Cabin area controller assembly

Abstract

The utility model relates to the technical field of automobile cabin equipment, and provides a cabin area controller assembly, a shell cover, a controller body and a locking structure, the shell cover is provided with a containing cavity and a mounting opening communicated with the containing cavity, the controller body is arranged on the shell cover in a sliding mode through the mounting opening, and the controller body can slide to a locking position. The locking structure is arranged between the housing and the controller body, and the locking structure is used for realizing locking connection between the housing and the controller body at the locking position. According to the cabin area controller assembly, the housing is arranged to serve as the mounting seat of the controller body, the accommodating cavity is formed in the housing, and the mounting opening is formed in one side of the accommodating cavity, so that the controller body is mounted in the accommodating cavity from the mounting opening and slides to the locking position in the accommodating cavity; the shell cover and the controller body are locked and fixed through the locking structure at the locking position, screw holes do not need to be aligned manually, and installation is more convenient and trouble-saving.

Description

Technical Field

[0001] The utility model relates to the technical field of automotive cockpit equipment, in particular to a cockpit domain controller assembly. Background Art

[0002] With the advent of automotive intelligence, automotive electronic hardware has shifted from being decentralized to centralized, and vehicle domain controllers are gradually replacing traditional controller units. Among them, the cockpit domain controller, as the core unit of the domain controller, is arranged and installed on the vehicle instrument panel assembly.

[0003] In the prior art, the cockpit domain controller is usually bolted to the instrument panel assembly. During actual installation, it is necessary to align each screw hole of the cockpit domain controller with each screw hole of the instrument panel assembly and then install the bolts, which is inconvenient, time-consuming, and laborious. Summary of the Utility Model

[0004] The utility model provides a cockpit domain controller assembly to solve the defects of inconvenient installation, time-consuming, and laborious of the cockpit domain controller in the prior art.

[0005] The utility model provides a cockpit domain controller assembly, including:

[0006] A housing cover and a controller body. The housing cover has a receiving cavity and an installation opening communicating with the receiving cavity. The controller body is slidably disposed in the housing cover through the installation opening, and the controller body can slide to a locking position.

[0007] A locking structure is disposed between the housing cover and the controller body, and the locking structure is used to realize the locking connection between the housing cover and the controller body at the locking position.

[0008] According to the cockpit domain controller assembly of the utility model, a guiding groove is provided on the inner wall of the receiving cavity, and a sliding member is provided on the controller body. The sliding member is used to slide along the extending direction of the guiding groove until the controller body reaches the locking position.

[0009] According to the cockpit domain controller assembly of the utility model, an opening is provided at the first end of the guiding groove facing the installation opening, and the sliding member is used to enter the guiding groove from the opening.

[0010] When the controller body is in the locking position, the sliding member abuts against the second end of the guiding groove.

[0011] According to the cockpit domain controller assembly of the utility model, the guiding groove includes a connected guiding section and a locking section.

[0012] The guiding section is provided with the opening, and the width of the guiding section gradually decreases from one end of the opening towards the locking section;

[0013] When the controller body is in the locking position, the sliding member abuts against the groove wall of the locking section.

[0014] According to the cockpit domain controller assembly of the present utility model, the sliding member includes a cylinder and a flexible sleeve. The cylinder is arranged on the controller body, and the flexible sleeve is sleeved on the cylinder. The flexible sleeve is in sliding fit with the groove wall of the guiding groove.

[0015] According to the cockpit domain controller assembly of the present utility model, the sliding member includes a cylinder and a spherical member. The first end of the cylinder is connected to the controller body, the second end of the cylinder is connected to the spherical member, and the groove wall of the guiding groove is an arc-shaped groove wall that fits the spherical member; the spherical member is in sliding fit with the groove wall of the guiding groove.

[0016] According to the cockpit domain controller assembly of the present utility model, the sliding member includes a roller. The roller is rotatably arranged on the controller body and is in rolling fit with the groove wall of the guiding groove.

[0017] According to the cockpit domain controller assembly of the present utility model, the locking structure includes a first locking member and a second locking member; the first locking member is arranged at the installation opening, and the second locking member is arranged on the controller body;

[0018] When the controller body is in the locking position, the first locking member and the second locking member are locked and connected.

[0019] According to the cockpit domain controller assembly of the present utility model, there are two first locking members, and the two first locking members are respectively arranged on opposite sides of the installation opening;

[0020] There are two second locking members, which are arranged in one-to-one correspondence with the two first locking members; a limiting hook is arranged on each second locking member; when the controller body is in the locking position, the limiting hook abuts against the first locking member.

[0021] According to the cockpit domain controller assembly of the present utility model, one of the first locking member and the second locking member is provided with a clamping hole, and a clamping portion is provided at a position corresponding to the clamping hole on the other; when the controller body is in the locking position, the clamping portion is clamped in the clamping hole;

[0022] Alternatively, the first locking member is provided with a first locking hole, the second locking member is provided with a second locking hole, and the first locking member and the second locking member are connected by a locking member passing through the first locking hole and the second locking hole.

[0023] For the cockpit domain controller assembly of the present utility model, by providing a housing cover as the mounting seat of the controller body, a receiving cavity is formed inside the housing cover, and an installation opening is provided on one side of the receiving cavity, so that the controller body can be inserted into the receiving cavity from the installation opening and slide to the locking position inside the receiving cavity. At the locking position, the housing cover and the controller body are locked and fixed through a locking structure, without the need for manual alignment of screw holes, making the installation more convenient and time-saving.

[0024] As can be seen from the above, for the cockpit domain controller assembly of the present utility model, through the sliding fit between the housing cover and the controller body, the controller body can be more conveniently guided to the locking position, and then the fixing installation of the controller body is completed through the locking structure. The installation is more convenient and fast, effectively solving the problems of inconvenient installation, time-consuming and laborious in the prior art for the cockpit domain controller. BRIEF DESCRIPTION OF THE DRAWINGS

[0025] In order to more clearly illustrate the technical solutions in the present utility model or the prior art, the following will briefly introduce the drawings required for use in the description of the embodiments or the prior art. Obviously, the drawings in the following description are some embodiments of the present utility model. For those of ordinary skill in the art, without creative efforts, other drawings can also be obtained based on these drawings.

[0026] Figure 1 It is a schematic diagram of the cockpit domain controller assembly provided by an embodiment of the present utility model.

[0027] Figure 2 It is a schematic diagram of the housing cover provided by an embodiment of the present utility model.

[0028] Figure 3 It is one of the partial schematic diagrams of the controller body and the second locking member provided by an embodiment of the present utility model.

[0029] Figure 4 It is a partial schematic diagram of the controller body and the second locking member provided by another embodiment of the present utility model.

[0030] Figure 5 It is a partial schematic diagram of the controller body and the second locking member provided by still another embodiment of the present utility model.

[0031] Figure 6 It is the second of the partial schematic diagrams of the controller body and the second locking member provided by an embodiment of the present utility model.

[0032] Figure 7It is a schematic diagram of the cooperation among the controller body, the housing, the first locking member and the second locking member provided by the embodiment of the present utility model.

[0033] Figure 8 It is a schematic diagram of the cockpit domain controller assembly provided by another embodiment of the present utility model.

[0034] Figure 9 It is a schematic diagram of the locking structure provided by another embodiment of the present utility model.

[0035] Figure 10 It is a cross-sectional view of the locking structure provided by another embodiment of the present utility model.

[0036] Reference numerals:

[0037] 1. Housing; 11. Accommodating cavity; 111. Guide groove; 1111. Guide section; 1112. Locking section;

[0038] 2. Controller body; 21. Sliding member; 211. Cylinder; 212. Flexible sleeve; 213. Spherical member; 214. Roller;

[0039] 3. Locking structure; 31. First locking member; 311. Buckle portion; 312. First locking hole; 32. Second locking member; 321. Clamping hole; 322. Second locking hole; 33. Limit hook. Detailed implementation manners

[0040] To make the objectives, technical solutions and advantages of the present utility model clearer, the technical solutions in the present utility model will be clearly and completely described below with reference to the accompanying drawings in the present utility model. Apparently, the described embodiments are some but not all of the embodiments of the present utility model. All other embodiments obtained by those of ordinary skill in the art based on the embodiments in the present utility model without making creative efforts fall within the scope of protection of the present utility model.

[0041] The following combines Figures 1 - 10 to describe the cockpit domain controller assembly of the present utility model.

[0042] As Figure 1 and Figure 2 shown, the present utility model provides a cockpit domain controller assembly, including: a housing 1, a controller body 2 and a locking structure 3. The housing 1 has an accommodating cavity 11 and an installation opening communicating with the accommodating cavity 11. The controller body 2 is slidably disposed in the housing 1 through the installation opening, and the controller body 2 can slide to a locking position. The locking structure 3 is disposed between the housing 1 and the controller body 2, and the locking structure 3 is used to realize the locking connection between the housing 1 and the controller body 2 at the locking position.

[0043] In this embodiment, it can be understood that the housing 1 can be integrated on the instrument panel assembly in the cockpit to serve as the mounting seat for the controller body 2. The housing 1 is provided with a receiving cavity 11 which can be used to receive and mount the controller body 2. An installation opening communicating with the receiving cavity 11 is provided on the housing 1 so that the controller body 2 can be placed into the housing 1 through the installation opening.

[0044] It can be understood that structures that can cooperate for relative sliding (such as sliders and chutes, guide posts and guide holes, etc.) are respectively provided on the inner sides of the controller body 2 and the housing 1, enabling the controller body 2 to slide within the receiving cavity 11 and be able to slide to a locking position, which is a preset installation position of the controller body 2.

[0045] Meanwhile, by providing a locking structure 3 between the housing 1 and the controller body 2, when the controller body 2 slides to the locking position, the locking structure 3 can lock and connect the housing 1 and the controller body 2, thereby fixing the controller body 2 within the receiving cavity 11 of the housing 1 and completing the installation and fixation of the controller body 2.

[0046] For the cockpit domain controller assembly of the present utility model, by providing the housing 1 as the mounting seat for the controller body 2, a receiving cavity 11 is formed within the housing 1, and an installation opening is provided on one side of the receiving cavity 11 so that the controller body 2 can be loaded into the receiving cavity 11 from the installation opening and slide within the receiving cavity 11 to the locking position. At the locking position, the housing 1 and the controller body 2 are locked and fixed by the locking structure 3, eliminating the need for manual alignment of screw holes and making the installation more convenient and time-saving.

[0047] As can be seen from the above, for the cockpit domain controller assembly of the present utility model, through the sliding cooperation between the housing 1 and the controller body 2, the controller body 2 can be more conveniently guided to the locking position, and then the fixation and installation of the controller body 2 are completed through the locking structure 3. The installation is more convenient and fast, effectively solving the problems of inconvenient installation, time-consuming and laborious in the prior art for the cockpit domain controller.

[0048] Specifically, in some embodiments, as Figure 1 shown, a guide groove 111 is provided on the inner wall of the receiving cavity 11, and the controller body 2 is provided with a sliding member 21 which is used to slide along the extending direction of the guide groove 111 until the controller body 2 reaches the locking position.

[0049] In this embodiment, by providing a guiding groove 111 on the inner wall of the accommodating cavity 11 and a sliding member 21 adapted to the guiding groove 111 on the controller body 2, after the controller body 2 is inserted into the accommodating cavity 11 from the installation opening, the sliding member 21 is inserted into the guiding groove 111, and the controller body 2 is continuously pushed inward to slide. At the same time, the sliding member 21 slides along the guiding groove 111 to limit the sliding direction of the controller body 2, and finally the controller body 2 is guided to the locking position, so as to facilitate locking and fixing the controller body 2 and the housing 1. The structure is simple and the operation is convenient.

[0050] In a specific embodiment, there are two guiding grooves 111 and two sliding members 21. The two guiding grooves 111 are respectively arranged on opposite sides inside the accommodating cavity 11, and the sliding members 21 and the guiding grooves 111 are arranged in one-to-one correspondence.

[0051] Further, in some embodiments, as Figure 1 and Figure 2 shown, an opening is provided at the first end of the guiding groove 111 facing the installation opening, and the sliding member 21 is adapted to enter the guiding groove 111 from the opening. In the case where the controller body 2 is in the locking position, the sliding member 21 abuts against the second end of the guiding groove 111.

[0052] In this embodiment, by providing an opening at the first end of the guiding groove 111 facing the installation opening, after the controller body 2 is inserted into the accommodating cavity 11 from the installation opening, the sliding member 21 is inserted into the guiding groove 111 from the opening, which is more convenient for installation. After the sliding member 21 is inserted into the guiding groove 111, the controller body 2 is continuously pushed inward to slide. The controller body 2 slides to the locking position under the cooperation and guidance of the sliding member 21 and the guiding groove 111. After the controller body 2 slides to the locking position, the sliding member 21 abuts against the second end of the guiding groove 111, which plays a limiting role on the controller body 2, facilitating the installer to confirm whether the controller body 2 reaches the locking position and keeping the controller body 2 at the locking position, so as to lock and fix the controller body 2 to the housing 1 through the locking structure 3 subsequently, and the installation is more convenient.

[0053] Specifically, in some embodiments, as Figure 1 and Figure 2 shown, the guiding groove 111 includes a connected guiding section 1111 and a locking section 1112. The guiding section 1111 is provided with an opening, and the width of the guiding section 1111 gradually decreases from one end of the opening to the direction of the locking section 1112. In the case where the controller body 2 is in the locking position, the sliding member 21 abuts against the groove wall of the locking section 1112.

[0054] In this embodiment, by dividing the guiding groove 111 into a guiding section 1111 and a locking section 1112, an opening is provided in the guiding section 1111 so that the sliding member 21 can be loaded into the guiding section 1111 and guided to slide towards the locking section 1112. The width of the guiding section 1111 gradually decreases in the direction from one end of the opening towards the locking section 1112, making the guiding section 1111 form a groove section that tapers from the outside to the inside, with a relatively large width of the opening of the guiding section 1111, which facilitates the installer to load the sliding member 21 into the guiding section 1111 through the opening. When the sliding member 21 slides inward along the guiding section 1111, the width of the guiding section 1111 gradually decreases, so as to better limit and guide the sliding member 21, enabling the sliding member 21 to smoothly slide into the locking section 1112. The groove wall of the locking section 1112 abuts against the sliding member 21 to limit the sliding member 21, facilitating the installer to confirm whether the controller body 2 reaches the locking position and keeping the controller body 2 at the locking position, which is convenient for subsequently fixing and locking the controller body 2 and the housing 1.

[0055] It can be understood that the groove shape of the locking section 1112 can be adapted to the outer shape of the sliding member 21, so that the groove wall of the locking section 1112 can surround and fit the sliding member 21.

[0056] Optionally, in some embodiments, as Figure 1 and Figure 3 shown, the sliding member 21 includes a cylinder 211 and a flexible sleeve 212. The cylinder 211 is arranged on the controller body 2, and the flexible sleeve 212 is sleeved on the cylinder 211. The flexible sleeve 212 is in sliding fit with the groove wall of the guiding groove 111.

[0057] In this embodiment, by sleeving the flexible sleeve 212 on the cylinder 211, when the sliding member 21 slides along the guiding groove 111, the cylinder 211 contacts the groove wall of the guiding groove 111 through the flexible sleeve 212, which can make the sliding of the sliding member 21 smoother. At the same time, the flexible sleeve 212 can also play a buffering role between the groove wall of the guiding groove 111 and the cylinder 211, avoiding the collision between the cylinder 211 and the groove wall of the guiding groove 111 from generating vibration or noise and causing damage to the cylinder 211 and the guiding groove 111.

[0058] Further, when the controller body 2 is in the locking position, the cylinder 211 and the flexible sleeve 212 can be in interference fit with the groove wall of the guiding groove 111 to fix the cylinder 211 and the controller body 2 in their corresponding positions. The cylinder 211 abuts against the guiding groove 111 through the flexible sleeve 212, thereby playing a buffering role between the groove wall of the guiding groove 111 and the cylinder 211, reducing the vibration and noise between the controller body 2 and the housing 1 during subsequent use.

[0059] Optionally, in another embodiment, as Figure 4As shown, the sliding member 21 includes a cylinder 211 and a spherical member 213. The first end of the cylinder 211 is connected to the controller body 2, the second end of the cylinder 211 is connected to the spherical member 213, and the groove wall of the guiding groove 111 is an arc-shaped groove wall that fits the spherical member 213; the spherical member 213 is in sliding fit with the groove wall of the guiding groove 111.

[0060] In this embodiment, by providing the cylinder 211 on the controller body 2 and connecting a spherical member 213 to the end of the cylinder 211 away from the controller body 2, when the sliding member 21 slides along the guiding groove 111, the spherical member 213 is in contact and cooperation with the guiding groove 111, and the groove wall of the guiding groove 111 is an arc-shaped surface that fits the spherical member 213, so as to increase the contact area between the spherical member 213 and the groove wall of the guiding groove 111, reduce the sway of the spherical member 213 in the depth direction of the guiding groove 111, and make the limiting of the spherical member 213 by the guiding groove 111 more stable and reliable.

[0061] Optionally, in another embodiment, as Figure 5 shown, the sliding member 21 includes a roller 214, and the roller 214 is rotatably provided on the controller body 2 and is in rolling fit with the groove wall of the guiding groove 111.

[0062] In this embodiment, by providing a rotatable roller 214 on the controller body 2, when the controller body 2 slides relative to the housing 1, the roller 214 can roll along the groove wall of the guiding groove 111. While realizing the guiding function, the frictional resistance between the sliding member 21 and the groove wall of the guiding groove 111 is reduced, which is more convenient and labor-saving.

[0063] In some embodiments, as Figure 1 and Figure 2 shown, the locking structure 3 includes a first locking member 31 and a second locking member 32. The first locking member 31 is provided at the installation opening, and the second locking member 32 is provided on the controller body 2. In the case where the controller body 2 is in the locked position, the first locking member 31 and the second locking member 32 are locked and connected.

[0064] In this embodiment, by providing the first locking member 31 at the installation opening in the housing 1 and providing the second locking member 32 on the controller body 2, when the controller body 2 is inserted into the accommodation cavity 11 from the installation opening and slides to the locked position, the first locking member 31 and the second locking member 32 cooperate with each other to lock, thereby fixing the controller body 2 and the housing 1 to each other. At the same time, since the first locking member 31 is provided at the installation opening, when the controller body 2 slides to the locked position, the second locking member 32 also moves to a position close to the first locking member 31, and both the first locking member 31 and the second locking member 32 are located at the installation opening, which is convenient for the installer to lock and connect the first locking member 31 and the second locking member 32 to each other.

[0065] In some embodiments, asFigure 1 , Figure 2 , Figure 6 and Figure 7 As shown in Figure 6 and Figure 7 , there are two first locking members 31, and the two first locking members 31 are respectively arranged on opposite sides of the installation opening. There are two second locking members 32, and they are arranged in one-to-one correspondence with the two first locking members 31. A limit hook 33 is arranged on each second locking member 32; when the controller body 2 is in the locked position, the limit hook 33 abuts against the first locking member 31.

[0066] In this embodiment, by respectively arranging one first locking member 31 on opposite sides of the installation opening and correspondingly arranging two second locking members 32 on the controller body 2, when the controller body 2 moves to the locked position, the two first locking members 31 and the two second locking members 32 are locked with each other in one-to-one correspondence, so that both sides of the controller body 2 are locked and fixed to both sides of the installation opening respectively, making the connection between the controller body 2 and the housing 1 more stable and reliable. At the same time, by arranging the limit hook 33 on the second locking member 32, when the controller body 2 moves to the locked position, the limit hook 33 abuts against the first locking member 31, restricting the relative positions of the second locking member 32 and the first locking member 31, enabling the second locking member 32 and the first locking member 31 to be aligned with each other for locking connection, and ensuring that the controller body 2 moves to the predetermined locked position. The structure is simple, convenient and practical.

[0067] In a specific embodiment, as Figure 1 and Figure 7 shown, when the controller body 2 is in the locked position, the limit hook 33 abuts against the side of the first locking member 31 away from the inner wall of the installation opening. The two limit hooks 33 are located between the two first locking members 31 and respectively abut against the first locking members 31 on both sides, which can limit the controller body 2 and prevent the controller body 2 from laterally shifting relative to the installation opening.

[0068] Optionally, in some embodiments, as Figure 8 , Figure 9 and Figure 10 shown, one of the first locking member 31 and the second locking member 32 is provided with a clamping hole 321, and at the position corresponding to the clamping hole 321 on the other one, a clamping portion 311 is provided; when the controller body 2 is in the locked position, the clamping portion 311 is clamped in the clamping hole 321.

[0069] In this embodiment, by respectively providing mating buckle portions 311 and latching holes 321 on the first locking member 31 and the second locking member 32, when the controller body 2 slides to the locking position, the buckle portion 311 is inserted into the latching hole 321 and latches with the latching hole 321, thereby locking and connecting the first locking member 31 and the second locking member 32, and further fixing the controller body 2 to the housing 1, which is convenient for disassembly and assembly.

[0070] It can be understood that the positions of the buckle portion 311 and the latching hole 321 can be swapped according to requirements. For example, the buckle portion 311 is provided on the first locking member 31, and correspondingly, the latching hole 321 is provided on the second locking member 32; or, the buckle portion 311 can also be provided on the second locking member 32, and correspondingly, the latching hole 321 is provided on the first locking member 31.

[0071] Optionally, in some other embodiments, as Figure 8 、 Figure 9 and Figure 10 shown, the first locking member 31 is provided with a first locking hole 312, the second locking member 32 is provided with a second locking hole 322, and the first locking member 31 and the second locking member 32 are connected by a locking member passing through the first locking hole 312 and the second locking hole 322.

[0072] In this embodiment, by respectively providing the first locking hole 312 and the second locking hole 322 on the first locking member 31 and the second locking member 32, when the controller body 2 slides to the locking position, the first locking hole 312 and the second locking hole 322 are aligned with each other, so as to sequentially pass the locking member through the first locking hole 312 and the second locking hole 322, thereby locking and fixing the first locking member 31 and the second locking member 32.

[0073] In a specific embodiment, the locking member can be a fastening bolt, and the first locking hole 312 and the second locking hole 322 can be screw holes adapted to the fastening bolt.

[0074] Finally, it should be noted that the above embodiments are only used to illustrate the technical solutions of the present invention, rather than to limit them; although the present invention has been described in detail with reference to the foregoing embodiments, those of ordinary skill in the art should understand that they can still modify the technical solutions recorded in the foregoing embodiments, or perform equivalent replacements for some of the technical features; and these modifications or replacements do not make the essence of the corresponding technical solutions deviate from the spirit and scope of the technical solutions of the various embodiments of the present invention.

Claims

1. A cockpit domain controller component, characterized in that, Comprising: A housing cover and a controller body. The housing cover has a receiving cavity and an installation opening communicating with the receiving cavity. The controller body is slidably disposed in the housing cover through the installation opening, and the controller body can slide to a locking position. A locking structure is disposed between the housing cover and the controller body. The locking structure is used to realize the locking connection between the housing cover and the controller body at the locking position.

2. The cockpit domain controller assembly according to claim 1, wherein, A guiding groove is provided on the inner wall of the receiving cavity, and a sliding member is provided on the controller body. The sliding member is used to slide along the extending direction of the guiding groove until the controller body reaches the locking position.

3. The cockpit domain controller component according to claim 2, wherein, The first end of the guiding groove facing the installation opening is provided with an opening, and the sliding member is used to enter the guiding groove from the opening. When the controller body is in the locking position, the sliding member abuts against the second end of the guiding groove.

4. The cockpit domain controller assembly according to claim 3, characterized in that The guiding groove includes a connected guiding section and a locking section. The guiding section is provided with the opening, and the width of the guiding section gradually decreases from one end of the opening to the direction of the locking section. When the controller body is in the locking position, the sliding member abuts against the groove wall of the locking section.

5. The cockpit domain controller assembly according to any one of claims 2 to 4, characterized in that, The sliding member includes a cylinder and a flexible sleeve. The cylinder is disposed on the controller body, and the flexible sleeve is sleeved on the cylinder. The flexible sleeve is in sliding fit with the groove wall of the guiding groove.

6. The cockpit domain controller assembly according to any one of claims 2 to 4, characterized in that, The sliding member includes a cylinder and a spherical member. The first end of the cylinder is connected to the controller body, and the second end of the cylinder is connected to the spherical member. The groove wall of the guiding groove is an arc-shaped groove wall that fits the spherical member. The spherical member is in sliding fit with the groove wall of the guiding groove.

7. The cockpit domain controller assembly according to any one of claims 2 to 4, characterized in that, The sliding member includes a roller. The roller is rotatably disposed on the controller body and is in rolling fit with the groove wall of the guiding groove.

8. The cockpit domain controller assembly according to any one of claims 1 to 4, characterized in that The locking structure includes a first locking member and a second locking member. The first locking member is disposed at the installation opening, and the second locking member is disposed on the controller body. When the controller body is in the locking position, the first locking member and the second locking member are locked and connected.

9. The cockpit domain controller component according to claim 8, characterized in that, There are two first locking members, and the two first locking members are respectively disposed on opposite sides of the installation opening. There are two second locking members, which are arranged in one-to-one correspondence with the two first locking members. A limiting hook is provided on each second locking member. When the controller body is in the locking position, the limiting hook abuts against the first locking member.

10. The cockpit domain controller assembly according to claim 8, characterized in that, One of the first locking member and the second locking member is provided with a clamping hole, and a clamping portion is provided at a position corresponding to the clamping hole on the other. When the controller body is in the locking position, the clamping portion is clamped in the clamping hole. Alternatively, the first locking member is provided with a first locking hole, the second locking member is provided with a second locking hole, and the first locking member and the second locking member are connected by a locking member passing through the first locking hole and the second locking hole.

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