Unit cabin and container

Abstract

The utility model provides a unit cabin and a container. The unit cabin comprises a cabin body, a cabin door and a sealing plate assembly. The cabin body is provided with a containing cavity used for containing unit equipment, and in the state that the cabin body contains the unit equipment, a gap area is formed between the periphery of the unit equipment and the containing cavity; the cabin door is connected to the cabin body; the sealing plate assembly is connected to the back of the cabin door. The sealing plate assembly comprises a first sealing plate and a second sealing plate; the first sealing plate and the second sealing plate are used for abutting against the unit equipment, and the first sealing plate, the second sealing plate and the end face of the unit equipment form a closed structure so as to cut off communication between the gap area and the external environment. According to the unit cabin disclosed by the utility model, even if foreign matters such as mice, insects and the like enter the unit cabin through the cabin door, the foreign matters can be blocked by the closed structure and cannot enter the unit equipment, so that the influence of the foreign matters on the operation and safety of the unit equipment is eliminated.

Description

Technical Field

[0001] The utility model generally relates to the technical field of container structures, and more specifically to a crew cabin and a container. Background Art

[0002] Liquid cooling units are currently widely used in energy storage equipment. Through a liquid cooling system, the circulating coolant absorbs the heat generated by the battery during charging and discharging, and dissipates it into the environment, thereby maintaining the normal operating temperature of the battery and improving the battery life and performance. In order to meet the requirements of external heat exchange of the liquid cooling unit, a separate area is generally set up in the energy storage box as a liquid cooling unit cabin. The refrigeration system of the energy storage box liquid cooling unit relies on an air-cooled condenser to exchange heat with the external environment. Therefore, the liquid cooling unit cabin is generally set up as an open structure to facilitate heat exchange of the liquid cooling unit. However, the open structure is not protected against small foreign objects such as mice and insects, which can freely enter and exit the liquid cooling unit cabin, which may pose a threat to the operation and safety of the equipment.

[0003] Therefore, it is necessary to provide a crew cabin and a container to at least partially solve the above problems. Utility Model Content

[0004] A series of simplified concepts are introduced in the utility model content section, which will be further described in detail in the detailed implementation section. The utility model content section of the utility model does not mean to attempt to define the key features and essential technical features of the technical solution claimed for protection, nor does it mean to attempt to determine the scope of protection of the technical solution claimed for protection.

[0005] In order to at least partially solve the above problems, the first aspect of the present invention provides a crew cabin for accommodating crew equipment, the crew cabin comprising:

[0006] A cabin body, the cabin body having a receiving cavity for receiving the unit equipment, wherein when the cabin body receives the unit equipment, a gap area is formed between the outer periphery of the unit equipment and the receiving cavity;

[0007] a hatch connected to the cabin;

[0008] A sealing plate assembly, the sealing plate assembly is connected to the back side of the cabin door, and the sealing plate assembly comprises:

[0009] a first sealing plate, two of the first sealing plates being spaced apart along a height direction of the crew cabin;

[0010] a second sealing plate, wherein two of the second sealing plates are spaced apart along a first direction perpendicular to a height direction of the crew compartment;

[0011] The first sealing plate and the second sealing plate are used to abut against the unit equipment, and the first sealing plate, the second sealing plate and the end surface of the unit equipment form a closed structure to cut off the communication between the gap area and the external environment.

[0012] Optionally, the first sealing plate and the second sealing plate are configured to be adjustable so as to cover the gap area.

[0013] Optionally, the hatch is openably connected to the cabin body, and the hatch comprises:

[0014] A door body, wherein the door body has an air inlet and an air outlet communicating with the external environment;

[0015] a door frame connected to the outer periphery of the door body;

[0016] A fixing member, the fixing member being connected to the door frame and close to the back side of the door body, the sealing plate assembly being connected to the fixing member;

[0017] The crew compartment further includes a position-limiting member, which is detachably connected to at least one of the fixing member and the sealing plate assembly, and is used to fix the position of the sealing plate assembly after adjustment.

[0018] Optionally, the fixing member has an assembly hole, the sealing plate assembly has an adjustment hole corresponding to the position of the assembly hole, and the limiting member is detachably connected to the assembly hole and the adjustment hole to adjust the position of the sealing plate assembly relative to the fixing member.

[0019] Optionally, the fixing member comprises:

[0020] a first connection portion, the first connection portion being connected to the door frame;

[0021] A first bending portion, wherein the first bending portion and the first connecting portion are integrally formed, and the first bending portion is connected to the sealing plate assembly.

[0022] Optionally, the cabin door further comprises:

[0023] An air duct component, the air duct component is connected to the air inlet and outlet and communicates with the external environment, and the air duct component has a sealing portion to ensure the sealing degree of the connection between the air duct component and the air inlet and outlet;

[0024] A filter component is connected to the air inlet and outlet.

[0025] Optionally, the crew cabin further includes:

[0026] a first sealing member connected to the first sealing plate;

[0027] a second sealing member connected to the second sealing plate;

[0028] When the cabin door is in a closed state, the first sealing member abuts against the crew equipment along a second direction, the second direction being perpendicular to the height direction of the crew cabin and the first direction, and the second sealing member abuts against the crew equipment along the first direction.

[0029] Optionally, the first sealing plate and the second sealing plate both include:

[0030] a second connection portion, the second connection portion being connected to the hatch;

[0031] a second bending portion, the second bending portion being located at an end of the second connecting portion away from the cabin door;

[0032] a flanging portion, the flanging portion being located at an end of the second bending portion away from the second connecting portion, the flanging portion and the second connecting portion being located on the same side of the second bending portion;

[0033] The second connecting portion, the second bending portion and the flange portion are integrally formed.

[0034] Optionally, the first sealing member is connected to the flange portion of the first sealing plate, and the second sealing member is connected to the second bent portion of the second sealing plate.

[0035] Optionally, the first sealing plate located below is provided with a ventilation structure.

[0036] Optionally, the crew cabin further includes a load-bearing member connected to the bottom surface of the accommodating cavity, and when the cabin accommodates the crew equipment, the crew equipment abuts against the top surface of the load-bearing member so that the crew equipment and the bottom surface of the accommodating cavity form an operating space.

[0037] A second aspect of the present invention provides a container, comprising the crew cabin provided by the first aspect of the present invention.

[0038] According to the crew cabin of the utility model, by arranging a sealing plate on the back of the cabin door to cooperate with the crew equipment, when the cabin door is closed, the sealing plate can abut against the crew equipment, so that the sealing plate and the end face of the crew equipment form a closed structure, that is, the connection between the gap area formed by the periphery of the crew equipment and the accommodating cavity and the external environment is blocked. Even if foreign objects such as mice and insects enter the crew cabin through the cabin door, they will be blocked by the closed structure and cannot enter the interior of the crew equipment, thereby eliminating the impact of foreign objects on the operation and safety of the crew equipment. BRIEF DESCRIPTION OF THE DRAWINGS

[0039] The following drawings of the embodiments of the present invention are used as part of the present invention for understanding the present invention. The drawings show the embodiments of the present invention and their descriptions, and are used to explain the principles of the present invention. In the drawings,

[0040] Figure 1 It is a schematic front view of a container with a crew cabin according to a preferred embodiment of the utility model;

[0041] Figure 2 for Figure 1 A rear view structural diagram of the door end of the container shown;

[0042] Figure 3 for Figure 1 A schematic diagram of the structure when the sealing plate in the crew cabin blocks the gap area shown;

[0043] Figure 4 For along Figure 3 A schematic cross-sectional view of the structure cut along line AA in FIG.

[0044] Figure 5 For along Figure 3 A schematic cross-sectional view of the structure cut along line BB in FIG.

[0045] Figure 6 for Figure 4 A schematic diagram of the enlarged structure of part C in FIG.

[0046] Figure 7 for Figure 5 An enlarged structural diagram of part D in FIG.

[0047] Figure 8 A schematic diagram of the structure of the first sealing plate and the first sealing member being installed and matched; and

[0048] Fig. 9 It is a structural schematic diagram of the unit equipment located in the accommodating cavity.

[0049] Description of reference numerals:

[0050] 1 container 2 crew compartment

[0051] 2a Gap area 2b Operation space

[0052] 3 Unit equipment 11 Box

[0053] 12 Door 20 Cabin

[0054] 20a Accommodation chamber 30 Hatch door

[0055] 30a Air inlet and outlet 31 Door

[0056] 32 Door frame 33 Fixed component

[0057] 33a First connecting portion 33b First bending portion

[0058] 40 Sealing plate assembly 41 First sealing plate

[0059] 41a Second connecting portion 41b Second bending portion

[0060] 41c flange portion 42 second sealing plate

[0061] 43 first sealing member 44 second sealing member

[0062] 50 Limiting member 61 Load bearing member

[0063] 62 pad 411 ventilation structure

[0064] D1 First direction D2 Second direction

[0065] DH Height Direction DETAILED DESCRIPTION

[0066] In the following description, a large number of specific details are given to provide a more thorough understanding of the present invention. However, it is obvious to those skilled in the art that the present invention can be implemented without one or more of these details. In other examples, in order to avoid confusion with the present invention, some technical features known in the art are not described.

[0067] In order to fully understand the implementation of the present invention, a detailed structure will be presented in the following description. Obviously, the implementation of the implementation of the present invention is not limited to the specific details familiar to those skilled in the art.

[0068] It should be understood that the purpose of the terms used herein is only to describe specific embodiments and is not intended to limit the present invention, and the singular forms "a", "an" and "said / the" are also intended to include plural forms, unless the context clearly indicates otherwise. When the terms "comprise" and / or "include" are used in this specification, it indicates the presence of the features, integral bodies, steps, operations, elements and / or components, but does not exclude the presence or addition of one or more other features, integral bodies, steps, operations, elements, components and / or combinations thereof.

[0069] Ordinal numbers such as "first" and "second" cited in the present invention are merely identifiers and do not have any other meaning, such as a specific order. Moreover, for example, the term "first component" itself does not imply the existence of a "second component", and the term "second component" itself does not imply the existence of a "first component". It should be noted that the terms "upper", "lower", "front", "back", "left", "right", "inner", "outer" and similar expressions used in the present invention are for illustrative purposes only and are not limiting.

[0070] Hereinafter, specific embodiments of the present invention will be described in more detail with reference to the accompanying drawings. These drawings show representative embodiments of the present invention and are not intended to limit the present invention.

[0071] The utility model provides a container 1, which can be constructed to meet the needs of heat exchange, such as an energy storage container. The battery in the energy storage container generates heat during the charging and discharging process. In order to facilitate the heat exchange between the container 1 and the external environment, please refer to Figures 1 to 4 The container 1 is also provided with a crew compartment 2, and the crew compartment 2 is used to accommodate the crew equipment 3. Specifically, the container 1 may include a box body 11 and a door 12, the door 12 is pivotally connected to the box body 11, and a locking rod assembly is further provided between the box body 11 and the door 12 to control the opening and closing of the door 12.

[0072] Further, the crew cabin 2 may include a cabin body 20 and a cabin door 30. It is understandable that the cabin body 20 has a storage cavity 20a for accommodating the crew equipment 3. In the state where the cabin body 20 accommodates the crew equipment 3, a gap area 2a is formed between the periphery of the crew equipment 3 and the storage cavity 20a. Of course, there is still a gap between the front and rear ends of the crew equipment 3 and the storage cavity 20a, which is not directly related to the technical problem of the present utility model and is not described here. The cabin door 30 is connected to the cabin body 20 in an openable and closable manner. In order to prevent foreign objects such as mice and insects from entering the crew equipment 3 through the gap area 2a, the crew cabin 2 also includes a sealing plate assembly 40, which is connected to the back of the cabin door 30. Specifically, the sealing plate assembly 40 may include a first sealing plate 41 and a second sealing plate 42. The two first sealing plates 41 are spaced along the height direction DH of the crew cabin 2, and the two second sealing plates 42 are spaced along the first direction D1 perpendicular to the height direction DH of the crew cabin 2. It should be noted that the plane formed by the first direction D1 and the height direction DH is parallel to the plane of the hatch 30. Figure 1In the embodiment, the hatch 30 and the box door 12 are spaced apart along the width direction of the container 1, and the first direction D1 is the width direction of the container 1, rather than the thickness direction of the hatch 30. When the hatch 30 is closed, the first sealing plate 41 and the second sealing plate 42 are used to abut against the unit equipment 3, and the first sealing plate 41, the second sealing plate 42 and the end surface of the unit equipment 3 form a closed structure to cut off the communication between the gap area 2a and the external environment.

[0073] According to the crew cabin 2 of the utility model, by arranging a sealing plate on the back of the cabin door 30 to cooperate with the crew equipment 3, when the cabin door 30 is closed, the sealing plate can abut against the crew equipment 3, so that the sealing plate and the end face of the crew equipment 3 form a closed structure, that is, the connection between the gap area 2a formed by the periphery of the crew equipment 3 and the accommodating cavity 20a and the external environment is blocked. Even if foreign objects such as mice and insects enter the crew cabin 2 through the cabin door 30, they will be blocked by the closed structure and cannot enter the interior of the crew equipment 3, thereby eliminating the influence of foreign objects on the operation and safety of the crew equipment 3.

[0074] It should be noted that, in order to facilitate the placement of the unit equipment 3 and to facilitate shielding of the gap area 2 a , the first sealing plate 41 and the second sealing plate 42 are configured to be adjustable, that is, their positions can be adjusted relative to the cabin door 30 .

[0075] See also Figures 4 to 7 The door 30 may include a door body 31 and a door frame 32. The door body 31 has an air inlet and outlet 30a communicating with the external environment, and the door frame 32 is connected to the outer periphery of the door body 31. Figure 1, the door body 31 can be constructed as a mesh door, and the air inlet and outlet 30a can be constructed as mesh holes on the mesh door, so that the unit equipment 3 can exchange heat with the outside world. In an embodiment not shown, the cabin door 30 may include an air duct component, which is connected to the air inlet and outlet 30a and communicates with the external environment. It is easy to imagine that in order to ensure the sealing of the connection between the air duct component and the air inlet and outlet 30a, the air duct component may have a sealing portion, such as a sealing gasket. Of course, in order to avoid large-volume foreign objects blocking the air duct, the cabin door 30 may also be provided with a filter component, which is connected to the air inlet and outlet 30a. In order to facilitate the connection between the sealing plate assembly 40 and the cabin door 30, the cabin door 30 is also provided with a fixing member 33, which is connected to the door frame 32 and close to the back of the door body 31, and the sealing plate assembly 40 is connected to the fixing member 33. It can be understood that in order to fix the position of the sealing plate assembly after the adjustment is completed, the crew cabin 2 may also include a limiting member 50, which is detachably connected to at least one of the fixing member 33 and the sealing plate assembly 40. For example, the fixing member 33 has an assembly hole, and the closing plate assembly 40 has an adjustment hole corresponding to the position of the assembly hole. The adjustment hole can be constructed as a special-shaped hole, a waist-shaped hole, etc., by moving the closing plate assembly 40 relative to the fixing member 33, after the adjustment is completed, the closing plate assembly 40 can be locked by using the limiting member 50. Alternatively, the closing plate assembly 40 has a sliding portion, and the fixing member 33 has a guide portion adapted to the sliding portion. After the closing plate assembly 40 is slid and adjusted, the position of the closing plate assembly 40 can be locked by using the limiting member 50 to abut against the guide portion. In the present embodiment, preferably, the fixing member 33 includes a first connecting portion 33a and a first bending portion 33b. The first connecting portion 33a is connected to the door frame 32, and the first bending portion 33b is integrally formed with the first connecting portion 33a, and the first bending portion 33b is connected to the closing plate assembly 40. For example Figure 6 In the embodiment, the first connecting portion 33a is perpendicular to the first bending portion 33b.

[0076] See also Figure 6 and Figure 7 In order to improve the fit between the sealing plate assembly 40 and the unit equipment 3 and prevent the sealing plate assembly 40 from damaging the outer surface of the unit equipment 3, the unit cabin 2 may also include a first sealing member 43 and a second sealing member 44. Specifically, the first sealing member 43 is connected to the first sealing plate 41, and the second sealing member 44 is connected to the second sealing plate 42. When the cabin door 30 is in a closed state, the first sealing member 43 abuts against the unit equipment 3 along the second direction D2. The second direction D2 is perpendicular to the height direction DH of the unit cabin 2 and the aforementioned first direction D1. The second sealing member 44 abuts against the unit equipment along the first direction D1. For example Figure 4 and Figure 5 In the embodiment, the first direction D1 is configured as the width direction of the container 1 , and correspondingly, the second direction D2 is configured as the length direction of the container 1 .

[0077] Please continue reading Figure 6 and Figure 7 More specifically, the first sealing plate 41 and the second sealing plate 42 each include a second connecting portion 41a, a second bending portion 41b and a flange portion 41c. The second connecting portion 41a is connected to the hatch 30, or to the fixing member 33. The second bending portion 41b is located at an end of the second connecting portion 41a away from the hatch 30. The flange portion 41c is located at an end of the second bending portion 41b away from the second connecting portion 41a, and the flange portion 41c and the second connecting portion 41a are located on the same side of the second bending portion 41b. The second connecting portion 41a, the second bending portion 41b and the flange portion 41c are constructed as an integral molding. For example Figure 6 and Figure 7 , the second connection portion 41a and the flange portion 41c are both perpendicular to the second bent portion 41b. The first sealing member 43 is connected to the flange portion 41c of the first sealing plate 41, and the second sealing member 44 is connected to the second bent portion 41b of the second sealing plate 42. It can be understood that when the cabin door 30 is closed, the first sealing member 43 abuts against the front end surface of the unit equipment 3, and the second sealing member 44 abuts against the side of the unit equipment 3.

[0078] See also Figure 1 , Figure 8 and Fig. 9 In order to increase the air intake of the crew cabin 2, the first sealing plate 41 located at the bottom can be provided with a ventilation structure 411. Under the premise of ensuring that foreign matter cannot pass through, the ventilation structure 411 can be constructed as a mesh, a shutter, etc. In addition, in order to facilitate wiring and operation in the accommodating cavity 20a, please refer to Fig. 9 , the crew cabin 2 may further include a load-bearing member 61, which is connected to the bottom surface of the accommodating chamber 20a. When the cabin 20 accommodates the crew equipment 3, the crew equipment 3 abuts against the top surface of the load-bearing member 61. For example, the crew equipment 3 has a foot, which is adapted to the load-bearing member 61. The load-bearing member 61 may be constructed as a plurality of square tubes spaced apart along the first direction D1. In order to improve the stability of the placement of the crew equipment 3, the crew cabin 2 may further include a cushion block 62, which is located between the crew equipment 3 and the load-bearing member 61. For example Fig. 9 There are three load-bearing members 61, two of which are in contact with the feet of the unit equipment, and the middle load-bearing member 61 is in contact with the bottom surface of the unit equipment 3 via the pad 62, so that the unit equipment 3 and the bottom surface of the accommodating cavity 20a form an operating space 2b, which is convenient for wiring and operation.

[0079] According to the container 1 of the utility model, by providing a separate unit cabin 2, it is convenient to place the unit equipment 3, and by providing a sealing plate with adjustable position to cooperate with the unit equipment 3, when the cabin door 30 is closed, the sealing plate and the end surface of the unit equipment 3 form a closed structure to prevent foreign matter from entering the unit equipment 3. In addition, the sealing plate is easy to disassemble and adjust, which is convenient for later inspection and maintenance.

[0080] Unless otherwise defined, the technical and scientific terms used herein have the same meaning as those generally understood by those skilled in the art in the technical field of the present invention. The terms used herein are only for describing specific implementation purposes and are not intended to limit the present invention. Terms such as "setting" appearing in this article may indicate that one component is directly attached to another component, or that one component is attached to another component through an intermediate. Features described in this article in one embodiment may be applied to another embodiment alone or in combination with other features, unless the feature is not applicable in the other embodiment or otherwise specified.

[0081] The utility model has been described through the above embodiments, but it should be understood that the above embodiments are only for the purpose of example and description, and are not intended to limit the utility model to the described embodiments. It can be understood by those skilled in the art that more variations and modifications can be made according to the teachings of the utility model, and these variations and modifications all fall within the scope of the protection claimed by the utility model.

Claims

1. A crew cabin for accommodating crew equipment, characterized in that: The crew compartment comprises: A cabin body, the cabin body having a receiving cavity for receiving the unit equipment, wherein when the cabin body receives the unit equipment, a gap area is formed between the outer periphery of the unit equipment and the receiving cavity; a hatch connected to the cabin; A sealing plate assembly, the sealing plate assembly is connected to the back side of the cabin door, and the sealing plate assembly comprises: a first sealing plate, two of the first sealing plates being spaced apart along a height direction of the crew cabin; a second sealing plate, wherein two of the second sealing plates are spaced apart along a first direction perpendicular to a height direction of the crew compartment; The first sealing plate and the second sealing plate are used to abut against the unit equipment, and the first sealing plate, the second sealing plate and the end surface of the unit equipment form a closed structure to cut off the communication between the gap area and the external environment.

2. The crew compartment according to claim 1, characterized in that: The first sealing plate and the second sealing plate are configured to be adjustable so as to cover the gap area.

3. The crew compartment according to claim 1, characterized in that: The hatch is openably connected to the cabin body, and the hatch comprises: A door body, wherein the door body has an air inlet and an air outlet communicating with the external environment; a door frame connected to the outer periphery of the door body; A fixing member, the fixing member being connected to the door frame and close to the back side of the door body, the sealing plate assembly being connected to the fixing member; The crew compartment further includes a position-limiting member, which is detachably connected to at least one of the fixing member and the sealing plate assembly, and is used to fix the position of the sealing plate assembly after adjustment.

4. The crew compartment according to claim 3, characterized in that: The fixing member has an assembly hole, the sealing plate assembly has an adjustment hole corresponding to the position of the assembly hole, and the limiting member is detachably connected to the assembly hole and the adjustment hole to adjust the position of the sealing plate assembly relative to the fixing member.

5. The crew compartment according to claim 4, characterized in that: The fixing member comprises: a first connection portion, the first connection portion being connected to the door frame; A first bending portion, wherein the first bending portion and the first connecting portion are integrally formed, and the first bending portion is connected to the sealing plate assembly.

6. The crew compartment according to claim 3, characterized in that: The hatch also includes: An air duct component, the air duct component is connected to the air inlet and outlet and communicates with the external environment, and the air duct component has a sealing portion to ensure the sealing degree of the connection between the air duct component and the air inlet and outlet; A filter component is connected to the air inlet and outlet.

7. The crew compartment according to claim 1, characterized in that: The crew compartment also includes: a first sealing member connected to the first sealing plate; a second sealing member connected to the second sealing plate; When the cabin door is in a closed state, the first sealing member abuts against the crew equipment along a second direction, the second direction being perpendicular to the height direction of the crew cabin and the first direction, and the second sealing member abuts against the crew equipment along the first direction.

8. The crew compartment according to claim 7, characterized in that: The first sealing plate and the second sealing plate both include: a second connection portion, the second connection portion being connected to the hatch; a second bending portion, the second bending portion being located at an end of the second connecting portion away from the cabin door; a flanging portion, the flanging portion being located at an end of the second bending portion away from the second connecting portion, the flanging portion and the second connecting portion being located on the same side of the second bending portion; The second connecting portion, the second bending portion and the flange portion are integrally formed.

9. The crew compartment according to claim 8, characterized in that: The first sealing member is connected to the flange portion of the first sealing plate, and the second sealing member is connected to the second bent portion of the second sealing plate.

10. The crew compartment according to claim 1, characterized in that: The first sealing plate located at the bottom is provided with a ventilation structure.

11. The crew compartment according to any one of claims 1 to 10, characterized in that: The crew cabin also includes a load-bearing member connected to the bottom surface of the accommodating cavity. When the cabin accommodates the crew equipment, the crew equipment abuts against the top surface of the load-bearing member so that the crew equipment and the bottom surface of the accommodating cavity form an operating space.

12. A container, characterized in that: Comprising a crew compartment according to any one of claims 1 to 11.

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