CN215042437U

CN215042437U - Traffic fault flight cone

Info

Publication number: CN215042437U
Application number: CN202120604009.9U
Authority: CN
Inventors: 王金水; 张银合
Original assignee: Individual
Current assignee: Individual
Priority date: 2021-03-24
Filing date: 2021-03-24
Publication date: 2021-12-07
Anticipated expiration: 2031-03-24

Abstract

The utility model discloses a traffic trouble flight awl section of thick bamboo, including the awl barrel, be provided with a plurality of flight arm mechanisms on the outer wall of awl barrel to be provided with control mechanism in the awl barrel, control mechanism is connected with a plurality of flight arm mechanism electricity, control mechanism and control terminal wireless connection. The user can also use the control terminal to control the control mechanism in the cone cylinder; the traffic fault flight cone barrel lands at about 150m behind the automobile, so that traffic fault reminding is provided for a user and a rear vehicle, and a traffic accident caused by the fact that the rear vehicle collides with the user or the fault automobile is avoided; after the traffic fault is relieved, the user can use the control terminal to start the traffic fault flight cone cylinder to fly back so as to facilitate the user to take back the traffic fault flight cone cylinder, thereby effectively eliminating the defects that the traditional traffic fault cone cylinder is time-consuming and labor-consuming in placement, falls down, slides to, is turned on a vehicle, and the like.

Description

Traffic fault flight cone

Technical Field

The utility model relates to a traffic signal technical field, more specifically say, the utility model relates to a traffic trouble flight awl section of thick bamboo.

Background

The traditional cone cylinder for the fortune passing fault usually needs to be manually placed about 50m away from the rear of an accident vehicle, is time-consuming and labor-consuming, has the problems that people fall down, slip down, encounter traffic accidents and the like during the placement process, has low visibility in severe weather, and cannot play a role in warning a complex environment due to passive light reflection of the traditional cone cylinder in a complex road section. Therefore, there is a need for a traffic jam drogue to at least partially solve the problems of the prior art.

SUMMERY OF THE UTILITY MODEL

In the summary section a series of concepts in a simplified form is introduced, which will be described in further detail in the detailed description section. The inventive content does not imply any attempt to define the essential features and essential features of the claimed solution, nor is it implied to be intended to define the scope of the claimed solution.

For at least partly solving above-mentioned problem, the utility model provides a traffic trouble flight awl section of thick bamboo, include: the outer wall of the conical barrel body is provided with a plurality of flying arm mechanisms, a control mechanism is arranged in the conical barrel body, the control mechanism is electrically connected with the plurality of flying arm mechanisms, and the control mechanism is wirelessly connected with a control terminal.

Preferably, in the traffic fault flight cone cylinder, the flight arm mechanism comprises a supporting rod, a motor and fins, one end of the supporting rod is connected with the outer wall of the cone cylinder, the motor is arranged at the other end of the supporting rod, a plurality of fins are arranged on an output shaft of the motor, and the plurality of motors are electrically connected with the control mechanism.

Preferably, the traffic trouble flight awl section of thick bamboo in, flight arm mechanism still includes folding mechanism, folding mechanism includes auxiliary rod, first solid fixed ring, the solid fixed ring of second and hasp portion, the one end of auxiliary rod with the outer wall connection of awl barrel, first solid fixed ring sets up on the other end of auxiliary rod is served, the bottom of first solid fixed ring one end face with the solid fixed ring's of second terminal surface bottom rotates to be connected, first solid fixed ring's top with the top of the solid fixed ring's of second top one end face is passed through hasp portion is connected, the solid fixed ring of second sets up on one end of branch.

Preferably, in the traffic fault flight cone, the locking part includes a hook member and a clamping seat, the hook member is disposed at one end of the first fixing ring, the clamping seat is disposed at one end of the second fixing ring, and the hook member is matched with the clamping seat.

Preferably, in the traffic fault flight cone, the flight arm further includes a rectifying cap and an anti-collision ring, the anti-collision ring is disposed on the strut and is sleeved outside the plurality of fins, and the rectifying cap is disposed at an end of the motor output shaft.

Preferably, in the traffic fault flight cone, the flight arm mechanism further comprises a wide-angle lens, the wide-angle lens is arranged on the outer wall of the anti-collision ring, and the wide-angle lens is electrically connected with the control mechanism.

Preferably, in the traffic fault flight cone, the outer wall of the cone body is provided with a plurality of reflective belts, and the lower end of the cone body is provided with anti-skid rubber.

Preferably, in the traffic fault flight cone, a transparent cover is arranged at the upper end of the cone body, an LED lamp bank is arranged at a position close to the transparent cover in the cone body, and the LED lamp bank is electrically connected with the control mechanism.

Preferably, in the traffic fault flight cone, the control mechanism includes a power supply mechanism, a flight controller and an antenna module, the controller is arranged in the cone, the flight controller is arranged in the cone, the power supply mechanism includes a power supply box and a lithium battery arranged in the power supply box, the power supply box is arranged below the flight controller, and the antenna module is arranged above the flight controller.

Compared with the prior art, the utility model discloses at least, including following beneficial effect:

the utility model provides a traffic fault flight cone, which comprises a cone body, wherein the outer wall of the cone body is provided with a plurality of flight arm mechanisms, and a control mechanism is arranged in the cone body and is used for controlling and starting the plurality of flight arm mechanisms; the traffic fault flight cone barrel lands at about 150m behind the automobile, so that traffic fault reminding is provided for a user and a rear vehicle, and a traffic accident caused by the fact that the rear vehicle collides with the user or the fault automobile is avoided; after the traffic fault is relieved, the user can use the control terminal to start the traffic fault flight cone cylinder to fly back so as to facilitate the user to take back the traffic fault flight cone cylinder, thereby effectively eliminating the defects that the traditional traffic fault cone cylinder is time-consuming and labor-consuming in placement, falls down, slides to, is turned on a vehicle, and the like.

Traffic trouble flight cone, other advantages, objects and features of the invention will be in part apparent from the following description, and in part will be understood by those skilled in the art through a study and practice of the invention.

Drawings

The accompanying drawings are included to provide a further understanding of the invention, and are incorporated in and constitute a part of this specification, illustrate embodiments of the invention, and together with the description serve to explain the invention and not to limit the invention. In the drawings:

fig. 1 is a front view of the structure of the present invention.

Fig. 2 is a front view of the internal structure of the present invention.

Fig. 3 is a schematic structural diagram of the middle folding mechanism of the present invention.

Fig. 4 is an enlarged schematic structural diagram of a point a in fig. 3 according to the present invention.

Fig. 5 is a schematic structural view of the middle flying arm mechanism of the present invention when folded.

Fig. 6 is an enlarged schematic structural diagram of the present invention at B in fig. 5.

Fig. 7 is a top view of the structure of the present invention.

Detailed Description

The present invention is further described in detail below with reference to the drawings and examples so that those skilled in the art can implement the invention with reference to the description.

It will be understood that terms such as "having," "including," and "comprising," as used herein, do not preclude the presence or addition of one or more other elements or groups thereof.

As shown in fig. 1-2, the utility model provides a traffic fault flight cone, include: the flight control device comprises a cone body 1, wherein a plurality of flight arm mechanisms 2 are arranged on the outer wall of the cone body 1, a control mechanism 3 is arranged in the cone body 1, the control mechanism 3 is electrically connected with the flight arm mechanisms 2, and the control mechanism 3 is in wireless connection with a control terminal.

The working principle and the beneficial effects of the technical scheme are as follows: the utility model provides a traffic fault flight cone, this traffic fault flight cone includes cone 1, specifically speaking, be provided with a plurality of flight arm mechanisms 2 on the outer wall of this cone 1, installed control mechanism 3 in this cone 1 simultaneously, control mechanism 3 is used for with control, start a plurality of flight arm mechanisms 2, simultaneously, the user can also use control terminal (not shown), like the remote controller, or, the smart mobile phone starts and controls control mechanism 3 in cone 1; generally speaking, the utility model discloses a traffic trouble flight awl section of thick bamboo is placed in the trunk of car, when taking place traffic trouble, the user opens the trunk after getting off and takes out this traffic trouble flight awl section of thick bamboo, place traffic trouble flight awl section of thick bamboo subaerial, after reserving its space of taking off, can use smart mobile phone (having installed APP in the smart mobile phone) to start to have installed control mechanism 3 in the awl section of thick bamboo 1, and then control mechanism 3 starts a plurality of flight arm mechanism 2 on the awl section of thick bamboo 1, flight arm mechanism 2 and then drive this awl section of thick bamboo 1, the user reuses smart mobile phone and controls traffic trouble flight awl section of thick bamboo to descend about 150m behind the car, provide traffic trouble warning for user and rear vehicle, avoid rear vehicle to strike user or trouble car and take place the car accident; after the traffic fault is relieved, the user can use the control terminal to start the traffic fault flight cone cylinder to fly back so as to facilitate the user to take back the traffic fault flight cone cylinder, thereby effectively eliminating the defects that the traditional traffic fault cone cylinder is time-consuming and labor-consuming in placement, falls down, slides to, is turned on a vehicle, and the like.

It should be noted that the control operation principle between the control terminal and the control mechanism is well known to those skilled in the art, and the detailed structural principle is not described again.

In one embodiment, the flying arm mechanism 2 includes a supporting rod 21, a motor 22 and a wing 23, one end of the supporting rod 21 is connected to the outer wall of the conical cylinder 1, the motor 22 is disposed at the other end of the supporting rod 21, a plurality of the wings 23 are disposed on an output shaft of the motor 22, and the plurality of the motors 22 are electrically connected to the control mechanism 3.

The working principle and the beneficial effects of the technical scheme are as follows: the structure of flight arm mechanism 2 is provided in this embodiment, flight arm mechanism 2 of this structure includes branch 21, motor 22 and fin 23, particularly, the one end of branch 21 is installed on the outer wall of awl barrel 1, motor 22 is being installed at the other end of branch 21, then a plurality of fins 23 are being installed on the output shaft of motor 22, when control mechanism 3 starts motor 22, motor 22's output shaft 23 rotates, and then a plurality of fins 23 rotate, make flight arm mechanism 2 drive awl barrel 1 and fly, replace the user and place the car rear with awl barrel 1, convenience of customers uses.

As shown in fig. 3 to 6, in one embodiment, the flying arm mechanism 2 further includes a folding mechanism 24, the folding mechanism 24 includes an auxiliary rod 241, a first fixing ring 242, a second fixing ring 243, and a locking portion 244, one end of the auxiliary rod 241 is connected to the outer wall of the cone body, the first fixing ring 242 is disposed at the other end of the auxiliary rod 241, the bottom of one end face of the first fixing ring 242 is rotatably connected to the bottom of one end face of the second fixing ring 243, the top of the first fixing ring 242 is connected to the top of one end face of the top of the second fixing ring 243 through the locking portion 244, and the second fixing ring 243 is disposed at one end of the strut 21.

The working principle and the beneficial effects of the technical scheme are as follows: in the embodiment, the flying arm mechanism 2 further includes a flying arm mechanism 24, the flying arm mechanism 24 includes an auxiliary rod 241, a first fixing ring 242, a second fixing ring 243, and a locking part 244, specifically, one end of the auxiliary rod 241 is mounted on the outer wall of the conical cylinder 1, the first fixing ring 242 is mounted at the other end of the auxiliary rod 241, the second fixing ring 243 is mounted at one end of the strut 21, and the bottoms of the first fixing ring 242 and the second fixing ring 243 adopt a movable connection manner, so that the second fixing ring 243 can rotate relative to the first fixing ring 242, and the movable connection may be a mechanism capable of rotating, such as a rotating screw, a folding rotating shaft, a pivoting, a hinge joint, and the like; meanwhile, the tops of the first fixing ring 242 and the second fixing ring 243 are connected by the locking portions 244, wherein, since the auxiliary rod 241 has a certain length, such as 10cm, an opening space is left for the locking portions 244; the strut 21 in the flying arm mechanism 2 can be folded to be close to the outer wall of the cone body 1 through the folding mechanism 24, so that the traffic fault flying cone has a compact structure and can be easily placed in a trunk of an automobile by a user, and the occupied space is avoided.

In one embodiment, the locking portion 244 includes a hooking member 245 and a catching seat 246, the hooking member 245 is disposed at one end of the first fixing ring 242, the catching seat 246 is disposed at one end of the second fixing ring 243, and the hooking member 245 is engaged with the catching seat 246.

The working principle and the beneficial effects of the technical scheme are as follows: the embodiment provides a structure of the locking part 244, and the locking part 244 of the structure comprises a latch member 245 and a latch seat 246, wherein the latch member 245 is installed on the first fixing ring 242, and the latch seat 246 is installed on the second fixing ring 243, however, here, the latch seat 246 is also installed on the first fixing ring 242, and the latch member 245 is installed on the second fixing ring 243, which can also realize the folding rotation of the flying arm mechanism 2; as shown in fig. 4, when the hooking part 245 of the locking part 244 and the hooking seat 246 are closed, the supporting rod 21 can be closely attached to the auxiliary rod 241; as shown in fig. 6, when the hooking member 245 of the locking portion 244 is separated from the hooking seat 246, the supporting rod 21 is coupled with the auxiliary rod 241 by a rotating screw. It is understood that the locking portion 244 may be other structures that enable the flying arm mechanism 2 to be folded and unfolded, and this embodiment is not limited thereto.

Further, as shown in fig. 5, a fixing block 15 is further disposed on the outer wall of the cone body 1, so that when the locking portion 244 is separated, the flying arm mechanism 2 can be folded downward to be close to the cone body 1, and a locking groove is formed in the fixing block 15, so as to fix the motor 22, so that the flying arm mechanism 2 and the cone body 1 are fixed to play a role in safety protection.

As shown in fig. 3, in one embodiment, the flying arm mechanism 2 further includes a fairing cap 25 and an impact ring 26, the impact ring 26 is disposed on the strut 21 and is sleeved outside the plurality of fins 23, and the fairing cap 25 is disposed at an end of the output shaft 221.

The working principle and the beneficial effects of the technical scheme are as follows: the flight arm mechanism 2 in this example further includes a fairing cap 25 and an anti-collision ring 26, specifically, the anti-collision ring 26 is mounted on the strut 21, and the anti-collision ring 26 is simultaneously sleeved outside the fins 23 to enclose the fins 23, so as to protect the fins 23, where of course, the anti-collision ring 26 may also be fixed with the motor 22 through other structures;

in order to reduce the resistance, a rectifying cap 25 is mounted at the end of the output shaft 221 of the motor 22, it can be understood that the top end of the rectifying cap 25 is arc-shaped, an internal threaded hole is formed inside the rectifying cap 25, and the end of the output shaft 221 is provided with an external thread, so that the two are screwed; wherein, the bottom projection area of fairing 25 is greater than the projection area of motor 22, perhaps, the bottom of fairing 25 can shelter from fin 23 and output shaft 221 coupling part to this plays better rectification effect, and simultaneously, fairing 25 has better pleasing to the eye effect, and at unmanned aerial vehicle flight in-process, can be used for adjusting the air current simultaneously, has the effect of reducing drag, and fairing 25 adopts aluminum alloy material to make, can be when proof strength, also guarantee that weight can not be too heavy.

As shown in fig. 7, in one embodiment, the flying arm mechanism 2 further includes a wide-angle lens 27, the wide-angle lens 27 is disposed on an outer wall of the impact ring 26, and the wide-angle lens 27 is electrically connected to the control mechanism 3.

The working principle and the beneficial effects of the technical scheme are as follows: flight arm mechanism 2 still includes wide-angle lens 27 in this embodiment, can install a plurality of wide-angle lenses 27 here on anticollision ring 26, and wide-angle lens 27 on the same direction can be shot other cars to control terminal to the user through control mechanism 3, send video image on the smart mobile phone promptly, with this vehicle that convenience of customers observed the rear, when this traffic trouble flight cone was collided to the rear vehicle, the user can in time know in order to avoid the rear vehicle to avoid the car accident.

In one embodiment, the outer wall of the conical cylinder body 1 is provided with a plurality of reflective belts 11, and the lower end is provided with anti-slip rubber 12.

The working principle and the beneficial effects of the technical scheme are as follows: in the embodiment, the outer wall of the conical cylinder body 1 is provided with a plurality of reflective belts 11, so that a vehicle behind can conveniently notice the conical cylinder body 1; the antiskid rubber 12 is arranged at the lower end of the cone body 1, so that the friction force between the whole traffic fault flight cone and the ground is increased, and the traffic fault flight cone is prevented from being blown by airflow generated by vehicles behind after falling on the ground.

As shown in fig. 2, in one embodiment, a transparent cover 13 is disposed at an upper end of the conical cylinder 1, and an LED lamp group 14 is disposed in the conical cylinder 1 near the transparent cover 13 and electrically connected to the control mechanism 3.

The working principle and the beneficial effects of the technical scheme are as follows: generally speaking, the upper end of the cone body 1 has no part for actively reminding a vehicle behind, and at night or when light is not good, the upper end of the cone body 1 alone cannot provide a sufficient reminding function by means of the reflective belt 11, so in the embodiment, the transparent cover 13 is arranged at the upper end of the cone body 1, and meanwhile, the LED lamp set 14 is arranged in the cone body 1 close to the transparent cover 13, and it can be understood that the LED lamp set 14 comprises a lamp holder 141 and an LED lamp module 142, the lamp holder 141 is fixedly arranged on the inner wall of the cone body 1, the LED lamp module 142 is arranged on the lamp holder 141, when the traffic fault flight cone falls to a position 150m behind, a user can use a control terminal to start the LED lamp module 142 through the control mechanism 3, and the LED lamp module 142 can emit flickering light, so as to better remind a vehicle behind.

As shown in fig. 2, in one embodiment, the control mechanism 3 includes a power supply mechanism 31, a flight controller 32, and an antenna module 33, the controller is disposed in the cone body 1, the flight controller 32 is disposed in the cone body 1, the power supply mechanism 31 includes a power supply box 311 and a lithium battery 312 disposed in the power supply box 311, the power supply box 311 is disposed below the flight controller 32, and the antenna module 33 is disposed above the flight controller 32.

The working principle and the beneficial effects of the technical scheme are as follows: the present embodiment provides a structure of a control mechanism 3, the structure control mechanism 3 includes a power supply mechanism 31, a flight controller 32 and an antenna module 33, specifically, the flight controller 32 is installed on the inner wall of the cone body 1, the power supply mechanism 31 is fixed at the bottom of the flight controller 32, specifically, the power supply mechanism 31 includes a power supply box 311 and a lithium battery 312, where the upper end of the power supply box 311 is fixed at the bottom of the flight controller 32, the lithium battery 312 is installed in the power supply box 311, and the lithium battery 312 supplies power to the flight controller 32; it can be understood that a certain distance, for example 10-20cm, is provided between the power box 311 and the lower end of the conical cylinder 1, so as to prevent the power box 311 from directly contacting the ground, and furthermore, the bottom of the power box 311 is provided with an openable door plate, so as to facilitate a user to take out the lithium battery 312 for charging;

the antenna module 33 is installed on the top of the flight controller 32, the flight controller 32 is wirelessly connected with the control terminal through the antenna module 33, and it can be understood that a 5G communication module is also installed in the flight controller 32 to be better in communication connection with the smart phone; the traffic fault flight cone is also provided with a GPS/Beidou single-mode positioning module or a dual-mode positioning module, so that the traffic fault flight cone can accurately fly to the position 150m behind the automobile; the flight controller 32 and the antenna module 33 are conventional components known to those skilled in the art, and the specific structural models thereof are not described again.

In the description of the present invention, it is to be understood that the terms "center", "longitudinal", "lateral", "length", "width", "thickness", "upper", "lower", "front", "rear", "left", "right", "vertical", "horizontal", "top", "bottom", "inner", "outer", "clockwise", "counterclockwise", "axial", "radial", "circumferential", and the like, indicate the orientation or positional relationship indicated based on the drawings, and are only for convenience of description and simplicity of description, and do not indicate or imply that the device or element referred to must have a particular orientation, be constructed and operated in a particular orientation, and therefore, should not be construed as limiting the present invention.

In the present invention, unless otherwise expressly stated or limited, the terms "mounted," "connected," and "fixed" are to be construed broadly and may, for example, be fixedly connected, detachably connected, or integrally formed; may be mechanically coupled, may be electrically coupled or may be in communication with each other; they may be directly connected or indirectly connected through intervening media, or they may be connected internally or in any other suitable relationship, unless expressly stated otherwise. The specific meaning of the above terms in the present invention can be understood according to specific situations by those skilled in the art.

While the embodiments of the invention have been disclosed above, it is not limited to the applications listed in the description and the embodiments, which are fully applicable in all kinds of fields of application suitable for this invention, and further modifications may be readily made by those skilled in the art, and the invention is therefore not limited to the specific details shown and described herein without departing from the general concept defined by the claims and their equivalents.

Claims

1. A traffic fault flight cone, comprising:

the aircraft flight control device comprises a cone barrel body (1), wherein a plurality of flight arm mechanisms (2) are arranged on the outer wall of the cone barrel body (1), a control mechanism (3) is arranged in the cone barrel body (1), the control mechanism (3) is electrically connected with the flight arm mechanisms (2), and the control mechanism (3) is in wireless connection with a control terminal.

2. The traffic-failure flight cone drum according to claim 1, characterized in that the flight arm mechanism (2) comprises a support rod (21), a motor (22) and a wing (23), one end of the support rod (21) is connected with the outer wall of the cone drum body (1), the motor (22) is arranged at the other end of the support rod (21), the output shaft of the motor (22) is provided with a plurality of the wings (23), and the plurality of the motors (22) are electrically connected with the control mechanism (3).

3. The traffic fault flight cone drum according to claim 2, wherein the flight arm mechanism (2) further comprises a folding mechanism (24), the folding mechanism (24) comprises an auxiliary rod (241), a first fixing ring (242), a second fixing ring (243) and a locking part (244), one end of the auxiliary rod (241) is connected with the outer wall of the cone drum body, the first fixing ring (242) is arranged at the other end of the auxiliary rod (241), the bottom of one end face of the first fixing ring (242) is rotatably connected with the bottom of one end face of the second fixing ring (243), the top of the first fixing ring (242) is connected with the top of one end face of the top of the second fixing ring (243) through the locking part (244), and the second fixing ring (243) is arranged at one end of the strut (21).

4. The traffic fault cone flight according to claim 3, characterized in that the locking portion (244) comprises a hooking element (245) and a catching seat (246), the hooking element (245) being arranged at one end of the first fixing ring (242), the catching seat (246) being arranged at one end of the second fixing ring (243), the hooking element (245) cooperating with the catching seat (246).

5. The traffic jam drogue cone of claim 2, characterized in that the flying arm mechanism (2) further comprises a fairing cap (25), an anti-collision ring (26), the anti-collision ring (26) being arranged on the strut (21) and being sleeved outside the plurality of fins (23), the fairing cap (25) being arranged at an end of an output shaft of the motor (22).

6. Traffic breakdown flight cone according to claim 5, characterized in that the flight arm mechanism (2) further comprises a wide-angle lens (27), the wide-angle lens (27) being arranged on the outer wall of the crash ring (26), the wide-angle lens (27) being electrically connected to the control mechanism (3).

7. The traffic fault flight cone drum according to claim 1, characterized in that a plurality of reflective strips (11) are arranged on the outer wall of the cone drum body (1), and an anti-skid rubber (12) is arranged at the lower end.

8. The traffic-failure flight cone drum according to claim 1, characterized in that a transparent cover (13) is arranged at the upper end of the cone drum body (1), an LED lamp group (14) is arranged in the cone drum body (1) close to the transparent cover (13), and the LED lamp group (14) is electrically connected with the control mechanism (3).

9. The traffic jam flight cone of claim 1, wherein the control mechanism (3) comprises a power supply mechanism (31), a flight controller (32) and an antenna module (33), the controller is disposed in the cone body (1), the flight controller (32) is disposed in the cone body (1), the power supply mechanism (31) comprises a power supply box (311) and a lithium battery (312) disposed in the power supply box (311), the power supply box (311) is disposed below the flight controller (32), and the antenna module (33) is disposed above the flight controller (32).