Star chain terminal fixing mechanism and star chain terminal device
By designing a Starlink terminal fixing mechanism, the Starlink terminal is enclosed in a receiving slot using a housing and a shield, which solves the problem of Starlink terminals being damaged by hail and rain on vehicles and achieves effective protection.
Patent Information
- Application Number
- CN202520386122.2
- Authority / Receiving Office
- CN · China
- Patent Type
- Utility models(China)
- Current Assignee / Owner
- Filing Date
- 2025-03-06
- Publication Date
- 2026-02-27
- Estimated Expiration
- 2035-03-06
AI Technical Summary
When Starlink terminals are used on vehicles, they are easily damaged by hail and rain.
Design a Starlink terminal fixing mechanism, including a housing and a shielding part. The housing forms a receiving groove and an opening, and the shielding part closes the opening. The housing is fitted with the Starlink terminal and the shielding part encloses it in the receiving groove to prevent hail and rainwater from contacting it.
Effectively prevents damage to Starlink terminals from hail and rain, protecting them from external environmental erosion.
Smart Images

Figure CN223957561U_ABST
Abstract
Description
TECHNICAL FIELD
[0001] The utility model relates to star chain terminal fixing technical field, concretely relates to a star chain terminal fixing mechanism and star chain terminal device. BACKGROUND
[0002] A satellite terminal refers to a device used for data exchange with a communication satellite, which can send and receive signals from the satellite, thereby realizing functions such as long-distance communication, broadcasting, internet access, etc. For example, in the Starlink satellite network project, users need to use a specific type of satellite terminal (also known as a Starlink terminal, satellite antenna or satellite dish), which is specially designed to connect to a low earth orbit satellite cluster to provide high-speed internet services.
[0003] When the Starlink terminal is placed on a vehicle for use, it is usually placed directly on the top of the vehicle outside to avoid blocking the radio signal.
[0004] When the Starlink terminal is used on a vehicle, it is directly exposed to the outside and may be damaged by hail and rain erosion. SUMMARY
[0005] The utility model aims at overcoming the above technical deficiencies and proposes a Starlink terminal fixing mechanism and Starlink terminal device to solve the technical problem that the Starlink terminal may be damaged by hail and rain erosion in the prior art.
[0006] To achieve the above technical purpose, the utility model adopts the following technical scheme:
[0007] In a first aspect, the utility model provides a Starlink terminal fixing mechanism, comprising:
[0008] a housing formed with a receiving groove and a first opening communicating with the receiving groove, for sleeving a Starlink terminal through the receiving groove and the first opening; and
[0009] a shielding part connected to the housing and closing the first opening of the receiving groove.
[0010] In one embodiment, the size of the receiving groove matches the size of the Starlink terminal.
[0011] In one embodiment, the shielding part is detachably connected to the housing.
[0012] In one embodiment, the housing is externally provided with a cable passage communicating with the receiving groove.
[0013] In one embodiment, the housing is formed with a stepped groove, which is spaced from the receiving groove and arranged around the receiving groove.
[0014] In one of the embodiments, a reinforcing block is arranged at the corner of the stepped groove.
[0015] In one of the embodiments, a strip-shaped groove and / or a through hole are arranged on the side of the shell away from the opening.
[0016] The star chain terminal fixing mechanism further comprises a connecting part, which partially penetrates through the strip-shaped groove or the through hole and is connected with the shell, and the connecting part is any one of an adhesive part, a suction cup part and a magnetic part.
[0017] In one of the embodiments, the star chain terminal fixing mechanism further comprises a sealing ring, which is arranged between the shell and the shielding part.
[0018] In one of the embodiments, the shielding part is provided with a fixing hole relative to the sealing ring.
[0019] The star chain terminal fixing mechanism further comprises a fixing part, one part of which penetrates through the fixing hole and the sealing ring and is connected with the shell, and the other part of the fixing part abuts against the side of the shielding part away from the shell.
[0020] In the second aspect, the utility model further provides a star chain terminal device, which comprises the above-mentioned star chain terminal fixing mechanism and a star chain terminal covered by the shell and the shielding part.
[0021] Compared with the prior art, the star chain terminal fixing mechanism and the star chain terminal device provided by the utility model can avoid the contact of hail and rain with the star chain terminal in the star chain terminal fixing mechanism and the damage of hail and rain to the star chain terminal by arranging the shell, sleeving the star chain terminal in the shell through the first opening and the accommodating groove and then enclosing the star chain terminal in the accommodating groove through the shielding part. BRIEF DESCRIPTION OF DRAWINGS
[0022] Figure 1 is an exploded view of the star chain terminal device provided by an embodiment of the utility model;
[0023] Figure 2 is a structural schematic view of the star chain terminal fixing mechanism provided by an embodiment of the utility model;
[0024] Figure 3 is a structural schematic view of the shell in the star chain terminal fixing mechanism provided by an embodiment of the utility model;
[0025] Figure 4 is a structural schematic view of the shell in the star chain terminal fixing mechanism provided by an embodiment of the utility model;
[0026] Figure 5It is the structural schematic view of the shielding part in the star chain terminal fixing mechanism provided by an embodiment of the utility model.
[0027] Figure 6 It is the structural schematic view of the star chain terminal in the star chain terminal fixing device provided by an embodiment of the utility model.
[0028] Mark explanation:
[0029] The shell 1, the containing groove 1a, the first opening 1b, the second opening 1c, the cable passage 1d, the stepped groove 1e, the strip-shaped groove 1f, the through-hole 1g,
[0030] The shielding part 2, the fixing hole 2a,
[0031] The star chain terminal 3,
[0032] The reinforcing block 4,
[0033] The sealing ring 5,
[0034] The fixing part 6. Specific embodiment
[0035] In order to make the purpose, technical scheme and advantages of the utility model more clearly, the utility model is further explained in detail below by combining with the drawings and examples.It should be understood that the specific examples described here are only used to explain the utility model and not to limit the utility model.
[0036] In order to solve the technical problem that the satellite terminal can be damaged by foreign matter impact, the utility model provides a kind of star chain terminal fixing mechanism and star chain terminal device, can avoid foreign matter impact star chain terminal, avoid that star chain terminal is damaged by impact.
[0037] It should be noted that the star chain terminal fixing mechanism described in the utility model is used but not limited to vehicle-mounted star chain terminal, in order to facilitate explanation, in the utility model, only with star chain terminal fixing mechanism is applied to vehicle-mounted star chain terminal as an example to explain, and the principle of star chain terminal fixing mechanism fixed on other equipment is substantially same with the principle applied to vehicle-mounted star chain terminal, not repeated here.
[0038] Please refer to Figure 1 , Figure 1 It is the explosion view of the star chain terminal fixing device in an embodiment of the utility model, and the star chain terminal fixing mechanism includes shell 1 and shielding part 2, the shell 1 is formed with containing groove 1a and the first opening 1b being communicated with containing groove 1a, for the star chain terminal 3 being set through containing groove 1a and first opening 1b;Shielding part 2 is connected with shell 1, and the first opening 1b of containing groove 1a is closed.
[0039] By setting the shell 1, the shell 1 can be sleeved on the star chain terminal 3 through the first opening 1b and the accommodating groove 1a, and then the star chain terminal 3 is enclosed in the accommodating groove 1a by the shielding part 2, so that the hail and rain can be prevented from contacting the star chain terminal 3 in the star chain terminal fixing mechanism, and the hail and rain can be prevented from damaging the star chain terminal 3.
[0040] It should be understood that the star chain terminal fixing mechanism is used for but not limited to fixing and protecting the vehicle-mounted star chain terminal, and the star chain terminal fixing mechanism can be fixed on a building or the like.
[0041] It should be understood that the star chain terminal 3 refers to a hardware device used by a user to access the SpaceX star chain satellite Internet system. It is an interface between the user and the star chain satellite network, responsible for receiving and sending data, enabling the user to access Internet services.
[0042] It should be understood that the shape of the shielding part 2 can be plate-shaped, rectangular, square, circular, etc., and the material of the shielding part 2 can be glass, acrylic, etc. Specifically, as shown in Figure 5 in one embodiment, the shielding part 2 is square, and the shielding part 2 is made of light-transmitting acrylic material.
[0043] It should be understood that the shell 1 can only have the first opening 1b, or other openings can be provided, such as Figure 3 in one embodiment, the side of the shell 1 away from the shielding part 2 has a second opening 1c, and the second opening 1c communicates with the accommodating groove 1a.
[0044] By providing the second opening 1c, the second opening 1c can accommodate excess cables, and the second opening 1c can also be used for heat dissipation of the star chain terminal 3 outward; at the same time, when the shell 1 is fixed to the vehicle, the second opening 1c faces the vehicle, and the rain flows downward under the action of gravity and is not easy to enter the accommodating groove 1a from the second opening 1c.
[0045] It should be understood that the size of the accommodating groove 1a can be greater than, less than or equal to the size of the star chain terminal 3. When the size of the accommodating groove 1a is greater than the size of the star chain terminal 3, the star chain terminal 3 can move in the accommodating groove 1a, and when the size of the accommodating groove 1a is less than the size of the star chain terminal 3, the star chain terminal 3 needs to be enclosed together with the shielding part 2.
[0046] Specifically, as shown in Figure 1 in one embodiment, the size of the accommodating groove 1a cooperates with the size of the star chain terminal 3.
[0047] In this embodiment, by matching the size of the receiving groove 1a with that of the Starlink terminal 3, the Starlink terminal 3 can be fixed by the receiving groove 1a when it is built into the receiving groove 1a, thus preventing the Starlink terminal 3 from shaking or moving relative to the housing 1 and achieving the limitation of the Starlink terminal 3.
[0048] For different models and versions of Starlink Terminal 3, a receiving slot 1a can be designed to match different models of Starlink Terminal 3. Models of Starlink Terminal 3 include UTA-201, UTA-211, UTA-212, etc., as shown in the figure. Figure 6 As shown, in one embodiment, the receiving slot 1a is coupled with a Starlink terminal 3 of model UTA-212.
[0049] To facilitate the removal of Starlink Terminal 3 and the replacement of the Starlink Terminal fixing mechanism, therefore, as follows: Figure 2 As shown, in one embodiment, the shielding part 2 is detachably connected to the housing 1.
[0050] When it is necessary to connect Starlink Terminal 3 to Starlink Terminal Fixing Mechanism, Starlink Terminal 3 is placed inside Housing 1, and then the shielding part 2 is connected to Housing 1. At this time, the shielding part 2 encloses Starlink Terminal 3 inside Housing 1. When Starlink Terminal Fixing Mechanism is no longer needed or needs to be replaced, the shielding part 2 is removed from Housing 1. At this time, Starlink Terminal 3 can be taken out from Receiving Slot 1a through the first opening 1b, and then a new Starlink Terminal Fixing Mechanism can be replaced.
[0051] It should be understood that the shielding part 2 and the housing 1 can be detachably connected by bolts, screws and clips.
[0052] The back of the Starlink Terminal 3 typically requires a power cord and a network cable to be connected. To facilitate this connection, the following steps are necessary: Figure 3 and Figure 4 As shown, in one embodiment, the outer side of the housing 1 has a cable channel 1d that communicates with the receiving groove 1a.
[0053] In this embodiment, when it is necessary to connect the power cord and network cable to the Starlink terminal 3, the cable is passed through the cable channel 1d into the housing 1 and connected to the Starlink terminal 3 inside the housing 1.
[0054] It should be understood that the cable channel 1d can be a notch, through hole, or through groove opened in the housing 1.
[0055] In order to reduce the weight of shell 1, therefore, as Figure 4 As shown, in one embodiment, the housing 1 is formed with a stepped groove 1e, which is spaced apart from and surrounds the receiving groove 1a.
[0056] In this embodiment, by arranging the stepped groove 1e in the shell 1, the weight of the shell 1 can be reduced without reducing the outer diameter of the shell 1.
[0057] As shown in Figure 4 , the stepped groove 1e penetrates one side of the shell 1, and the penetration direction is opposite to the opening direction of the first opening 1b. The cable passage 1d is in communication with the stepped groove 1e.
[0058] Since the stepped groove 1e is arranged in the shell 1, the structural strength of the shell 1 is affected. Therefore, as shown in Figure 4 , in one embodiment, a reinforcing block 4 is arranged at the corner of the stepped groove 1e.
[0059] By arranging the reinforcing block 4 in the stepped groove 1e, the structural strength of the corner of the stepped groove 1e can be strengthened.
[0060] It should be understood that the reinforcing block 4 can be square, triangular, etc. The number of reinforcing blocks 4 can be one, two, and multiple, etc. The number of reinforcing blocks 4 is arranged according to the required structural strength.
[0061] In order to fix the shell 1 to the vehicle, as shown in Figure 3 and Figure 4 , in one embodiment, a strip-shaped groove 1f and / or a through hole 1g are arranged on the side of the shell 1 opposite to the opening; the star chain terminal fixing mechanism further comprises a connecting part (not shown in the figure), which partially penetrates the strip-shaped groove 1f or the through hole 1g and is connected to the shell 1. The connecting part is any one of an adhesive, a suction cup, and a magnetic suction piece.
[0062] When it is necessary to connect the shell 1 to the vehicle, the connecting part is partially penetrated through the strip-shaped groove 1f and the through hole 1g, then the connecting part is connected to the shell 1, and finally the connecting part is fixed to the vehicle, thereby realizing the connection between the shell 1 and the connecting part.
[0063] It should be understood that the connecting part can be any one of an adhesive (not shown in the figure), a suction cup (not shown in the figure), and a magnetic suction piece (not shown in the figure). The adhesive can be a solid adhesive block or double-sided tape, which can be directly adhered to the glass and metal cover of the vehicle. The suction cup can be a combination of one or more suction cups, which can be adsorbed on the glass and metal cover of the vehicle, and the suction cup and the shell 1 can be connected by bolts, screws, buckles, etc. The magnetic suction piece can be an electromagnet or a permanent magnet, which can be magnetically attracted to the metal cover of the vehicle. The connecting part has bolts, screws, buckles, etc. The threaded ends of the bolts and screws penetrate the strip-shaped groove 1f and / or the through hole 1g, and are connected to the suction cup and the permanent magnet in the connecting part, so as to realize the connection between the connecting part and the shell 1.
[0064] It should be understood that the connecting part can also be connected to the shielding part 2 so that the Starlink terminal fixing mechanism can be fixed to the vehicle through the shielding part 2 and the connecting part.
[0065] To enhance the sealing between the shielding part 2 and the housing 1, therefore, as follows: Figure 1 As shown, in one embodiment, the Starlink terminal fixing mechanism further includes a sealing ring 5, which is disposed between the housing 1 and the shielding part 2.
[0066] In this embodiment, a sealing ring 5 is provided between the housing 1 and the shielding part 2. The sealing ring 5 can seal any gaps that may exist between the housing 1 and the shielding part 2, so as to prevent moisture and dust from seeping inward from between the housing 1 and the shielding part 2.
[0067] It should be understood that the cross-section of the sealing ring 5 can be U-shaped, O-shaped, square, strip-shaped, etc.
[0068] When the shielding part 2 is connected to the housing 1, in order to seal the connection, for example... Figure 1 and Figure 5 As shown, in one embodiment, the shielding part 2 has a fixing hole 2a opposite to the sealing ring 5; the Starlink terminal fixing mechanism also includes a fixing part 6, a part of the fixing part 6 passes through the fixing hole 2a and the sealing ring 5 and is connected to the housing 1, and the other part of the fixing part 6 abuts against the side of the shielding part 2 away from the housing 1.
[0069] When it is necessary to connect the housing 1 and the shielding part 2, a part of the fixing part 6 passes through the fixing hole 2a and the sealing ring 5 and is connected to the housing 1, thus realizing the connection between the fixing part 6 and the shielding part 2. At the same time, since the fixing part 6 needs to pass through the shielding part 2, a fixing hole 2a needs to be opened on the shielding part 2, which may pose a risk of rainwater penetration at the fixing hole 2a position of the shielding part 2. In this embodiment, the fixing hole 2a is set relative to the sealing ring 5, and the shielding part 2 passes through the sealing ring 5. The sealing ring 5 can seal the fixing hole 2a and the passage of the fixing part 6, further preventing rainwater from penetrating into the housing 1.
[0070] The fixing part 6 can be a screw, bolt, or clip.
[0071] like Figure 1 As shown, this utility model also relates to a Starlink terminal device, including the aforementioned Starlink terminal fixing mechanism and a Starlink terminal 3 covered by the housing 1 and the shielding part 2. Since this Starlink terminal device adopts the Starlink terminal fixing mechanism in the above embodiments, the technical effects of this Starlink terminal device are explained in the above embodiments.
[0072] In the description of the utility model, it is necessary to understand that the orientation or positional relation indicated by the terms "center", "upper", "lower", "front", "rear", "left", "right", "vertical", "horizontal", "top", "bottom", "inner", "outer" and the like is the orientation or positional relation shown based on the drawings, and is only for the convenience of describing the utility model and simplifying the description, and does not indicate or imply that the device or element indicated must have a particular orientation, be constructed and operated in a particular orientation, and therefore cannot be understood as a limitation on the utility model.
[0073] The terms "first", "second", "third", etc. are only used for the purpose of description, and cannot be understood as indicating or implying relative importance or implicitly indicating the number of the technical features indicated.
[0074] In the description of the utility model, it should be explained that, unless otherwise explicitly specified and limited, the terms "mounting", "connection", "connecting" should be understood in a broad sense, for example, can be fixedly connected, can be detachably connected, or integrally connected, can be directly connected, or indirectly connected through an intermediate medium, and can be the communication inside two elements.
[0075] In the description of the specification, specific features, structures, materials or characteristics can be combined in any one or more embodiments or examples in a suitable manner.
[0076] The specific embodiments of the utility model described above do not constitute a limitation on the protection scope of the utility model. Any various other corresponding changes and modifications made according to the technical concept of the utility model should be included in the protection scope of the claims of the utility model.
Claims
1. A satellite chain terminal fixing mechanism characterized by comprising: The star chain terminal fixing mechanism comprises: a housing, which is formed with a receiving groove and a first opening in communication with the receiving groove, and is used for sleeving the star chain terminal through the receiving groove and the first opening; and a shielding part, which is connected with the housing and closes the first opening of the receiving groove.
2. The star chain terminal fixing mechanism according to claim 1, wherein the size of the receiving groove is matched with the size of the star chain terminal.
3. The star chain terminal fixing mechanism according to claim 1, wherein the shielding part is detachably connected with the housing.
4. The star chain terminal fixing mechanism according to claim 1, wherein a cable passage in communication with the receiving groove is formed on the outside of the housing.
5. The star chain terminal fixing mechanism according to claim 1, wherein the housing is formed with a stepped groove, which is spaced from the receiving groove and is arranged around the receiving groove.
6. The star chain terminal fixing mechanism according to claim 5, wherein a reinforcing block is arranged at the corner of the stepped groove.
7. The star chain terminal fixing mechanism according to claim 1, wherein a strip-shaped groove and / or a through hole are formed on the side of the housing away from the opening; the star chain terminal fixing mechanism further comprises a connecting part, which partially penetrates through the strip-shaped groove or the through hole and is connected with the housing, and the connecting part is any one of an adhesive member, a suction disc member and a magnetic member.
8. The star chain terminal fixing mechanism according to claim 1, wherein a sealing ring is further arranged between the housing and the shielding part.
9. The star chain terminal fixing mechanism according to claim 8, wherein a fixing hole is formed in the shielding part relative to the sealing ring; the star chain terminal fixing mechanism further comprises a fixing part, one part of which penetrates through the fixing hole and the sealing ring and is connected with the housing, and the other part of the fixing part abuts against the side of the shielding part away from the housing.
10. A star chain terminal device, characterized by comprising: The star chain terminal fixing mechanism and the star chain terminal covered by the housing and the shielding part are included.