CN219320479U - Radar installation component and monitoring device - Google Patents

Abstract

The application discloses radar installation component and monitoring device, radar installation component includes: a first housing; the rotating piece is arranged in the first shell and is provided with a first concave part and a second concave part communicated with the first concave part; the radar equipment comprises a second shell and a rotating piece arranged on the second shell, wherein the second shell is positioned outside the first shell, the rotating piece penetrates through the first shell and is positioned in the first concave part, rotating parts are arranged at two ends of the rotating piece and can rotate in the first concave part, and the rotating parts can be inserted into the second concave part. The radar installation component can realize different angle adjustment of radar equipment, and is simple in structure.

Description

Radar installation component and monitoring device

Technical Field

The application relates to the technical field of security protection, in particular to a radar installation component and a monitoring device.

Background

The existing monitoring device is provided with a radar component besides a camera component. The radar component can make up for the functional defect that the camera component cannot acquire parameters such as the speed, the distance and the like of the moving object. However, because the radar component and the camera component are integrally connected, the radar component can only be adjusted in a linkage way along with the movement of the camera component, and cannot be adjusted by itself.

Disclosure of Invention

The application provides a radar installation component and monitoring device to solve in the current monitoring device because of radar subassembly and subassembly as an organic whole of making a video recording is connected, the radar subassembly only can be along with the subassembly motion of making a video recording and the linkage is adjusted, and the technical scheme of unable self regulation.

To solve the above technical problem, the present application proposes a radar installation assembly, including: a first housing; the rotating piece is arranged in the first shell and is provided with a first concave part and a second concave part communicated with the first concave part; the radar equipment comprises a second shell and a rotating piece arranged on the second shell, wherein the second shell is positioned outside the first shell, the rotating piece penetrates through the first shell and is positioned in the first concave part, rotating parts are arranged at two ends of the rotating piece and can rotate in the first concave part, and the rotating parts can be inserted into the second concave part.

The rotating part comprises two first arc surfaces which are oppositely arranged and two first side walls which are oppositely arranged, the two first arc surfaces and the first concave part are coaxially arranged, the distance between two ends of the first arc surfaces is smaller than or equal to the distance between two side walls of the second concave part, and the first side walls are matched with the side walls of the second concave part.

Wherein, first depressed part both sides wall is provided with two second arc surfaces, and two second arc surfaces and two first arc surfaces coaxial settings, and the second depressed part is including the second lateral wall of relative setting, and the second lateral wall matches with first lateral wall, and the one end of second arc surface is connected with the one end of second lateral wall.

The first side wall is a plane, the second side wall is a plane, and the first side wall and the second side wall are arranged in parallel.

The positioning piece is detachably and elastically clamped in the rotating piece and the first shell.

Wherein, one end face of the rotating part, which is away from the rotating part, is provided with a connecting surface, and the connecting surface is concavely provided with a connecting groove; the locating piece includes the location body and sets up in the first locating pin of location body, and first locating pin releasable formula elasticity joint is in the connection recess.

Wherein, a locating hole is arranged on one side surface of the rotating piece, which is close to the locating piece; the locating piece comprises a locating body and a second locating pin arranged on the locating body, and the second locating pin is detachably and elastically clamped in the locating hole.

The transverse section of the rotating piece is circular, the positioning holes comprise at least two positioning holes, and the at least two positioning holes are circumferentially arranged on the rotating piece; when the rotating piece rotates, the second locating pin can be clamped in different locating holes.

The positioning piece comprises a positioning body and a third positioning pin, the third positioning pin is arranged on one side surface of the positioning body, which is away from the rotating piece, one end of the elastic piece is connected in the first shell, and the other end of the elastic piece is connected to the positioning body and sleeved on the third positioning pin.

The first shell comprises a first sub-shell body and a second sub-shell body which is connected with the first sub-shell body in a disassembling mode, a moving groove is formed in the second sub-shell body, a poking rod is arranged at one end, deviating from the first sub-shell body, of the locating piece, and the poking rod penetrates through the moving groove and protrudes out of the surface, deviating from the first sub-shell body, of the second sub-shell body.

The first sub-shell is provided with a third concave part in a concave mode, the second sub-shell is detachably arranged in the third concave part, the bottom of the third concave part is provided with a fourth concave part and two fifth concave parts communicated with the fourth concave part, the two fifth concave parts are located at two ends of the fourth concave part, the rotating part is arranged in the fourth concave part, and the positioning part is arranged in the corresponding fifth concave part.

For solving the above technical problem, the present application proposes a monitoring device, including: a camera assembly; the radar installation assembly is characterized in that the first shell in the radar installation assembly is installed on the camera shooting assembly.

The beneficial effects of this application are: in other words, the radar mounting assembly comprises a first housing, a rotating member and radar equipment. The rotating piece is arranged in the first shell. The rotating piece is provided with a first concave part and a second concave part communicated with the first concave part. The radar apparatus includes a second housing and a rotating member provided to the second housing. The second housing is located outside the first housing. The rotating piece penetrates through the first shell and is positioned in the first concave part. The rotating parts are arranged at the two ends of the rotating piece. The radar equipment changes from a first state to a second state, the rotating part can rotate in the first concave part, and then the rotating part can be inserted in the second concave part. The rotating part rotates relative to the first concave part in the rotating part, and then the rotating part is inserted into the second concave part. Namely, the radar equipment is adjusted at different angles by rotating and inserting the rotating piece relatively, so that the structure is simple, and no external tool is needed.

Drawings

For a clearer description of the technical solutions in the embodiments of the present application, the drawings that are needed in the description of the embodiments will be briefly introduced below, it being obvious that the drawings in the following description are only some embodiments of the present application, and that other drawings may be obtained according to these drawings without inventive effort for a person skilled in the art, wherein:

FIG. 1 is an exploded view of one embodiment of a radar mounting assembly of the present application;

FIG. 2 is a schematic view of a partial explosion of the radar mounting assembly of the present application in a first state;

FIG. 3 is a second partial schematic view of the radar mounting assembly of the present application in a second state;

FIG. 4 is a first partial schematic view of an embodiment of the radar mounting assembly of the present application;

FIG. 5 is a partial side schematic view of a radar apparatus in the radar mounting assembly of the present application;

FIG. 6 is a partial front schematic view of a radar apparatus of the radar mounting assembly of the present application;

FIG. 7 is a schematic partial cross-sectional view of an embodiment of a radar mounting assembly of the present application;

FIG. 8 is a schematic view of the structure of FIG. 7A;

FIG. 9 is a schematic perspective view of a positioning member of the radar mounting assembly of the present application;

FIG. 10 is a schematic view of the construction of a first sub-housing in the radar mounting assembly of the present application;

FIG. 11 is a schematic view of the radar mounting assembly of the monitoring device of the present application in a first state;

fig. 12 is a schematic view of the structure of the radar mounting assembly in the second state in the monitoring device of the present application.

Reference numerals: 10. a radar mounting assembly; 1. a first housing; 11. a first sub-housing; 111. a third recess; 112. a fourth concave portion; 113. a fifth concave portion; 12. a second sub-housing; 121. a moving groove; 2. a radar device; 21. a second housing; 22. a rotating member; 221. a rotating part; 2221. a first arc surface; 2222. a first sidewall; 2223. a connection surface; 2224. a connection groove; 3. a rotating member; 31. a first concave portion; 311. a second arc surface; 32. a second concave portion; 321. a second sidewall; 33. positioning holes; 34. an avoidance groove; 4. a positioning piece; 41. positioning the body; 411. a first positioning pin; 4111. a guide slope; 412. a second positioning pin; 413. a third locating pin; 414. a toggle rod; 415. a mounting groove; 5. an elastic member; 100. a monitoring device; 20. and a camera shooting assembly.

Detailed Description

The following description of the technical solutions in the embodiments of the present application will be made clearly and completely with reference to the accompanying drawings in the embodiments of the present application, and it is apparent that the described embodiments are only some embodiments of the present application, not all embodiments. All other embodiments, which can be made by one of ordinary skill in the art without undue burden from the present disclosure, are within the scope of the present disclosure.

Reference herein to "an embodiment" means that a particular feature, structure, or characteristic described in connection with the embodiment may be included in at least one embodiment of the present application. The appearances of such phrases in various places in the specification are not necessarily all referring to the same embodiment, nor are separate or alternative embodiments mutually exclusive of other embodiments. Those of skill in the art will explicitly and implicitly appreciate that the embodiments described herein may be combined with other embodiments.

The radar mounting assembly and the monitoring device provided by the utility model are described in detail below with reference to the embodiments.

Referring to fig. 1, 2 and 3, fig. 1 is an exploded view of one embodiment of a radar mounting assembly of the present application; FIG. 2 is a schematic view of a partial explosion of the radar mounting assembly of the present application in a first state; fig. 3 is a second partial schematic view of the radar mounting assembly of the present application in a second state. The present application provides a radar mounting assembly 10. The radar mounting assembly 10 includes a first housing 1, a rotating member 3, and a radar apparatus 2. The rotating member 3 is disposed in the first housing 1. The rotation member 3 is provided with a first recess 31 and a second recess 32. The first recess 31 and the second recess 32 are disposed in communication. Wherein the first recess 31 is located at a position above the second recess 32. The radar apparatus 2 includes a second housing 21 and a rotating member 22. The second housing 21 is located outside the first housing 1. The rotating member 22 is inserted from one end of the first housing 1 and is located in the first recess 31, for example, the rotating member 22 is located in the first recess 31 by embedding, clamping, or the like. The rotating member 22 is provided at both ends with rotating portions 221. The rotating portion 221 rotates in the first recess 31 and can be inserted into the second recess 32.

When the radar apparatus 2 is in the first state, the rotation portion 221 is located in the first recess portion 31, and the radar apparatus 2 is disposed on the rotation member 3 in a horizontal state, at which time the first state is a horizontal state. The rotation part 221 may rotate in the first recess 31 during the change of the radar apparatus 2 from the first state to the second state. During the rotation process of the rotating portion 221 relative to the first concave portion 31, the rotating portion 221 may be inserted into the second concave portion 32, and the radar apparatus 2 is disposed on the rotating member 3 in a vertical state, and the second state is a vertical state. When the radar apparatus 2 changes from the second state to the first state, the process is reverse to the above-described radar apparatus 2 changing process. If the rotating portion 221 is released from the mating relationship with the second recess 32, then rotates relative to the first recess 31, so that the rotating portion 221 is located in the first recess 31 until the radar apparatus 2 is in the first state.

Through the rotation part 221 in the rotating piece 22 relatively to the first concave part 31, then the rotation part 221 is inserted into the second concave part 32, namely, the radar equipment 2 relatively rotates the piece 3 through rotation and insertion, the different angle adjustment of the radar equipment 2 is realized, the structure is simple, and no external tool such as a camera shooting assembly is needed.

The rotation of the rotating portion 221 relative to the first concave portion 31 may be performed in various manners, such as circular arc or arc rotation, and the like, so that the rotation of the rotating portion relative to the first concave portion 31 may be performed. In addition, the specific configuration of the rotation portion 221 that is inserted into the second recess portion 32 may be such that the radar apparatus 2 may be changed from the first state to the second state.

Referring to fig. 4, 5 and 6, fig. 4 is a first partial schematic view of an embodiment of the radar mounting assembly of the present application; FIG. 5 is a partial side schematic view of a radar apparatus in the radar mounting assembly of the present application; fig. 6 is a partial front schematic view of a radar apparatus of the radar mounting assembly of the present application. Referring to fig. 1 to 3, in particular, the rotating portion 221 includes two first circular arc surfaces 2221 disposed opposite to each other. The two first circular arc surfaces 2221 are disposed coaxially with the first concave portion 31, so that the rotating portion 221 rotates relative to the first concave portion 31 through the first circular arc surfaces 2221. The rotation part 221 includes two first side walls 2222 disposed opposite to each other. The distance X1 between the two ends of the first arc surface 2221 is smaller than or equal to the distance X2 between the two sidewalls of the second recess 32, and the first sidewall 2222 is matched with the sidewall of the second recess 32. Through the above arrangement, in the rotation process of the rotating portion 221 of the radar device 2, the first arc surface 2221 can be inserted into the second recess 32, so that the situation that the distance between two ends of the first arc surface 2221 is too large to enter the second recess 32 is avoided, and meanwhile, the situation that the first side wall 2222 is not matched with the side wall of the second recess 32, so that the interference rotating portion 221 is inserted into the second recess 32 is avoided, and the angle of the radar device 2 is convenient to quickly adjust.

Further, two second arc surfaces 311 are disposed on two sidewalls of the first recess 31. The two second arc surfaces 311 and the two first arc surfaces 2221 are coaxially disposed, so that the second arc surfaces 311 rotate relative to the first arc surfaces 2221, and the rotating portion 221 rotates relative to the first recess portion 31. The second recess 32 includes a second sidewall 321 disposed opposite thereto. The second side wall 321 is matched with the first side wall 2222, so that the first side wall 2222 of the rotating part 221 is inserted into the second concave part 32, and the phenomenon that the rotating part 221 cannot enter the second concave part 32 due to the fact that the first side wall 2222 is not matched with the second side wall 321 is avoided, so that the rapid angle adjustment of the radar device 2 is facilitated. In addition, the second arc surface 311 and the second sidewall 321 are connected, so that the rotation part 221 is convenient to transition from the first state to the second state, and interference problems are reduced.

Further, the first sidewall 2222 is planar. The second sidewall 321 is planar. The first side wall 2222 and the second side wall 321 are arranged in parallel, so that the insertion interference of the second concave part 32 to the rotating part 221 is reduced, and the rapid angle adjustment of the radar device 2 is further improved. In practice, to further promote the stability of the rotating member 22 in the second state, the first sidewall 2222 and the second sidewall 321 are disposed in close proximity.

Referring to fig. 7, 8 and 9, fig. 7 is a schematic partial cross-sectional view of an embodiment of a radar mounting assembly of the present application; FIG. 8 is a schematic view of the structure of FIG. 7A; fig. 9 is a schematic perspective view of a positioning member in the radar mounting assembly of the present application. Referring to fig. 1-6, in one embodiment, the radar mounting assembly 10 further includes two positioning members 4. Two positioning members 4 are located in the first housing 1. The positioning piece 4 is releasably and elastically clamped in the rotating piece 3 and the first shell 1. In this way, the rotation member 22 can be restricted from moving up and down in the vertical state, and further the radar apparatus 2 is prevented from moving up and down in the vertical state, and the stability of the radar apparatus 2 in the vertical state is improved.

When the radar apparatus 2 is in the first state, the rotating portion 221 has no related connection relation with the positioning member 4. When the radar apparatus 2 changes from the first state to the second state, the first circular arc surface 2221 in the rotating portion 221 presses the positioning member 4, and the positioning member 4 is compressed and sprung out by force. When the radar apparatus 2 is in the second state, the positioning member 4 is stressed to restore to the original state, and the positioning member 4 is elastically clamped on the rotating portion 221, so as to limit the radar apparatus 2 to move up and down in the vertical state.

Specifically, an end surface of the rotating portion 221 facing away from the rotating member 22 is provided with a connection surface 2223. The connection surface 2223 is connected to the two first circular arc surfaces 2221 and the two first side walls 2222, respectively. The connection surface 2223 is concavely provided with a connection groove 2224. The positioning member 4 includes a positioning body 41 and a first positioning pin 411. The first positioning pin 411 is fixed or integrally formed to the positioning body 41. The first positioning pin 411 is releasably elastically engaged in the connection groove 2224. By the above-described first positioning pin 411 and the connection groove 2224 being engaged with each other, the radar apparatus 2 can be quickly defined to move up and down in the vertical state, and the structure is simple and easy to implement.

When the radar apparatus 2 is in the first state to the second state, the first circular arc surface 2221 presses the first positioning pin 411, and the first positioning pin 411 is forced to spring, and at this time, the first positioning pin 411 is not elastically clamped in the connection groove 2224. When the first arc surface 2221 continues to rotate, the first positioning pin 411 and the connection groove 2224 are clamped as the first positioning pin 411 is restored and clamped in the connection groove 2224 at the same time, so that the first positioning pin 411 and the connection groove 2224 are clamped.

Further, an end face of the first positioning pin 411 facing away from the positioning body 41 is provided with a guide slope 4111. The distance between the guide slope 4111 and the positioning body 41 gradually increases in the direction from the first concave portion 31 to the second concave portion 32. The guide slope 4111 can function as a guide. When the rotating portion 221 falls into the second recess 32, the rotating portion 221 pushes the positioning member 4 through the guiding inclined surface 4111, and then the first positioning pin 411 is snapped into the connection groove 2224.

In one embodiment, the rotating member 3 is provided with a positioning hole 33. The positioning member 4 includes a positioning body 41 and a second positioning pin 412. The second positioning pin 412 is fixed or integrally formed to the positioning body 41. The second positioning pin 412 is releasably and elastically clamped in the positioning hole 33. The second positioning pin 412 may be elastically locked to the positioning hole 33, or may be disengaged from the positioning hole 33. The positioning hole 33 is matched with the second positioning pin 412 to limit the rotating member 3, so that the left and right shaking of the radar apparatus 2 in a horizontal state or a vertical state is reduced.

The positioning holes 33 may be one, two, three, or more than four. If the positioning hole 33 is one, the second positioning pin 412 is clamped in the positioning hole 33. When the number of the positioning holes 33 is more than two, the transverse cross section of the rotating member 3 is circular, and at least two positioning holes 33 are circumferentially arranged on the rotating member 3. When the rotating member 3 rotates, the second positioning pin 412 is clamped to the different positioning hole 33. The second positioning pins 412 are connected with different positioning holes 33, so that the radar device 2 can shake left and right in a horizontal state or a vertical state, and the stability of the radar device 2 is improved. As in the present embodiment, the number of the positioning holes 33 on both sides of the rotating member 3 is three.

Specifically, the second recess 32 is provided with a relief groove 34 therein. The avoidance groove 34 is used for avoiding the second positioning pin 412, so that interference on the second positioning pin 412 is reduced, and the angle adjustment of the radar device 2 is facilitated. The extending width of the avoidance groove 34 is determined by the distributing width of all the positioning holes 33, for example, the extending width of the avoidance groove 34 is greater than or equal to the distributing width of all the positioning holes 33 in at least two positioning holes 33. In this embodiment, the number of the positioning holes 33 is three, and the extending width of the avoiding groove 34 is equal to the distribution width of the three positioning holes 33.

In one embodiment, the radar mounting assembly 10 further comprises two elastic members 5. The elastic member 5 has a certain elastic force. The elastic member 5 may be, but is not limited to, a spring. The positioning member 4 includes a positioning body 41 and a third positioning pin 413. The third positioning pin 413 is disposed on a side surface of the positioning body 41 facing away from the rotating member 3. The first positioning pin 411 and the second positioning pin 412 are disposed on a side surface of the positioning body 41 near the rotating member 3. Namely, the first positioning pin 411 and the second positioning pin 412 are arranged on two sides of the positioning body 41 opposite to the third positioning pin 413. The third positioning pin 413 is fixed or integrally formed to the positioning body 41.

One end of the elastic member 5 is connected to the first housing 1, and the other end of the elastic member 5 is connected to the positioning body 41 and sleeved on the third positioning pin 413. For example, one end of an elastic member 5 is connected to the first housing 1, and the other end of the elastic member 5 is connected to the positioning body 41 and sleeved on the third positioning pin 413. One end of the other elastic member 5 is connected to the first housing 1, and the other end of the other elastic member 5 is connected to the other positioning body 41 and sleeved on the third positioning pin 413. By fitting the other end of the elastic member 5 over the third positioning pin 413, the compression and expansion directions of the elastic member 5 can be ensured. In addition, by providing two elastic members 5 between the positioning member 4 and the first housing 1, the first positioning pin 411 can be releasably elastically engaged in the connection groove 2224, and the second positioning pin 412 can be releasably elastically engaged in the positioning hole 33.

In order to further ensure the compression and expansion directions of the elastic member 5 in the actual process, the positioning body 41 is provided with a mounting groove 415, and the third positioning pin 413 is located in the mounting groove 415 and protrudes out of the outer surface of the positioning body 41. The other end of the elastic piece 5 is embedded in the mounting groove 415 and sleeved on the third positioning pin 413.

In an embodiment, the first housing 1 comprises a first sub-housing 11 and a second sub-housing 12. The first sub-housing 11 is detachably connected to the second sub-housing 12. The rotating member 3, the two positioning members 4 and the two elastic members 5 are located in the first sub-housing 11 and the second sub-housing 12. The second sub-housing 12 is provided with two moving grooves 121. The end of the positioning member 4 facing away from the first sub-housing 11 is provided with a tap lever 414. The toggle rod 414 penetrates through the moving groove 121 and protrudes out of the surface of the second sub-housing 12, which faces away from the first sub-housing 11. The movement slots 121 provide a path of movement for movement of the tap lever 414.

The toggle rod 414 can control the first positioning pin 411 in the positioning piece 4 to be in elastic clamping connection with the connecting groove 2224, and simultaneously, the second positioning pin 412 is in elastic clamping connection with the positioning hole 33, so that the radar device 2 can be changed from the second state to the first state, and at the moment, the second positioning pin 412 can be in elastic clamping connection with the positioning hole 33. In addition, the toggle rod 414 can control the second positioning pin 412 to be in elastic clamping connection with the positioning hole 33, and then control the radar device 2 and the rotating piece 3 to rotate, so that the second positioning pin 412 can be clamped in other positioning holes 33, and the radar device 2 can be adjusted in different left and right angle ranges in a horizontal state or a vertical state.

Referring to fig. 10, fig. 10 is a schematic structural view of a first sub-housing in the radar mounting assembly of the present application. Referring to fig. 1 to 9, in an embodiment, the first sub-housing 11 is concavely provided with a third concave portion 111. The third recess 111 is used for installing the second sub-housing 12, so that the second sub-housing 12 is detachably disposed in the third recess 111. In addition, the rotation member 3 and the two positioning members 4 can be defined during the mounting of the second sub-housing 12 to the first sub-housing 11. The groove bottom of the third recess 111 is concavely provided with a fourth recess 112 and two fifth recesses 113. The fourth recess 112 communicates with two fifth recesses 113. Two fifth concave portions 113 are located on both sides of the fourth concave portion 112. The fourth recess 112 is used for installing the rotating member 3, and the rotating member 3 is disposed in the fourth recess 112. The fourth recess 112 is cylindrical in shape due to the circular cross-section of the rotating member 3.

The fifth recess 113 is used for mounting the positioning member 4. The positioning members 4 are disposed in the corresponding fifth concave portions 113. The fifth recess 113 provides a mounting path and a moving path for the positioning member 4 and the elastic member 5. Such as a positioning member 4 and an elastic member 5, is disposed in a fifth recess 113. The other positioning element 4 and the other elastic element 5 are positioned in the other fifth concave portion 113.

The radar mounting assembly 10 is specifically tuned as follows. When the radar apparatus 2 needs to be turned from the first state to the second state, the first circular arc surface 2221 on the rotating member 22 in the radar apparatus 2 rotates around the second circular arc surface 311 on the first concave portion 31 in the rotating member 3. Since the rotating member 22 is further provided with the first sidewall 2222, the combined gravity force may transition from the first circular arc surface 2221 contact to the first sidewall 2222 contact during the rotation of the rotating member 22. During the process of changing the radar apparatus 2 from the first state to the second state, the first circular arc surface 2221 contacts the first positioning pin 411 of the positioning member 4, and pushes the toggle rod 414 in the positioning member 4 to move to the left and right sides along the moving slot 121 of the second sub-housing 12. When the radar apparatus 2 falls to a certain position, the first positioning pin 411 will rebound under the compression force of the elastic member 5, and at this time, the first positioning pin 411 on the positioning member 4 is inserted into the connection groove 2224 on the rotating member 22, so as to ensure that the radar apparatus 2 cannot move up and down. Meanwhile, the groove bottom of the connection groove 2224 of the radar device 2 and the end face of the first positioning pin 411 on the positioning member 4 are coaxially disposed for cooperation with subsequent rotation adjustment.

When the radar apparatus 2 needs to rotate left and right in a horizontal state or a vertical state, the two toggle rods 414 are moved along the left side and the right side of the moving groove 121 of the second sub-housing 12, the positioning member 4 is separated from the positioning hole 33, and at this time, the radar apparatus 2 is adjusted to rotate horizontally, and the radar apparatus 2 drives the rotating member 3 to rotate. When the plurality of positioning holes 33 on the rotating member 3 are matched with the second positioning pins 412 on the positioning member 4, the positioning member 4 can be inserted into the positioning holes 33 under the action of the compression force of the elastic member 5, so that the radar device 2 can horizontally rotate and be positioned and adjusted.

In contrast to the prior art, the radar mounting assembly includes a first housing, a rotating member, and a radar apparatus. The rotating piece is arranged in the first shell. The rotating piece is provided with a first concave part and a second concave part communicated with the first concave part. The radar apparatus includes a second housing and a rotating member provided to the second housing. The second housing is located outside the first housing. The rotating piece penetrates through the first shell and is positioned in the first concave part. The rotating parts are arranged at the two ends of the rotating piece. The radar equipment changes from a first state to a second state, the rotating part can rotate in the first concave part, and then the rotating part can be inserted in the second concave part. The rotating part rotates relative to the first concave part in the rotating part, and then the rotating part is inserted into the second concave part. Namely, the radar equipment is adjusted at different angles by rotating and inserting the rotating piece relatively, so that the structure is simple, and no external tool is needed.

Referring to fig. 11 and 12, fig. 11 is a schematic structural view of a radar mounting assembly in a first state in the monitoring device of the present application; fig. 12 is a schematic view of the structure of the radar mounting assembly in the second state in the monitoring device of the present application. In connection with fig. 1, a monitoring device 100 is provided. The monitoring device 100 includes a camera assembly 20 and a radar mounting assembly 10. The camera assembly 20 is used for monitoring, camera shooting and other functions. The specific configuration of camera assembly 20 is a matter of routine choice for those skilled in the art and is not limited herein. The radar apparatus 2 in the radar mounting assembly 10 is capable of acquiring parameters such as the speed and distance of a moving object. The monitoring device 100 is mutually matched with the camera assembly 20 and the radar installation assembly 10, so that the use requirement is improved. When the monitoring apparatus 100 is used for road conditions, it is possible to accommodate more complicated and varied road conditions, etc.

Specifically, the radar mounting assembly 10 is mounted to the camera assembly 20 through its first housing 1. This radar mounting assembly 10 is the radar mounting assembly 10 set forth in the above embodiments. The first housing 1 may be detachably or fixedly attached to the image pickup assembly 20. As in the present embodiment, the first housing 1 in the radar mounting assembly 10 is fixed to the outer surface of the camera assembly 20 by screws or the like.

When the radar mounting assembly 10 is mounted on the camera assembly 20, the radar mounting assembly 10 can be independently adjusted relative to the camera assembly 20 to achieve a rapid change in the radar apparatus 2 from the first state to the second state. When the radar apparatus 2 is in the first state, the radar mounting assembly 10 is in a parallel state with the camera assembly 20 as a whole, and the radar mounting assembly 10 is in a housed state, and the entire structure of the monitoring device 100 is compact. When the radar apparatus 2 is in the second state, the radar apparatus 2 is in a vertical state with the image pickup assembly 20. In addition, when the radar mounting assembly 10 is in either the first state or the second state, the radar apparatus 2 can be rotated as the rotating member 3 is rotated, and thus the rotation angle range of the radar apparatus 2 can be adjusted. Therefore, by the above-mentioned camera assembly 20 and radar installation assembly 10 cooperating with each other, the radar device 2 in the monitoring device 100 can be adjusted along with the angle linkage of the camera assembly 20, and the radar device 2 and the camera assembly 20 can be independently adjusted, so that the use function requirement of the monitoring device 100 is increased.

The terms "first," "second," "third," and the like in this application are used for descriptive purposes only and are not to be construed as indicating the number of features indicated. Thus, a feature defining "a first", "a second", and "a third" may explicitly or implicitly include at least one such feature. All directional indications (such as up, down, left, right, front, back … …) in the embodiments of the present application are merely used to explain the relative positional relationship, movement, etc. between the components in a particular gesture (as shown in the drawings), and if the particular gesture changes, the directional indication changes accordingly. Furthermore, the terms "comprise" and "have," as well as any variations thereof, are intended to cover a non-exclusive inclusion. A process, method, system, article, or apparatus that comprises a list of steps or elements is not limited to only those listed but may alternatively include other steps or elements not listed or inherent to such process, method, article, or apparatus.

The foregoing description is only exemplary embodiments of the present application and is not intended to limit the scope of the present application, and all equivalent structures or equivalent processes using the descriptions and the drawings of the present application, or direct or indirect application in other related technical fields are included in the scope of the present application.

Claims (12)

1. A radar mounting assembly, comprising:

a first housing;

the rotating piece is arranged in the first shell and is provided with a first concave part and a second concave part communicated with the first concave part;

the radar equipment comprises a second shell and a rotating piece arranged on the second shell, wherein the second shell is positioned outside the first shell, the rotating piece penetrates through the first shell and is positioned in the first concave part, rotating parts are arranged at two ends of the rotating piece and can rotate in the first concave part, and the rotating parts can be inserted into the second concave part.

2. The radar mounting assembly of claim 1, wherein the rotating portion includes two first arc surfaces disposed opposite to each other and two first side walls disposed opposite to each other, the two first arc surfaces and the first recess are disposed coaxially, a distance between two ends of the first arc surfaces is smaller than or equal to a distance between two side walls of the second recess, and the first side walls are matched with the side walls of the second recess.

3. The radar mounting assembly of claim 2, wherein two sidewalls of the first recess are provided with two second arc surfaces, the two second arc surfaces are coaxially disposed with the two first arc surfaces, the second recess includes oppositely disposed second sidewalls, the second sidewalls are matched with the first sidewalls, and one end of the second arc surface is connected with one end of the second sidewall.

4. A radar mounting assembly according to claim 3 wherein the first side wall is planar and the second side wall is planar, the first and second side walls being arranged in parallel.

5. The radar mounting assembly of claim 1, further comprising two positioning members located within the first housing, the positioning members being releasably resiliently snap-fitted within the rotating member and the first housing.

6. The radar mounting assembly of claim 5, wherein an end face of the rotating portion facing away from the rotating member is provided with a connection face, the connection face being concavely provided with a connection groove;

the locating piece comprises a locating body and a first locating pin arranged on the locating body, and the first locating pin is detachably and elastically clamped in the connecting groove.

7. The radar mounting assembly of claim 5, wherein a side of the rotating member adjacent the positioning member is provided with a positioning hole;

the locating piece comprises a locating body and a second locating pin arranged on the locating body, and the second locating pin is detachably and elastically clamped in the locating hole.

8. The radar mounting assembly of claim 7, wherein the rotor is circular in transverse cross-section, the locating holes include at least two, and at least two of the locating holes are circumferentially disposed in the rotor; when the rotating piece rotates, the second locating pin can be clamped in different locating holes.

9. The radar mounting assembly of claim 5, further comprising two elastic members, wherein the positioning member comprises a positioning body and a third positioning pin, the third positioning pin is disposed on a side surface of the positioning body facing away from the rotating member, one end of the elastic member is connected to the first housing, and the other end of the elastic member is connected to the positioning body and sleeved on the third positioning pin.

10. The radar mounting assembly of claim 5, wherein the first housing comprises a first sub-housing and a second sub-housing detachably connected to the first sub-housing, the second sub-housing is provided with a moving slot, one end of the positioning member facing away from the first sub-housing is provided with a toggle rod, and the toggle rod penetrates the moving slot and protrudes from a surface of the second sub-housing facing away from the first sub-housing.

11. The radar mounting assembly of claim 10, wherein the first sub-housing is provided with a third recess, the second sub-housing is detachably disposed in the third recess, a bottom recess of the third recess is provided with a fourth recess and two fifth recesses communicated with the fourth recess, the two fifth recesses are disposed at two ends of the fourth recess, the rotating member is disposed in the fourth recess, and the positioning member is disposed in the corresponding fifth recess.

12. A monitoring device, comprising:

a camera assembly;

the radar mounting assembly of any one of claims 1-11, a first housing in the radar mounting assembly mounted to the camera assembly.

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