and the other is provided with a first limiting groove (310); the connecting piece (300) is limited on the front support (200) by being threaded into the first limiting groove (310) through the first limiting block (210).

4. The fuselage frame of claim 3, wherein, The first limiting block (210) is arranged on the front support (200), and the first limiting groove (310) is arranged on the connecting piece (300); The first limiting block (210) has two first limiting surfaces (211) arranged at intervals along a second direction, and the first limiting surfaces (211) block the movement of the connecting piece (300) along the second direction by contacting the groove wall of the first limiting groove (310); The first limiting block (210) also has a second limiting surface (212), the direction from the first limiting surface (211) to the second limiting surface (212) is a third direction, and the first direction, the second direction and the third direction are perpendicular to each other; the second limiting surface (212) blocks the movement of the connecting piece (300) along the third direction by contacting the groove bottom of the first limiting groove (310).

5. The fuselage frame of claim 4, wherein, The front support (200) is also provided with a second limiting block (220), and the second limiting block (220) is located on one side of the first limiting block (210) in the third direction; The connecting piece (300) is clamped between the first limiting block (210) and the second limiting block (220) on both sides in the third direction.

6. The fuselage frame of claim 5, wherein, The second limiting block (220) includes two limiting protrusions (221) arranged at intervals along the second direction.

7. The fuselage frame of claim 4, wherein, One of the connecting piece (300) and the back plate (400) is provided with a third limiting block (320), and the other is provided with a second limiting groove (411); the connecting piece (300) is limited on the back plate (400) by being threaded into the second limiting groove (411) through the third limiting block (320).

8. The fuselage frame of claim 7, wherein, The third limiting block (320) is arranged on the connecting piece (300), and the second limiting groove (411) is arranged on the back plate (400); The back plate (400) has a mounting plate (410), part of the structure on the mounting plate (410) is arranged protruding towards the front support (200) along the first direction, and forms a limiting gap between the surface of the mounting plate (410) close to the front support (200); The third limiting block (320) can be inserted into the limiting gap along the third direction, the surface of the mounting plate (410) away from the front support (200) blocks the third limiting block (320) from moving along the second direction by contacting the third limiting block (320); the limiting gap is formed as the second limiting slot (411).

9. The fuselage frame of any of claims 4 to 8, characterized in that The fuselage frame further comprises a base (500), a side plate (600) and a top plate (700), the base (500), the side plate (600), the top plate (700), the front door plate (100) and the back plate (400) form a cuboid structure fuselage frame.

10. The fuselage frame of claim 9, wherein, One of the side plate (600) and the base (500) is provided with a fourth limiting block (510), and the other is provided with a third limiting slot (610); the side plate (600) is limited on the base (500) by penetrating the fourth limiting block (510) into the third limiting slot (610).

11. The fuselage frame of Claim 9, wherein, The fuselage frame further comprises a reinforcing member (800), the reinforcing member (800) extends along the third direction and is connected with the front door plate (100), the front support (200) and the side plate (600). 12.A laundry treating apparatus, characterized by, The fuselage frame comprises a drum (900) and the fuselage frame of any one of claims 4 to 11, the drum (900) is installed in the fuselage frame, and the drum (900) is provided with the connecting member (300) on at least one side along the third direction. 13.The laundry treating apparatus of claim 12, wherein The drum (900) has a middle section perpendicular to the second direction, and the connecting member (300) is located above the middle section. The drum (900) has a middle section perpendicular to the second direction, and the connecting member (300) is located above the middle section.

Images