Machine body assembly and fan

Abstract

The invention relates to a machine body assembly and a fan. The machine body assembly comprises a machine body rod, a support and a battery piece. The support is connected to the top of the machine body rod and used for installing a machine head of the fan. The battery piece is arranged on the top of the machine body rod and used for supplying power to the machine head. According to the machine body assembly, the battery piece serves as a power source to supply power to the machine head, and the battery piece is located at the position, closer to the machine head, of the top of the machine body rod. Therefore, the power supply wiring of the machine head can achieve the effects of taking power from the battery piece and supplying power to the machine head without passing through most structures such as the machine body assembly from the chassis. Therefore, the wiring difficulty on the machine body assembly is lower, and the influence of other structures on the circuit is smaller.

Description

Technical Field

[0001] The present application relates to the field of electrical technology, and in particular to a body assembly and a fan. Background Art

[0002] In the related art, the circulation fan usually sets the power supply module at the bottom chassis, and its wiring needs to pass through most of the structures such as the body of the circulation fan to reach the head to power the motor. In addition, structures such as large-range telescopic and motion structures that have a significant change in the shape of the fan are usually quite unfavorable for internal wiring, and are prone to problems such as lack of space to accommodate excess wires and wear of the moving wiring due to changes in the shape. Summary of the invention

[0003] Based on this, it is necessary to provide a body component and a fan that can reduce the difficulty of wiring in order to solve the above-mentioned problems.

[0004] A fuselage assembly, the fuselage assembly comprising:

[0005] fuselage rod;

[0006] a bracket connected to the top of the fuselage rod and used for mounting the head of the fan; and

[0007] The battery component is arranged on the top of the body rod and is used to supply power to the head.

[0008] The above-mentioned body assembly has a battery as a power source to supply power to the head, and the battery is located at the top of the body rod, which is closer to the head. Therefore, the power supply wiring of the head does not need to pass through the chassis and most structures such as the body assembly to achieve the effect of drawing power from the battery and supplying power to the head. In this way, the wiring on the body assembly is less difficult, and the line is less affected by other structures. In addition, because of the battery, the fan with the body assembly can be used in outdoor scenes such as picnics, and the usage scenarios are richer.

[0009] In one embodiment, the bracket is rotatably connected to the fuselage rod, and the bracket has an unfolded position and a folded position that can be switched by rotation;

[0010] The body assembly also includes a first conductive member, which is arranged on the bracket and is used to be electrically connected to the head; the battery component has a second conductive member; the first conductive member is configured to be able to contact the second conductive member when the bracket is in the unfolded position to form an electrical connection with the battery component.

[0011] In this way, the fan head can be folded relative to the body rod through the bracket to reduce the storage space required when the fan is not in use. On the basis that the body assembly enables the fan head to have a folding function, the first conductive member and the second conductive member are in contact with each other to form an electrical connection when the bracket is in the unfolded position, and the power supply to the fan head can be reduced. The impact of the flipping action on the service life of the power supply line can be reduced, and the difficulty of routing at the folding position can be reduced.

[0012] In one embodiment, the battery unit is detachably mounted on the top of the body rod; and / or, the battery unit is rechargeable.

[0013] In this way, the user can disassemble and assemble the battery component, replace the battery component, charge the battery component, etc. according to needs.

[0014] In one embodiment, the fuselage assembly further comprises a mounting shell, the battery component and the mounting shell are connected together to form a battery module, and the battery module is detachably disposed on the top of the fuselage rod;

[0015] The bracket has a first abutting surface, and the battery module has a second abutting surface. When the bracket is in the expanded position, the first abutting surface abuts against the second abutting surface, and the first conductive member and the second conductive member form an electrical connection at the first abutting surface and the second abutting surface.

[0016] In this way, the mounting shell can protect and support the battery component, and the two are connected together to form a battery module, which is convenient for users to disassemble and assemble. After the bracket is unfolded in place, the first conductive member and the second conductive member naturally form contact at the abutting surface of the two and form an electrical connection.

[0017] In one embodiment, the top of the fuselage rod has a mounting position, the battery module is detachably arranged at the mounting position, and the mounting shell is formed as a top cover of the fuselage rod;

[0018] And / or, the body rod and the battery module respectively have a first engaging portion and a second engaging portion, and the first engaging portion engages with the second engaging portion.

[0019] In this way, the battery module can be assembled by simply installing the mounting shell at least partially outward at the mounting position on the top of the fuselage rod, and the mounting shell naturally becomes the top cover of the fuselage rod. The battery module is easier to disassemble and assemble, and the fuselage assembly is more integrated after the battery module is installed. The battery module can be quickly disassembled and assembled by snap-fit ​​installation. It is understandable that in some other embodiments, the battery module can also be installed on the fuselage rod by magnetic connection, threaded connection, etc., which is not specifically limited here.

[0020] In one embodiment, the first conductive member is at least partially exposed to form a first contact point, the second conductive member is at least partially exposed to form a second contact point, and the first conductive member and the second conductive member are in contact with each other through the first contact point and the second contact point.

[0021] In this way, the first conductive member can be electrically connected to the second conductive member through the first contact point formed by the first conductive member being exposed.

[0022] In one embodiment, the battery module has a slot, the second contact is located in the slot, the first conductive member has a convex portion that matches the slot, and the top of the convex portion is formed as the first contact;

[0023] Alternatively, the bracket has a slot, the first contact is located in the slot, the second conductive member has a convex portion matched with the slot, and the top end of the convex portion is formed as the second contact.

[0024] In this way, the protrusion is inserted into the slot to realize electrical connection between the first conductive member and the second conductive member. The matching mode of the slot and the protrusion can improve the positioning accuracy between the first contact point and the second contact point and improve the power connection efficiency.

[0025] In one embodiment, the body rod includes a rod body and a shaking head part, the bracket is connected to the shaking head part by rotating around a first direction, the battery component is arranged on the shaking head part, and the shaking head part is rotatable around a second direction and arranged on the top of the rod body; wherein the first direction intersects with the second direction.

[0026] In this way, the body assembly can realize the shaking head function, and the battery component is arranged on the shaking head part, so that it can remain still relative to the bracket when the fan is shaking.

[0027] In one embodiment, the rod is configured to be telescopic.

[0028] In this way, the height of the body assembly can be adjusted by the extension of the rod body, that is, the use height of the fan can be changed. Since the battery component is located on the shaking head, the electrical connection between the battery component and the head can be unaffected by the extension of the rod body.

[0029] A fan comprises the above-mentioned fuselage assembly. BRIEF DESCRIPTION OF THE DRAWINGS

[0030] In order to more clearly illustrate the embodiments of the present application or the technical solutions in the prior art, the drawings required for use in the embodiments or the description of the prior art will be briefly introduced below. Obviously, the drawings described below are only some embodiments of the present application. For ordinary technicians in this field, other drawings can be obtained based on these drawings without paying creative work.

[0031] FIG. 1 is a schematic cross-sectional view of a fan having a body assembly according to an embodiment of the present application.

[0032] FIG. 2 is an enlarged structural schematic diagram of the fan shown in FIG. 1 at position A. FIG.

[0033] FIG. 3 is a schematic diagram of a cross-sectional structure of the fan shown in FIG. 1 at another angle.

[0034] FIG. 4 is an enlarged structural schematic diagram of the fan shown in FIG. 1 at position B. FIG.

[0035] FIG. 5 is a schematic structural diagram of a battery component and a first conductive component in the fan shown in FIG. 1 .

[0036] FIG. 6 is a schematic structural diagram of a battery component in the fan shown in FIG. 1 .

[0037] FIG. 7 is a schematic structural diagram of a first conductive member in the fan shown in FIG. 1 .

[0038] FIG. 8 is an enlarged structural schematic diagram of the first conductive member at position C shown in FIG. 7 .

[0039] Explanation of the reference numerals: 100, body assembly; 10, body rod; 11, first engaging portion; 13, second engaging portion; 15, rod body; 17, shaking head; 20, bracket; 30, battery module; 31, battery component; 311, second conductive member; 33, mounting shell; 331, power indicator light; 333, charging port; 35, slot; 40, chassis; 50, first conductive member; 51, convex portion; 200, fan; 210, head; 211, fan blades; 213, motor. DETAILED DESCRIPTION

[0040] In order to make the above-mentioned purposes, features and advantages of the present application more obvious and easy to understand, the specific implementation methods of the present application are described in detail below in conjunction with the accompanying drawings. In the following description, many specific details are set forth to facilitate a full understanding of the present application. However, the present application can be implemented in many other ways different from those described herein, and those skilled in the art can make similar improvements without violating the connotation of the present application, so the present application is not limited by the specific embodiments disclosed below.

[0041] In the description of the present application, it should be understood that if the terms "center", "longitudinal", "lateral", "length", "width", "thickness", "up", "down", "front", "back", "left", "right", "vertical", "horizontal", "top", "bottom", "inside", "outside", "clockwise", "counterclockwise", "axial", "radial", "circumferential", etc. appear, the orientation or position relationship indicated by these terms is based on the orientation or position relationship shown in the accompanying drawings, which 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 specific orientation, be constructed and operated in a specific orientation, and therefore it should not be understood as a limitation on the present application.

[0042] In addition, if the term "and / or" appears, "and / or" is merely a way to describe the association relationship between associated objects, and indicates that three relationships may exist, for example, A and / or B can represent the association relationship between A and B: A exists alone, A and B exist at the same time, and B exists alone. In addition, the character " / " in this article generally indicates that there is an "or" relationship between the associated objects before and after it. If the terms "first" and "second" appear, these terms are only used for descriptive purposes and cannot be understood as indicating or implying relative importance or implicitly indicating the number of technical features indicated. Therefore, the features defined as "first" and "second" may explicitly or implicitly include at least one of the features. In the description of this application, if the term "multiple" appears, the meaning of "multiple" is at least two, such as two, three, four, five, etc., unless otherwise clearly and specifically defined.

[0043] In this application, unless otherwise clearly specified and limited, if the terms "installed", "connected", "connected", "fixed" and the like appear, these terms should be understood in a broad sense. For example, it can be a fixed connection, a detachable connection, or an integrated connection; it can be a mechanical connection or an electrical connection; it can be a direct connection or an indirect connection through an intermediate medium, it can be the internal connection of two elements or the interaction relationship between two elements, unless otherwise clearly defined. For ordinary technicians in this field, the specific meanings of the above terms in this application can be understood according to specific circumstances.

[0044] In the present application, unless otherwise clearly specified and limited, if there is a description that a first feature is "above" or "below" a second feature, etc., or similar descriptions appear, it may mean that the first and second features are in direct contact, or that the first and second features are in indirect contact through an intermediate medium. Moreover, the first feature being "above", "above" and "above" the second feature may mean that the first feature is directly above or obliquely above the second feature, or simply means that the first feature is higher in level than the second feature. The first feature being "below", "below" and "below" the second feature may mean that the first feature is directly below or obliquely below the second feature, or simply means that the first feature is lower in level than the second feature.

[0045] It should be noted that if an element is referred to as being "fixed to" or "disposed on" another element, it may be directly on the other element or there may be a central element. If an element is considered to be "connected to" another element, it may be directly connected to the other element or there may be a central element at the same time. If any, the terms "vertical", "horizontal", "upper", "lower", "left", "right" and similar expressions used in this application are for illustrative purposes only and do not represent the only implementation method.

[0046] Referring to FIGS. 1 to 5 , a fuselage assembly 100 provided in one embodiment of the present application includes a fuselage rod 10, a bracket 20, and a battery component 31. The bracket 20 is connected to the top of the fuselage rod 10 and is used to install the head 210 of the fan 200. The battery component 31 is disposed at the top of the fuselage rod 10 and is used to supply power to the head 210.

[0047] The fuselage assembly 100 is used for the fan 200. Specifically, the fan 200 can be, but is not limited to, a circulation fan. The bracket 20 of the fuselage assembly 100 is used to connect the head 210 of the fan 200 to achieve the installation of the head 210 relative to the fuselage assembly 100. In order to achieve its normal function, the head 210 includes a fan blade 211, a motor 213, etc. The motor 213 is used to drive the fan blade 211 to rotate to generate an air supply airflow. Among them, the battery component 31 is used to power the head 210, that is, it serves as a power source and can supply power to the motor 213. In addition, due to the battery component 31, the fan 200 with the fuselage assembly 100 can be used in outdoor scenes such as picnics, and the usage scenarios are richer.

[0048] It can be understood that the fuselage rod 10 has two ends, a top and a bottom, in its own height direction. The top is used to connect the bracket 20 to install the head 210, and the bottom is used to support the placement surface of the fan 200, such as the ground. Specifically, the fuselage assembly 100 also includes a chassis 40, which is connected to the bottom of the fuselage rod 10 and is used to support the fan 200.

[0049] The above-mentioned fuselage assembly 100 has a battery unit 31 as a power source to supply power to the head 210, and the battery unit 31 is located at the top of the fuselage rod 10, which is closer to the head 210. Therefore, the power supply line of the head 210 does not need to pass through the chassis 40 and most structures such as the fuselage assembly 100 to achieve the effect of taking power from the battery unit 31 and supplying power to the head 210. In this way, the wiring difficulty on the fuselage assembly 100 is lower, and the line is less affected by other structures.

[0050] In some embodiments, the bracket 20 is rotatably connected to the fuselage rod 10 , and the bracket 20 has an unfolded position and a folded position that can be switched by rotation.

[0051] It can be understood that the bracket 20 is rotatably connected to the top of the fuselage rod 10, and the head 210 of the fan 200 is installed on the bracket 20. It can be flipped by rotating the bracket 20 relative to the fuselage rod 10 as the bracket 20 switches between the unfolded position and the folded position. The bracket 20 is the flipping mechanism for the head 210 to achieve flipping.

[0052] When the bracket 20 is in the unfolded position, the head 210 is unfolded relative to the body rod 10, and the fan 200 is in normal use; when the bracket 20 is in the folded position, the head 210 is folded relative to the body rod 10, and the fan 200 is in the stored state.

[0053] In this way, the head 210 can be folded relative to the body rod 10 through the bracket 20 to reduce the storage space required for the fan 200 when not in use.

[0054] Please refer to Figures 6 to 8 together. Further, the body assembly 100 further includes a first conductive member 50, and the battery member 31 has a second conductive member 311. The first conductive member 50 is provided on the bracket 20 and is used to be electrically connected to the head 210. The first conductive member 50 is configured to be able to contact the second conductive member 311 when the bracket 20 is in the unfolded position, so as to form an electrical connection with the battery member 31.

[0055] The first conductive member 50 is used to be electrically connected to the handpiece 210 , that is, it can be electrically connected to the motor 213 of the handpiece 210 , so that the power source can supply power to the motor 213 through the first electrical connector.

[0056] The second conductive component 311 of the battery component 31 can be an electrode of the battery component 31 or other conductive components electrically connected to the electrode, etc. As long as the first conductive component 50 and the second conductive component 311 are in contact to form an electrical connection, the motor 213 can be electrically connected to the battery through the first conductive component 50 and the second conductive component 311, and no specific limitation is made here.

[0057] It can be understood that both the first conductive member 50 and the second conductive member 311 have conductive properties and are at least partially made of conductive materials. Specifically, the conductive material can be a metal, such as copper, aluminum, stainless steel, etc., or a conductive non-metal such as graphite, which is not specifically limited here. When the bracket 20 is in the unfolded position, the first conductive member 50 is in contact with the second conductive member 311, and when the bracket 20 is in the folded position, the first conductive member 50 and the second conductive member 311 are not in contact with each other.

[0058] In this way, based on the fact that the body assembly 100 has a folding function for the head 210 of the fan 200, power is supplied to the head 210 in such a way that the first conductive member 50 and the second conductive member 311 are in contact to form an electrical connection when the bracket 20 is in the unfolded position. This can reduce the impact of the flipping action on the service life of the power supply line and reduce the difficulty of wiring at the folding position.

[0059] In some embodiments, the battery unit 31 is detachably mounted on the top of the body rod 10; and / or, the battery unit 31 is rechargeable. In this way, the user can disassemble and assemble the battery unit 31, replace the battery unit 31, charge the battery unit 31, etc. as needed.

[0060] Furthermore, the fuselage assembly 100 also includes a mounting shell 33 , and the battery component 31 and the mounting shell 33 are connected together to form a battery module 30 , and the battery module 30 is detachably disposed on the top of the fuselage rod 10 .

[0061] The battery component 31 and the mounting shell 33 can be connected to the mounting shell 33 by bonding or snapping with sponge or glue, and can be assembled and disassembled together.

[0062] In this way, the mounting shell 33 can protect and support the battery component 31 , and the two are connected together to form a battery module 30 , which is convenient for users to disassemble and assemble.

[0063] In some embodiments, the top of the fuselage pole 10 has a mounting position, the battery module 30 is detachably arranged at the mounting position, and the mounting shell 33 forms a top cover of the fuselage pole 10. In addition, the mounting shell 33 may also have a power indicator light 331 and a charging interface 333, the power indicator light 331 is used to display the current power, and the charging interface 333 is used to charge the battery unit 31.

[0064] In this way, the battery module 30 can be assembled by simply installing the mounting shell 33 at least partially outwardly at the mounting position on the top of the fuselage rod 10, and the mounting shell 33 naturally becomes the top cover of the fuselage rod 10. The battery module 30 can be assembled and disassembled more easily, and the fuselage assembly 100 has a stronger integrity after the battery module 30 is installed.

[0065] In some embodiments, the body rod 10 and the battery module 30 respectively have a first engaging portion 11 and a second engaging portion 13 , and are engaged with each other through the first engaging portion 11 and the second engaging portion 13 .

[0066] In this way, the battery module 30 can be quickly assembled and disassembled by means of snap-fit ​​installation. It is understandable that in some other embodiments, the battery module 30 can also be installed on the fuselage rod 10 by means of magnetic connection, threaded connection, etc., which is not specifically limited here.

[0067] In some embodiments, the bracket 20 has a first abutting surface, and the battery module 30 has a second abutting surface. When the bracket 20 is in the expanded position, the first abutting surface abuts against the second abutting surface, and the first conductive member 50 and the second conductive member 311 form an electrical connection at the first abutting surface and the second abutting surface.

[0068] The first abutment surface of the battery module 30 can be used as a support surface for the bracket 20 after it is unfolded. When the bracket 20 switches from the folded position to the unfolded position, it rotates along the first direction. When the bracket 20 rotates to the unfolded position and abuts against the first abutment surface, it may be blocked by the first abutment surface and cannot continue to rotate along the first direction.

[0069] In this way, after the bracket 20 is deployed in place, the first conductive member 50 and the second conductive member 311 naturally form contact at the abutting surfaces thereof and form an electrical connection.

[0070] In some embodiments, the first conductive member 50 is at least partially exposed to form a first contact, and the second conductive member 311 is at least partially exposed to form a second contact. The first conductive member 50 and the second conductive member 311 are in contact with each other through the first contact and the second contact.

[0071] Specifically, the first contact is exposed at the first abutting surface of the bracket 20, and the second contact is exposed at the second abutting surface of the mounting shell 33, and the two can contact each other when the bracket 20 is in the unfolded position. There can be multiple first contacts and multiple second contacts.

[0072] In this way, the first conductive member 50 can be electrically connected to the second conductive member 311 through the first contact point formed by the first conductive member 50 being exposed.

[0073] In one embodiment, the battery module 30 has a slot 35 , the second contact is located in the slot 35 , the first conductive member 50 has a protrusion 51 that matches the slot 35 , and the top of the protrusion 51 is formed as the first contact.

[0074] In this way, the first conductive member 50 is inserted into the slot 35 through the protrusion 51 having the first contact to contact the second contact and be electrically connected to the second conductive member 311. The matching manner of the slot 35 and the protrusion 51 can improve the positioning accuracy between the first contact and the second contact and improve the power connection efficiency.

[0075] In another embodiment, the bracket 20 has a slot 35 , the first contact is located in the slot 35 , the second conductive member 311 has a protrusion 51 that matches the slot 35 , and the top of the protrusion 51 is formed as the second contact.

[0076] In this way, the second conductive member 311 is inserted into the slot 35 through the protrusion 51 having the second contact to contact the first contact and be electrically connected to the first conductive member 50. The matching manner of the slot 35 and the protrusion 51 can improve the positioning accuracy between the first contact and the second contact and improve the power connection efficiency.

[0077] In some embodiments, the body rod 10 includes a rod body 15 and a shaking head 17, the bracket 20 is connected to the shaking head 17 by rotation around a first direction, the battery component 31 is disposed on the shaking head 17, and the shaking head 17 is rotatably disposed on the top of the rod body 15 around a second direction. The first direction intersects with the second direction.

[0078] It can be understood that the bracket 20 rotates around the first direction to drive the head 210 to fold relative to the body rod 10, and can follow the shaking head 17 to rotate around the second direction relative to the rod body 15, driving the head 210 to achieve the shaking head function. Specifically, the first direction can be a horizontal direction, and the second direction can be a vertical direction, and the two are perpendicular to each other.

[0079] In addition, the body assembly 100 also includes a driver for driving the oscillating part 17 to rotate, and the battery component 31 can also supply power to the driver.

[0080] In this way, the body assembly 100 can realize the shaking function, and the battery component 31 is arranged on the shaking portion 17, so that it can remain still relative to the bracket 20 when the fan 200 is shaking.

[0081] Furthermore, the rod body 15 is configured to be telescopic to change its own length.

[0082] Thus, the height of the body assembly 100 can be adjusted by the extension of the rod body 15, that is, the height of the fan 200 can be changed. Since the battery unit 31 is located on the oscillating portion 17, the electrical connection between the battery unit 31 and the head 210 is not affected by the extension of the rod body 15.

[0083] In some embodiments, the fuselage assembly 100 further includes a counterweight (not shown), which is disposed on the chassis 40. In this way, the weight of the counterweight can be used to improve the stability of the fuselage assembly 100.

[0084] The above-mentioned fuselage assembly 100 has the functions of folding, shaking head and telescopic, and includes a battery component 31 as a power source. The battery component 31 is arranged at the top of the fuselage rod 10, and is located close to the head 210, so that the head 210 can be powered nearby, and the wiring range is greatly shortened. Specifically, the battery component 31 is arranged on the shaking head portion 17 of the fuselage rod 10 and can rotate therewith, which means that its power supply wiring does not need to pass through the rod body 15 of the fuselage rod 10, and is not affected by the rotation of the shaking head portion 17 and the telescopic extension of the rod body 15. In addition, when the bracket 20 is in the unfolded position, the battery component 31 contacts the first conductive component 50 through its second conductive component 311 to form an electrical connection, and this connection method can reduce the impact of the folding of the bracket 20. In this way, the wiring difficulty on the fuselage assembly 100 is lower, and the line is less affected by its folding, shaking head and telescopic functions.

[0085] The present application also provides a fan 200, comprising the above-mentioned fuselage assembly 100. The fan 200 may be, but is not limited to, a circulation fan, a table fan, and the like.

[0086] The technical features of the above-described embodiments may be arbitrarily combined. To make the description concise, not all possible combinations of the technical features in the above-described embodiments are described. However, as long as there is no contradiction in the combination of these technical features, they should be considered to be within the scope of this specification.

[0087] The above-described embodiments only express several implementation methods of the present application, and the descriptions thereof are relatively specific and detailed, but they cannot be construed as limiting the scope of the patent application. It should be pointed out that, for a person of ordinary skill in the art, several variations and improvements can be made without departing from the concept of the present application, and these all belong to the protection scope of the present application. Therefore, the protection scope of the patent application shall be subject to the attached claims.

Claims

1. A fuselage assembly, characterized in that: The fuselage assembly comprises: Fuselage rod (10); a bracket (20) connected to the top of the fuselage rod (10) and used for mounting a fan head (210); and A battery component (31) is arranged on the top of the body rod (10) and is used to supply power to the head (210).

2. The fuselage assembly according to claim 1, characterized in that: The bracket (20) is rotatably connected to the fuselage rod (10), and the bracket (20) has an unfolded position and a folded position that can be switched by rotation; The fuselage assembly further comprises a first conductive member (50), the first conductive member (50) being arranged on the bracket (20) and being used for being electrically connected to the head (210); the battery member (31) has a second conductive member (311); the first conductive member (50) being configured to be able to contact the second conductive member (311) when the bracket (20) is in the unfolded position, so as to form an electrical connection with the battery member (31).

3. The fuselage assembly according to claim 2, characterized in that: The battery component (31) is detachably arranged on the top of the fuselage rod (10); and / or the battery component (31) is rechargeable.

4. The fuselage assembly according to claim 3, characterized in that: The fuselage assembly further comprises a mounting shell (33), the battery component (31) and the mounting shell (33) are connected together to form a battery module (30), and the battery module (30) is detachably arranged on the top of the fuselage rod (10); The bracket (20) has a first abutting surface, and the battery module (30) has a second abutting surface. When the bracket (20) is in the unfolded position, the first abutting surface abuts against the second abutting surface, and the first conductive member (50) and the second conductive member (311) form an electrical connection at the first abutting surface and the second abutting surface.

5. The fuselage assembly according to claim 4, characterized in that: The top of the fuselage rod (10) has a mounting position, the battery module (30) is detachably arranged at the mounting position, and the mounting shell (33) is formed as a top cover of the fuselage rod (10); And / or, the fuselage rod (10) and the battery module (30) respectively have a first engaging portion (11) and a second engaging portion (13), and the first engaging portion (11) and the second engaging portion (13) are engaged with each other.

6. The fuselage assembly according to claim 4, characterized in that: The first conductive member (50) is at least partially exposed to form a first contact point, the second conductive member (311) is at least partially exposed to form a second contact point, and the first conductive member (50) and the second conductive member (311) are in contact with each other via the first contact point and the second contact point.

7. The fuselage assembly according to claim 6, characterized in that: The battery module (30) has a slot, the second contact is located in the slot, the first conductive member (50) has a convex portion (51) that matches the slot, and the top end of the convex portion (51) forms the first contact; Alternatively, the bracket (20) has a slot, the first contact is located in the slot, the second conductive member (311) has a convex portion (51) that matches the slot, and the top end of the convex portion (51) forms the second contact.

8. The fuselage assembly according to any one of claims 2 to 7, characterized in that: The body rod (10) comprises a rod body (15) and an oscillating portion (17); the bracket (20) is rotatably connected to the oscillating portion (17) around a first direction; the battery component (31) is disposed on the oscillating portion (17); and the oscillating portion (17) is rotatably disposed on the top of the rod body (15) around a second direction; wherein the first direction intersects with the second direction.

9. The fuselage assembly according to claim 8, characterized in that: The rod body (15) is configured to be telescopic.

10. A fan, characterized in that: Comprising a fuselage assembly as described in any one of claims 1-9.

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