CN217784947U - Aviation obstruction beacon and safe obstacle avoidance device - Google Patents

Abstract

The utility model discloses an aviation obstruction light and a safe obstacle avoidance device, the aviation obstruction light comprises a light holder, a light source component, a light outlet cover, a camera component and a radar device, the light holder is suitable for being installed on an obstacle; the light source component is arranged in the lamp holder; the light-emitting cover is arranged at the top of the lamp holder, a seal is formed between the light-emitting cover and the lamp holder, and the top of the light-emitting cover is provided with an opening; the camera assembly comprises an installation frame and a camera, the lower end of the installation frame is positioned in the opening and is fixedly connected with the lamp holder, and the camera is fixed at the upper end of the installation frame and used for collecting near-empty video image data; the radar device is installed the upper end of mounting bracket for detect nearly empty aircraft. According to the utility model provides an aviation obstruction lamp and safe obstacle-avoiding device can accurately detect nearly empty aircraft, reaches more reliably stably the warning effect.

Description

Aviation obstruction light and safe obstacle avoidance device

Technical Field

The utility model relates to a lamps and lanterns especially relate to an aviation obstruction beacon and safe obstacle-avoiding device.

Background

Aviation Obstruction lights (also called navigation aid lighting devices) are special lamps for identifying obstacles, and belong to the navigation aid lighting device industry. The aviation obstruction light is used for displaying the outline of a structure, so that an aircraft operator can judge the height and the outline of the obstruction to play a role in warning.

In the related art, in order to play a better warning role, a radar module is configured on an aircraft obstruction light, the radar module is used for detecting whether an aircraft is near the air or not, and then the obstruction light is controlled according to a detection result to adjust different working modes, however, the radar detection mode is not accurate, and particularly after the aircraft is used for a certain period of time, faults are easy to occur or the detection is not reliable.

SUMMERY OF THE UTILITY MODEL

The present invention aims at solving one of the technical problems in the related art at least to a certain extent. Therefore, the utility model aims to provide an aviation obstruction beacon and safe barrier device of keeping away.

To achieve the above object, according to the utility model discloses an aviation obstruction light, include:

a lamp holder adapted to be mounted on an obstacle;

a light source assembly disposed within the lamp socket;

the light emitting cover is arranged at the top of the lamp holder and forms sealing with the lamp holder, and the top of the light emitting cover is provided with an opening;

the camera assembly comprises a mounting frame and a camera, the lower end of the mounting frame is positioned in the opening and is fixedly connected with the lamp holder, and the camera is fixed at the upper end of the mounting frame and is used for collecting near-space video image data;

and the radar device is arranged at the upper end of the mounting rack and used for detecting the near-air aircraft.

In addition, according to the utility model discloses aviation obstruction beacon of above-mentioned embodiment can also have following additional technical characterstic:

according to an embodiment of the present invention, the light source assembly comprises:

the outer wall of the reflecting cup is provided with a reflecting cambered surface protruding inwards;

the annular light source is coaxially arranged below the reflecting cup, the light emitting direction of the annular light source is upward, so that light rays are projected upward to the reflecting cambered surface and are emitted out from the circumferential direction of the light emitting cover after being reflected by the reflecting cambered surface.

According to an embodiment of the present invention, the lamp further comprises a bracket, the bracket comprises a bottom plate and a central cylinder, the bottom plate is fixed in the lamp holder, and the central cylinder is arranged in the center of the bottom plate and protrudes upwards;

the annular light source is arranged on the bottom plate and located outside the central cylinder, the light outlet cover is provided with an opening connected with the upper end of the central cylinder in a sealing manner, and the lower end of the mounting frame is connected with the upper end of the central cylinder in a sealing manner.

According to the utility model discloses an embodiment, center section of thick bamboo upper end has the flange seat, the mounting bracket includes bracing piece and ring flange, the ring flange is located the lower extreme of bracing piece and with ring flange fixed connection, camera and radar installation establish the upper end of bracing piece.

According to an embodiment of the invention, the opening has a sealing edge, which is press-sealed on the flange seat and around the outside of the flange.

According to an embodiment of the invention, the flange plate and the flange seat have a compressed gasket therebetween.

According to the utility model discloses an embodiment, the mounting bracket is still including carrying the pole, it connects to carry the pole the upper end of bracing piece and with the bracing piece is perpendicular, the camera is two, two the camera is installed respectively carry the both ends of pole, radar installations is established carry on the pole and be located two between the camera.

According to the utility model discloses an embodiment still includes wireless communication module, wireless communication module and controller, wireless communication module is used for communicating with remote monitoring equipment, be used for with video image data reaches radar data transmission that radar installations detected to remote monitoring equipment, and the control command that remote monitoring equipment sent, the controller with wireless communication module, camera, radar installations and light source subassembly are connected, are used for according to control command control the light source module changes mode.

On the other hand, according to the utility model discloses obstacle device is kept away to aviation obstruction beacon safety, include:

an aircraft obstruction light as described above;

and the remote monitoring equipment is in wireless communication connection with the aviation obstruction light, is used for outputting a control instruction according to the video image data and the radar data sent by the aviation obstruction light, and sends the control instruction to the aviation obstruction light.

According to the embodiment of the utility model provides an aviation obstruction lamp and safe obstacle-avoiding device, can gather nearly empty video image data through the camera on the aviation obstruction lamp, radar apparatus detects the radar signal of nearly empty, video image data and radar signal send to remote monitoring equipment, utilize remote monitoring equipment to carry out the image recognition after, confirm whether there is the aircraft near empty jointly with radar signal, so, can obtain more accurate testing result, switching mode according to testing result control obstruction lamp, and then can reach more reliably and stably warning effect. In addition, with camera and radar installations integration at above-mentioned aviation obstruction beacon, the structure is simpler, and the system is simplified, is convenient for arrange the implementation.

Additional aspects and advantages of the invention will be set forth in part in the description which follows and, in part, will be obvious from the description, or may be learned by practice of the invention.

Drawings

In order to more clearly illustrate the embodiments of the present invention or the technical solutions in the prior art, the drawings used in the embodiments or the prior art descriptions will be briefly described below, it is obvious that the drawings in the following description are only some embodiments of the present invention, and for those skilled in the art, other drawings can be obtained according to the structures shown in the drawings without creative efforts.

FIG. 1 is a schematic structural diagram of an aviation obstruction light according to an embodiment of the present invention;

fig. 2 is a sectional view of an aviation obstruction light according to an embodiment of the invention;

fig. 3 is an exploded view of an aircraft obstruction light according to an embodiment of the present invention;

fig. 4 is a specific exploded view of an aviation obstruction light according to an embodiment of the present invention.

Reference numerals are as follows:

10. a lamp socket;

11. a support;

111. a base plate;

112. a central barrel;

113. a flange seat;

20. a light source assembly;

201. a light reflecting cup;

s201, reflecting arc surfaces;

202. an annular light source;

202a, an annular substrate;

202b, an LED light source;

30. a light cover is discharged;

40. a camera assembly;

401. a mounting frame;

401a, a support rod;

401b, a flange plate;

401c, a carrier bar;

402. a camera;

50. provided is a radar device.

The realization, the functional characteristics and the advantages of the utility model are further explained by combining the embodiment and referring to the attached drawings.

Detailed Description

Reference will now be made in detail to embodiments of the present invention, examples of which are illustrated in the accompanying drawings, wherein like reference numerals refer to the same or similar elements or elements having the same or similar function throughout. The embodiments described below with reference to the drawings are exemplary and are intended to be used for explaining the present invention, but should not be construed as limiting the present invention, and all other embodiments obtained by those skilled in the art without making creative efforts based on the embodiments of the present invention belong to the protection scope of the present invention.

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", "circumferential", "radial", and the like, indicate the orientation or positional relationship indicated based on the orientation or positional relationship shown in 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.

Furthermore, the terms "first", "second" and "first" are used for descriptive purposes only and are not to be construed as indicating or implying relative importance or implicitly indicating the number of technical features indicated. Thus, a feature defined as "first" or "second" may explicitly or implicitly include one or more of that feature. In the description of the present invention, "a plurality" means two or more unless specifically limited otherwise.

In the present invention, unless otherwise expressly specified or limited, the terms "mounted," "connected," and "fixed" are to be construed broadly and may, for example, be fixedly connected, detachably connected, or integrally connected; can be mechanically or electrically connected; they may be connected directly or indirectly through intervening media, or they may be interconnected between two elements. The specific meaning of the above terms in the present invention can be understood according to specific situations by those skilled in the art.

In the present disclosure, unless expressly stated or limited otherwise, the first feature "on" or "under" the second feature may comprise direct contact between the first and second features, or may comprise contact between the first and second features not directly. Also, the first feature "on," "above" and "over" the second feature may include the first feature being directly above and obliquely above the second feature, or simply indicating that the first feature is at a higher level than the second feature. A first feature being "under," "below," and "beneath" a second feature includes the first feature being directly under and obliquely below the second feature, or simply meaning that the first feature is at a lesser elevation than the second feature.

The aviation obstruction light and the safety obstacle-avoiding device according to the embodiment of the present invention are described in detail with reference to the accompanying drawings.

Referring to fig. 1 to 4, an aviation obstruction light provided by the embodiment of the present invention includes a lamp holder 10, a light source assembly 20, a light-emitting cover 30, a camera assembly 40, and a radar device 50.

In particular, the lamp socket 10 is adapted to be mounted on an obstacle. The lamp socket 10 may be generally formed as a substantially cylindrical member, and the bottom of the lamp socket 10 is conveniently mounted on a barrier such as a building. A receiving space is formed in the lamp socket 10 to mount the light source assembly 20.

The light source assembly 20 is disposed in the lamp socket 10, and the light emitted by the light source assembly 20 during operation plays a role in warning, and the light source assembly 20 may have a plurality of different operation modes, such as flashing at a predetermined frequency, or keeping constant brightness, or alternatively flashing in different colors, etc.

The light outlet cover 30 is arranged on the top of the lamp holder 10 and forms a seal with the lamp holder 10, and the top of the light outlet cover 30 is provided with an opening.

The camera assembly 40 comprises a mounting frame 401 and a camera 402, the lower end of the mounting frame 401 is located in the opening and fixedly connected with the lamp holder 10, and the camera 402 is fixed at the upper end of the mounting frame 401 and used for collecting near-space video image data. The radar device 50 is installed at the upper end of the mounting frame 401 and used for detecting the near-air aircraft.

That is to say, the aviation obstruction light is provided with a camera 402 and a radar device 50, the camera 402 and the radar device 50 are installed at the top of the light through a mounting rack 401, near-empty video image data can be collected through the camera 402, and near-empty aircrafts can be detected through radar waves emitted by the radar device 50, and returned radar signals are received. Preferably, the camera 402 and the radar apparatus 50 may be arranged at an elevation angle, such as a 45 ° angle.

According to the utility model provides an aviation obstruction light can gather nearly empty video image data through camera 402 on the aviation obstruction light, radar installation 50 detects the radar signal of nearly empty, video image data and radar signal send to remote monitoring equipment, utilize remote monitoring equipment to carry out the image recognition after, confirm whether there is the aircraft near empty jointly with radar signal, so, can obtain more accurate testing result, switching mode according to testing result control obstruction light, and then can reach more reliably stably the warning effect. In addition, the camera 402 and the radar device 50 are integrated in the aviation obstruction light, so that the structure is simpler, the system is simplified, and the arrangement and implementation are convenient.

In some embodiments of the present invention, the light source assembly 20 includes a reflective cup 201 and an annular light source 202, the reflective cup 201 is formed into a horn-shaped structure with gradually decreasing diameter from top to bottom, the outer wall of the reflective cup 201 has a reflective arc surface S201 protruding towards the inner side.

The annular light source 202 is coaxially disposed below the reflective cup 201, and the light emitting direction is upward, so as to project light upward to the reflective arc surface S201, and emit light in the circumferential direction of the light emitting cover 30 after being reflected by the reflective arc surface S201. That is, the light emitted from the annular light source 202 may be projected upward to the outer surface of the reflector cup 201, and emitted in the circumferential direction by reflection to form an annular illumination light.

Illustratively, the annular light source 202 includes an annular substrate 202a and a plurality of LED light sources 202b spaced apart from the annular substrate 202a, the annular substrate 202a may be fixed in the lamp socket 10, for example, a step surface is provided in the lamp socket 10, and the annular substrate 202a is fixed on the step surface by a fastener.

In this embodiment, adopt above-mentioned light source subassembly 20 structure, utilize annular reflection arc to emit from the circumference of light-emitting cover 30 after the light that LED light source 202b jetted out emits, so, the ring illumination of formation can be observed from each different angles, plays better warning effect.

In an embodiment of the present invention, the lamp further includes a bracket 11, the bracket 11 includes a bottom plate 111 and a central tube 112, the bottom plate 111 is fixed in the lamp holder 10, and the central tube 112 is disposed in the center of the bottom plate 111 and protrudes upwards.

The annular light source 202 is arranged on the bottom plate 111, the annular light source 202 is located outside the central cylinder 112, the opening of the light outlet cover 30 is hermetically connected with the upper end of the central cylinder 112, and the lower end of the mounting frame 401 is hermetically connected with the upper end of the central cylinder 112.

In this embodiment, the annular light source 202 is installed through the bracket 11, the opening of the light-emitting cover 30 is hermetically connected with the upper end of the central tube 112, and the lower end of the mounting frame 401 is hermetically connected with the upper end of the central tube 112, so that the annular light source 202, the light-emitting cover 30 and the mounting frame 401 are conveniently assembled, and a relatively stable and reliable position relationship is formed. In addition, a sealing state is formed between the light-emitting cover 30, the mounting frame 401 and the lamp holder 10, so that a better waterproof sealing effect can be achieved, and the adaptability of the lamp holder used in the outdoor environment is improved.

In order to facilitate the assembly between the mounting frame 401 and the bracket 11, in an embodiment of the present invention, the flange seat 113 is disposed at the upper end of the central tube 112, the mounting frame 401 includes a supporting rod 401a and a flange 401b, the flange 401b is disposed at the lower end of the supporting rod 401a and is fixedly connected to the flange 401b, and the camera 402 and the radar device 50 are disposed at the upper end of the supporting rod 401 a.

In this embodiment, the flange 401b at the lower end of the support rod 401a is connected to the flange 401b at the upper end of the central tube 112 on the support 11, for example, the flange 401b and the flange seat 113 can be fastened and fixed by fasteners such as screws, which is convenient and reliable for connection and facilitates assembly between the mounting frame 401 and the support 11.

Advantageously, a compressed seal is provided between the flange 401b and the flange seat 113, so that a good sealing effect between the flange 401b and the flange seat 113 is ensured by the seal.

In order to achieve a good sealing effect between the light shield 30 and the support 11, the opening has a sealing edge, which is press-sealed against the flange seat 113 and surrounds the flange 401 b. During the equipment, compress tightly the light-emitting cover 30 downwards on lamp stand 10, at this moment, sealed along compressing tightly on flange seat 113, it is fixed through fasteners such as screws with the lower limb of light-emitting cover 30 again with lamp stand 10, so, light-emitting cover 30 and lamp stand 10 fixed connection axle, sealed edge and flange seat 113 can form the sealed effect of compressing tightly.

Preferably, a sealing ring may be disposed on the sealing edge, and the sealing performance between the sealing edge and the flange seat 113 is improved by using the elastic sealing performance of the sealing ring.

In an embodiment of the present invention, the mounting frame 401 further includes a carrying rod 401c, the carrying rod 401c is connected to the upper end of the supporting rod 401a and perpendicular to the supporting rod 401a, the number of the cameras 402 is two, two the cameras 402 are respectively installed at the two ends of the carrying rod 401c, the radar apparatus 50 is disposed on the carrying rod and is located between the cameras 402.

In this embodiment, adopt two cameras 402 to install at the both ends of carrying pole 401c, utilize two cameras 402 can increase the collection scope to, binocular camera 402 can obtain clearer video image data, improves image identification's accuracy. In addition, two cameras 402 and radar device 50 are installed on carrying pole 401c according to above-mentioned mode, simple to operate, and rationally distributed.

The utility model discloses an in an embodiment, still include wireless communication module, wireless communication module and controller, this wireless communication module can adopt mobile communication module, for example 4G or 5G module, also can adopt other wireless modules, and wireless communication module is used for communicating with telemonitoring equipment, be used for with video image data reaches radar data transmission that radar device 50 detected to telemonitoring equipment, and the control command that telemonitoring equipment sent. The controller is connected to the wireless communication module, the camera 402, the radar device 50 and the light source assembly 20, and is configured to control the light source module to change the working mode according to a control instruction.

That is to say, utilize wireless communication module can communicate with remote monitoring equipment, behind the video image data and the radar signal that remote monitoring equipment received, can carry out image recognition according to the video image data, whether have the aircraft in the discernment image, simultaneously, judge whether there is the aircraft near the sky according to the radar signal, exemplarily, if detect the aircraft at the radar signal, simultaneously, image recognition has the aircraft near the sky, so, both common result can obtain accurate testing result, aircraft detection's accuracy and reliability have been improved, and after detecting the aircraft, send control command to the barrier lamp, the controller can control mode switching according to this control command, for example, switch into the light of two kinds of different colours and flash, so, can play better warning effect.

The embodiment of the utility model provides an obstacle device is kept away to aviation obstruction beacon safety is still provided, include as above aviation obstruction beacon, and remote monitoring equipment, remote monitoring equipment with aviation obstruction beacon wireless communication connects, is used for the basis video image data and radar data output control command that aviation obstruction beacon sent, and send to aviation obstruction beacon.

According to the embodiment of the utility model provides a keep away barrier device safely, above-mentioned aviation obstruction beacon has, can gather near-empty video image data through camera 402 on the aviation obstruction beacon, radar installation 50 detects the radar signal of near-empty, video image data and radar signal send to remote monitoring equipment, utilize remote monitoring equipment to carry out the image recognition back, confirm whether there is the aircraft near-empty jointly with radar signal, so, can obtain more accurate testing result, switching mode according to testing result control obstruction beacon, and then can reach more reliable warning effect steadily. In addition, the camera 402 and the radar device 50 are integrated in the aviation obstruction light, so that the structure is simpler, the system is simplified, and the arrangement and implementation are convenient.

In the description herein, references to the description of the term "one embodiment," "some embodiments," "an example," "a specific example," or "some examples," etc., mean that a particular feature, structure, material, or characteristic described in connection with the embodiment or example is included in at least one embodiment or example of the invention. In this specification, the schematic representations of the terms used above are not necessarily intended to refer to the same embodiment or example. Furthermore, the particular features, structures, materials, or characteristics described may be combined in any suitable manner in any one or more embodiments or examples. Furthermore, various embodiments or examples and features of different embodiments or examples described in this specification can be combined and combined by one skilled in the art without contradiction.

The above only be the preferred embodiment of the utility model discloses a not consequently restriction the utility model discloses a patent range, all are in the utility model discloses a conceive, utilize the equivalent structure transform of what the content was done in the description and the attached drawing, or direct/indirect application all is included in other relevant technical field the utility model discloses a patent protection within range.

Claims (9)

1. An aviation obstruction light, comprising:

a lamp holder adapted to be mounted on an obstacle;

a light source assembly disposed within the lamp socket;

the light emitting cover is arranged at the top of the lamp holder and forms sealing with the lamp holder, and the top of the light emitting cover is provided with an opening;

the camera assembly comprises an installation frame and a camera, the lower end of the installation frame is positioned in the opening and is fixedly connected with the lamp holder, and the camera is fixed at the upper end of the installation frame and is used for collecting near-space video image data;

and the radar device is arranged at the upper end of the mounting rack and used for detecting the near-air aircraft.

2. The aircraft obstruction light of claim 1, wherein the light source assembly comprises:

the outer wall of the reflecting cup is provided with a reflecting cambered surface protruding inwards;

the annular light source is coaxially arranged below the reflecting cup, the light emitting direction of the annular light source is upward, so that light rays are projected upward to the reflecting cambered surface and are emitted out from the circumferential direction of the light emitting cover after being reflected by the reflecting cambered surface.

3. The aircraft obstruction light of claim 2, further comprising a bracket, wherein the bracket comprises a bottom plate and a central barrel, the bottom plate is fixed in the lamp holder, and the central barrel is arranged in the center of the bottom plate and protrudes upwards;

the annular light source is arranged on the bottom plate and located outside the central cylinder, the opening of the light outlet cover is connected with the upper end of the central cylinder in a sealing mode, and the lower end of the mounting frame is connected with the upper end of the central cylinder in a sealing mode.

4. The aircraft obstruction light of claim 3, wherein a flange seat is provided at the upper end of the central tube, the mounting rack comprises a support rod and a flange plate, the flange plate is located at the lower end of the support rod and is fixedly connected with the flange plate, and the camera and the radar device are arranged at the upper end of the support rod.

5. The aircraft obstruction light of claim 4, wherein the opening has a sealing rim that is compression sealed against the flange seat and surrounds the outside of the flange.

6. The aircraft obstruction light of claim 4, wherein a compressed gasket is disposed between the flange plate and the flange seat.

7. The aircraft obstruction light of claim 4, wherein the mounting bracket further comprises a carrier bar, the carrier bar is connected to the upper end of the support bar and perpendicular to the support bar, the number of the cameras is two, the two cameras are respectively mounted at two ends of the carrier bar, and the radar device is arranged on the carrier bar and located between the two cameras.

8. The aircraft obstruction light of claim 1, further comprising a wireless communication module, and a controller, wherein the wireless communication module is used for communicating with a remote monitoring device to transmit the video image data and the radar data detected by the radar device to the remote monitoring device and control instructions transmitted by the remote monitoring device, and the controller is connected with the wireless communication module, the camera, the radar device and the light source assembly to control the light source module to change the working mode according to the control instructions.

9. The utility model provides an obstacle device is kept away to aviation obstruction beacon safety which characterized in that includes:

an aviation obstruction light as claimed in any one of claims 1 to 8;

and the remote monitoring equipment is in wireless communication connection with the aviation obstruction light, is used for outputting a control instruction according to the video image data and the radar data sent by the aviation obstruction light, and sends the control instruction to the aviation obstruction light.

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