CN108105706B - Solar aviation obstruction light - Google Patents
Solar aviation obstruction light Download PDFInfo
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- CN108105706B CN108105706B CN201711490710.7A CN201711490710A CN108105706B CN 108105706 B CN108105706 B CN 108105706B CN 201711490710 A CN201711490710 A CN 201711490710A CN 108105706 B CN108105706 B CN 108105706B
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- 238000010438 heat treatment Methods 0.000 claims abstract description 64
- 230000006698 induction Effects 0.000 claims abstract description 16
- 239000005341 toughened glass Substances 0.000 claims description 13
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- VNWKTOKETHGBQD-UHFFFAOYSA-N methane Chemical compound C VNWKTOKETHGBQD-UHFFFAOYSA-N 0.000 claims description 4
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Classifications
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F21—LIGHTING
- F21S—NON-PORTABLE LIGHTING DEVICES; SYSTEMS THEREOF; VEHICLE LIGHTING DEVICES SPECIALLY ADAPTED FOR VEHICLE EXTERIORS
- F21S9/00—Lighting devices with a built-in power supply; Systems employing lighting devices with a built-in power supply
- F21S9/02—Lighting devices with a built-in power supply; Systems employing lighting devices with a built-in power supply the power supply being a battery or accumulator
- F21S9/03—Lighting devices with a built-in power supply; Systems employing lighting devices with a built-in power supply the power supply being a battery or accumulator rechargeable by exposure to light
- F21S9/032—Lighting devices with a built-in power supply; Systems employing lighting devices with a built-in power supply the power supply being a battery or accumulator rechargeable by exposure to light the solar unit being separate from the lighting unit
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F21—LIGHTING
- F21V—FUNCTIONAL FEATURES OR DETAILS OF LIGHTING DEVICES OR SYSTEMS THEREOF; STRUCTURAL COMBINATIONS OF LIGHTING DEVICES WITH OTHER ARTICLES, NOT OTHERWISE PROVIDED FOR
- F21V23/00—Arrangement of electric circuit elements in or on lighting devices
- F21V23/04—Arrangement of electric circuit elements in or on lighting devices the elements being switches
- F21V23/0442—Arrangement of electric circuit elements in or on lighting devices the elements being switches activated by means of a sensor, e.g. motion or photodetectors
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F21—LIGHTING
- F21V—FUNCTIONAL FEATURES OR DETAILS OF LIGHTING DEVICES OR SYSTEMS THEREOF; STRUCTURAL COMBINATIONS OF LIGHTING DEVICES WITH OTHER ARTICLES, NOT OTHERWISE PROVIDED FOR
- F21V23/00—Arrangement of electric circuit elements in or on lighting devices
- F21V23/04—Arrangement of electric circuit elements in or on lighting devices the elements being switches
- F21V23/0442—Arrangement of electric circuit elements in or on lighting devices the elements being switches activated by means of a sensor, e.g. motion or photodetectors
- F21V23/0464—Arrangement of electric circuit elements in or on lighting devices the elements being switches activated by means of a sensor, e.g. motion or photodetectors the sensor sensing the level of ambient illumination, e.g. dawn or dusk sensors
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F21—LIGHTING
- F21V—FUNCTIONAL FEATURES OR DETAILS OF LIGHTING DEVICES OR SYSTEMS THEREOF; STRUCTURAL COMBINATIONS OF LIGHTING DEVICES WITH OTHER ARTICLES, NOT OTHERWISE PROVIDED FOR
- F21V29/00—Protecting lighting devices from thermal damage; Cooling or heating arrangements specially adapted for lighting devices or systems
- F21V29/90—Heating arrangements
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F21—LIGHTING
- F21V—FUNCTIONAL FEATURES OR DETAILS OF LIGHTING DEVICES OR SYSTEMS THEREOF; STRUCTURAL COMBINATIONS OF LIGHTING DEVICES WITH OTHER ARTICLES, NOT OTHERWISE PROVIDED FOR
- F21V31/00—Gas-tight or water-tight arrangements
- F21V31/005—Sealing arrangements therefor
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F21—LIGHTING
- F21W—INDEXING SCHEME ASSOCIATED WITH SUBCLASSES F21K, F21L, F21S and F21V, RELATING TO USES OR APPLICATIONS OF LIGHTING DEVICES OR SYSTEMS
- F21W2111/00—Use or application of lighting devices or systems for signalling, marking or indicating, not provided for in codes F21W2102/00 – F21W2107/00
- F21W2111/04—Use or application of lighting devices or systems for signalling, marking or indicating, not provided for in codes F21W2102/00 – F21W2107/00 for waterways
Landscapes
- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Life Sciences & Earth Sciences (AREA)
- Sustainable Development (AREA)
- Circuit Arrangement For Electric Light Sources In General (AREA)
- Road Signs Or Road Markings (AREA)
Abstract
The invention is applicable to the technical field of aviation obstruction lights, and provides a solar aviation obstruction light, which comprises: the solar energy lamp comprises a lamp body base, a lamp body, a solar cell panel and a control device, wherein the lamp body is arranged above the lamp body base, the lamp body base is arranged above the control device, and the solar cell panel is arranged on one side of the control device; the solar aviation obstruction light further comprises a light induction sensor, a temperature induction sensor and a heating wire, wherein the light induction sensor and the temperature induction sensor are arranged on the base of the light body, and the heating wire is arranged in the light body and on the solar cell panel; the input end of the control device is connected with the light sensing sensor and the temperature sensing sensor, and the output end of the control device is connected with the heating wire. According to the solar energy aviation obstruction lamp, the temperature and the light information outside the lamp body are detected, so that the heating wire is controlled to automatically heat the solar cell panel and the lamp shade, the snow removing effect is achieved, and the problem that the solar energy aviation obstruction lamp cannot work normally under the condition of snow accumulation is solved.
Description
Technical Field
The invention belongs to the technical field of aviation obstruction lights, and particularly relates to a solar aviation obstruction light.
Background
According to the national standard, the high-rise building with the top 45 meters above the ground needs to be provided with aviation obstruction lights to display the outline of the building, thereby playing a role in warning the operator of the aircraft. With the continuous development of technology, solar aviation obstruction lights appear, and a new technical scheme is provided for the power supply mode of aviation obstruction lights. The solar cell panel is utilized by the aviation obstruction lights to convert solar energy into electric energy, so that power is supplied to the light bodies of the obstruction lights.
However, the solar cell panel of the traditional solar aviation obstruction light and the lampshade of the obstruction light are usually directly exposed in the air, the solar cell panel cannot work normally under the condition of snow in winter, and meanwhile, the light rays emitted by the obstruction light cannot be transmitted out due to the coverage of the snow, so that the solar aviation obstruction light cannot work normally, and accordingly an operator of an aircraft cannot be warned.
Disclosure of Invention
Therefore, the embodiment of the invention provides a solar aviation obstruction lamp to solve the problem that the solar aviation obstruction lamp in the prior art cannot work normally under the condition of snow accumulation.
The embodiment of the invention provides a solar aviation obstruction lamp, which comprises the following components: the solar lamp comprises a lamp body base, a lamp body, a solar panel and a control device, wherein the lamp body is arranged above the lamp body base, the lamp body base is arranged above the control device, and the solar panel is arranged on one side of the control device;
the solar lamp comprises a lamp body base, a lamp body, a solar cell panel, a temperature sensor, a light induction sensor, a temperature sensor and a heating wire, wherein the light induction sensor and the temperature sensor are arranged on the lamp body base; the input end of the control device is connected with the light sensing sensor and the temperature sensing sensor, the output end of the control device is connected with the heating wire and is used for receiving light information collected by the light sensing sensor and temperature information collected by the temperature sensing sensor, and sending out corresponding control instructions according to the received light information and temperature information and transmitting the control instructions to the heating wire.
Optionally, the control device includes: a micro control unit and a storage battery; the input end of the micro control unit is connected with the light sensing sensor and the temperature sensing sensor, and the output end of the micro control unit is connected with the heating wire; the input end of the storage battery is connected with the solar cell panel, and the output end of the storage battery is respectively connected with the lamp body, the light sensing sensor, the temperature sensing sensor, the heating wire and the micro-control unit.
Optionally, the lamp body includes: the lamp shade and the light emitting diode, the lamp shade is established on the lamp body base, the light emitting diode is located the lamp shade with the cavity that the lamp body base formed, the heater strip sets up on the lamp body base and be located in the cavity.
Optionally, a waterproof sealing ring is arranged at the joint of the lampshade and the lamp body base.
Optionally, the solar panel includes: the solar cell comprises a plurality of solar cells and toughened glass arranged above the solar cells, wherein the solar cells are horizontally arranged in parallel, gaps are reserved between adjacent edges of the solar cells, and the heating wires are arranged in the toughened glass corresponding to the gaps of the solar cells.
Optionally, the heating wire is a low-temperature wire of a carbon fiber wire.
Optionally, the output end of the control device is further connected to the light emitting diode, and the light emitting diode is configured to receive a control instruction sent by the control device.
Optionally, the solar aviation obstruction light further comprises a distance sensor, the distance sensor is arranged on the base of the light body, and the output end of the distance sensor is connected with the control device.
Optionally, the solar aviation obstruction light further comprises a micro alarm, wherein the micro alarm is arranged on the base of the light body, and the input end of the micro alarm is connected with the control device.
Optionally, the solar aviation obstruction light further comprises a micro alarm, wherein the micro alarm is arranged on the base of the light body, and the input end of the micro alarm is connected with the control device.
Compared with the prior art, the embodiment of the invention has the beneficial effects that: whether the solar aviation obstruction light flashes or not is detected by arranging the light sensing sensor on the light body base part of the solar aviation obstruction light, and meanwhile, the temperature around the light body is detected by arranging the temperature sensing sensor on the light body base part of the solar aviation obstruction light, the light information collected by the light sensing sensor and the temperature information collected by the temperature sensing sensor are received by arranging the control device below the light body base, corresponding control instructions are sent out according to the received light information and the temperature information, and the heating wires arranged in the light body and on the solar cell panel heat according to the received instructions so as to eliminate snow on the lampshade and the solar cell panel, so that the problem that the solar aviation obstruction light cannot work normally under the condition of snow in the prior art is solved.
Drawings
In order to more clearly illustrate the technical solutions of the embodiments of the present invention, the drawings that are needed in the embodiments or the description of the prior art will be briefly described below, it being obvious that the drawings in the following description are only some embodiments of the present invention, and that other drawings may be obtained according to these drawings without inventive effort for a person skilled in the art.
Fig. 1 is a schematic perspective view of a solar aviation obstruction beacon according to an embodiment of the present invention;
FIG. 2 is a block diagram of a control device according to an embodiment of the present invention;
FIG. 3 is a schematic view of a lamp base according to an embodiment of the present invention;
fig. 4 is a schematic structural diagram of a heating wire in a lamp body according to an embodiment of the present invention;
fig. 5 is a structural exploded view of a solar panel according to an embodiment of the present invention;
fig. 6 is a top view of a solar panel according to an embodiment of the present invention.
Detailed Description
In the following description, for purposes of explanation and not limitation, specific details are set forth such as the particular system architecture, techniques, etc., in order to provide a thorough understanding of the embodiments of the present invention. It will be apparent, however, to one skilled in the art that the present invention may be practiced in other embodiments that depart from these specific details. In other instances, detailed descriptions of well-known systems, devices, circuits, and methods are omitted so as not to obscure the description of the present invention with unnecessary detail.
In order to illustrate the technical scheme of the invention, the following description is made by specific examples.
Referring to fig. 1, a schematic perspective view of a solar aviation obstruction beacon is provided, which is described in detail below:
the solar aviation obstruction light comprises a light body base 101, a light body 102, a solar cell panel 103 and a control device 104, wherein the light body 102 is arranged above the light body base 101, the light body base 101 is arranged above the control device 104, the solar cell panel 103 is arranged on one side of the control device 104, and an included angle between the solar cell panel and the control device in the vertical direction is 45-60 degrees, so that the solar cell panel 103 can collect solar energy better and convert the solar energy into electric energy.
The solar aviation obstruction light further comprises a light induction sensor 105, a temperature induction sensor 106 and a heating wire, wherein the light induction sensor 105 and the temperature induction sensor 106 are arranged on the light body base 101, and the heating wire is arranged in the light body 102 and on the solar cell panel 103; the input end of the control device 104 is connected with the light sensing sensor 105 and the temperature sensing sensor 106, and the output end of the control device 104 is connected with the heating wire and is used for receiving the light information collected by the light sensing sensor 105 and the temperature information collected by the temperature sensing sensor 106, and sending out corresponding control instructions according to the received light information and temperature information and transmitting the corresponding control instructions to the heating wire.
In addition, a device base 107 is further arranged below the control device 104, so that a certain distance is reserved between the control device 104 and the ground, the control device 104 is not contacted with the ground, corrosion of the control device 104 by the ground is reduced, and the service life of the device is prolonged.
The inventor finds that the solar aviation obstruction lights can cause snow to exist outside the lampshade of the aviation obstruction lights and outside the solar panel under the condition of snow in winter in the process of realizing the solar aviation obstruction lights, and the solar panel cannot work normally due to the shielding of the snow, even the battery hot spot effect appears, and the battery panel is damaged; meanwhile, the light rays emitted by the aviation obstruction lights are also blocked by snow, so that an operator of the aircraft cannot be warned.
According to the invention, the light sensing sensor and the temperature sensing sensor are arranged on the lamp body base, the light information and the environment temperature information outside the lamp body are detected through the light sensing sensor and the temperature sensing sensor, the control device is arranged to collect the light information and the environment temperature information and process the received information, when the control device does not receive the light information, and meanwhile, when the received temperature information is smaller than a preset value, the control device sends a control instruction to the electric heating wire, so that the electric heating wire starts to heat, and snow accumulated outside the lamp body and snow accumulated outside the solar cell panel are eliminated.
Alternatively, referring to fig. 2, a composition diagram of a control device 104 is shown, the control device 104 including a micro control unit 1041 and a battery 1042; the input end of the micro control unit 1041 is connected with the light sensing sensor 105 and the temperature sensing sensor 106, and the output end of the micro control unit 1041 is connected with a heating wire; the input end of the storage battery 1042 is connected with the solar panel 103, and the output end of the storage battery 1042 is respectively connected with the lamp body 102, the light sensing sensor 105, the temperature sensing sensor 106, the heating wire and the micro-control unit 1041.
The control device 104 includes a micro control unit 1041 and a storage battery 1042, where the micro control unit 1041 is configured to receive information collected by the light sensor 105 and the temperature sensor 106, identify and determine the received information, and determine whether the current state is in a snow covered state.
The operation of the photo sensor 105 and the temperature sensor 106 is as follows: when detecting the optical signal, the optical sensor 105 converts the optical signal into an electrical signal and transmits the electrical signal to the micro control unit 1041 in the control device 104; the temperature sensor 106 may be an infrared temperature sensor, where the infrared temperature sensor may sense ambient temperature, when the temperature of the object is higher than absolute zero, infrared radiation is generated, and the infrared radiation generated by the object is related to the temperature of the object, the higher the temperature is, the stronger the infrared radiation is, the infrared temperature sensor generates corresponding electric signals after receiving the infrared radiation signals, and transmits the electric signals to the micro control unit 1041 in the control device 104, and the micro control unit 1041 determines the environmental status according to the received electric signals.
Referring to fig. 3, an arrangement of a photo sensor and a temperature sensor on a lamp body base is shown, and in order to ensure accuracy of light information and temperature information detected by the photo sensor and the temperature sensor, two photo sensors and two temperature sensors are respectively arranged on the lamp body base. Wherein the photo-sensing sensors 1051 and 1052 are respectively disposed in the horizontal direction of the lamp socket, and the temperature sensing sensors 1061 and 1062 are respectively disposed in the vertical direction of the lamp socket. It will be readily appreciated that the arrangement of the number and location of the sensors is merely an embodiment and is not limiting.
Illustratively, the process of determining the current environmental state by the micro control unit 1041 of the control device 104 according to the received electrical signal is: when the micro control unit 1041 continuously receives the signals of no light emitted by the light sensing sensors 1051 and 1052 and simultaneously receives the signals of less than 0 ℃ emitted by the temperature sensing sensors 1061 and 1062, the current environment is judged to be in a state of being covered with snow, and a heating signal is emitted to the heating wire; when the micro control unit 1041 continuously receives a signal that one of the light sensing sensors 1051 and 1052 emits no light and simultaneously receives a signal that one of the temperature sensing sensors 1061 and 1062 emits about 30 ℃, it is determined that the living organism in the current environment stays near the barrier lamp and emits a corresponding signal; when the micro control unit 1041 continuously receives a signal that one of the light sensing sensors 1051 and 1052 emits no light, and simultaneously receives a signal that one of the temperature sensing sensors 1061 or 1062 emits a signal of less than 0 degrees celsius, it determines that the current environment is snowy, and the default snow can be automatically melted without sending a heating signal to the heating wire.
In addition, the battery 1042 in the control device 104 serves to store the electric energy generated by the solar cell panel 103 and to supply electric energy for the light emitted by the lamp body at night. The output end of the storage battery is also connected with the light induction sensor, the temperature induction sensor, the heating wire and the control unit for providing electric energy for the normal operation of the storage battery.
Optionally, referring to fig. 4, the lamp body includes: the lamp shade 401 and emitting diode, lamp shade are established on the lamp body base, and emitting diode is located the lamp shade with the cavity that the lamp body base formed, heater strip 402 sets up on the lamp body base and is located the cavity. The heating wire is connected with the control device through a wire 403.
In order to enable the heating wire to rapidly remove snow outside the lampshade, the heating wire is uniformly distributed on one side close to the lampshade in a continuous U-shaped state, and the heating value of the heating wire is increased by arranging the heating wire into the U-shaped shape. By arranging the heating wire on the side close to the lampshade, the heat generated by the heating wire is preferentially conducted to the side close to the lampshade to eliminate snow on the lampshade, for example, the heating wire is close to the inner wall of the lampshade, and the maximum distance between the heating wire and the lampshade is smaller than a threshold value, for example, the threshold value can be one tenth of the diameter of the cylindrical part of the lampshade.
It is to be understood that the arrangement of the shape and position of the heating wire is only an embodiment, and is not limited thereto. The embodiment adopts a light emitting diode (Light Emitting Diode, LED) as a light source, and compared with the traditional xenon lamp tube, the LED lamp has the advantages of long service life and low power consumption.
Optionally, a waterproof sealing ring is arranged at the joint of the lampshade and the lamp body base. Through set up waterproof sealing circle in the junction of lamp shade and lamp shade base in the rainwater inflow lamp shade when avoiding sleet weather to and prevent in the lamp body flows into to the rainwater that the lamp shade heating produced through the heater strip under the snow circumstances, cause the damage of the internal circuit of lamp, thereby extension aviation obstruction lamp's life-span.
Optionally, the solar panel includes: the solar cell comprises a plurality of solar cells and toughened glass arranged above the solar cells, wherein the solar cells are horizontally arranged in parallel, gaps are reserved between adjacent edges of the solar cells, and the heating wires are arranged in the toughened glass corresponding to the gaps of the solar cells.
Referring to fig. 5, there is shown an exploded view of a solar panel comprising front and back tempered glass 501 and 505, eva encapsulant layers 502 and 504, and a solar cell sheet 503. The front-side tempered glass 501 is directly contacted with sunlight, and the sunlight passes through the front-side tempered glass 501 and the EVA packaging layer 502, so that the light energy is converted into electric energy on the solar cell 503. Wherein the heating wires are printed in the front tempered glass 501 and are close to the outer surface of the glass, so that the temperature will be preferentially conducted to the snow-covered outer surface when heating. For example, when the thickness of the front tempered glass is 4 to 6 mm, the heating wire may be disposed at 1 mm to 1.5 mm near the outer surface of the glass.
Referring to fig. 6, a top view of a solar panel is shown. Where 601 denotes a heating wire printed in front tempered glass and 602 denotes a solar cell. For example, an arrangement of 3 rows and 5 columns of solar cells is provided, where the solar cells are arranged in series or parallel to form a 3 row and 5 column arrangement, and a certain gap is left between every two rows or every two columns of solar cells. Here we use the position in the toughened glass corresponding to the gap between the cells to set the heater strip, thereby avoiding the heater strip from affecting the power generation of the solar cells. The drawings show a case where the heating wire is disposed by using the gap between the two rows of the battery pieces, and the heating wire may be disposed by using the gap between the two columns of the battery pieces, which is not particularly limited herein.
Optionally, the heating wire is a low-temperature wire of a carbon fiber wire. The low-temperature wire of the carbon fiber wire is a fibrous heating wire, is a novel material with electrical, mechanical and thermal properties, and has the characteristics of stability, long service life and high heat conversion rate. Due to the action of carbon molecules, the surface of the heating wire can be quickly heated.
Here, since the lowest softening temperature of EVA in the EVA encapsulation layer is 70 ℃, the heating temperature range of the heating wire may be set to 0-70 ℃, thereby ensuring that the temperature of the inner surface of the heating wire does not exceed 70 ℃ during heating. Experiments prove that when the temperature of the heating wire reaches 70 ℃, the temperature sensing sensor monitors that the external temperature reaches 55 ℃, the purpose of removing snow can be achieved by continuously heating for 1-4 minutes, and the purpose of removing ice can be achieved by continuously heating for 6-10 minutes.
Optionally, the output end of the control device is further connected to the light emitting diode, and the light emitting diode is used for receiving a control instruction sent by the control device.
The solar aviation obstruction lamp provided by the embodiment of the invention also has a sensor for monitoring whether organisms fall on the lamp body base. For example, when the micro control unit 1041 continuously receives a signal that one of the light sensing sensors 1051 and 1052 emits no light, and simultaneously receives a signal that one of the temperature sensing sensors 1061 and 1062 emits a signal of about 30 degrees celsius, it is determined that the living body stays near the obstruction light, and at this time, the micro control unit 1041 emits a signal for driving the living body to the light emitting diode, so that the light emitting diode blinks for a certain period of time to drive the living body, so as to prevent the living body from leaving feces on the base of the lamp body, and ensure that the light sensing sensor and the temperature sensing sensor can normally collect the temperature information and the light information of the accessory of the lamp body. Of course, this is the case if the obstruction light is in a non-24 hour mode of operation, and when the obstruction light is in a 24 hour mode of operation, the obstruction light will be in a continuously blinking state, i.e., no living organisms will remain in the vicinity of the obstruction light.
Optionally, the solar aviation obstruction light further comprises a distance sensor, the distance sensor is arranged on the base of the light body, and the output end of the distance sensor is connected with the control device.
The aviation obstruction light provided by the embodiment of the invention is also provided with the distance sensor, the distance sensor is also arranged on the light body base, the distance between the surrounding moving object and the obstruction light is detected through the distance sensor, the detected signal is sent to the control device, and the micro control unit in the control device is used for analyzing the received signal and sending out a corresponding instruction.
Optionally, the solar aviation obstruction light further comprises a micro alarm, wherein the micro alarm is arranged on the base of the light body, and the input end of the micro alarm is connected with the control device.
When the micro control unit in the control device analyzes that the received signal of the distance sensor is smaller than a preset value, a control signal is sent to the micro alarm, so that the alarm sends out audible and visual alarm information to remind an operator of the aircraft, the solar aviation obstruction lamp has more comprehensive functions, and the operator of the aircraft can be reminded when the aviation obstruction lamp temporarily cannot work due to the fact that snow on the outside of the aviation obstruction lamp is not melted.
Optionally, referring to fig. 1, a lightning protection device 108 is disposed above the lamp body. By arranging the lightning protection device 108, a certain lightning protection effect can be achieved, and the risk that the aviation obstruction light is damaged by lightning is reduced.
Above-mentioned solar energy aviation obstruction beacon, through setting up light-sensitive sensor and temperature-sensitive sensor setting on the lamp body base, detect outside light information of lamp body and ambient temperature information through light-sensitive sensor and temperature-sensitive sensor, and set up controlling means and collect light information and ambient temperature information, and handle the information of receiving, when controlling means did not receive light information, simultaneously when the temperature information of receiving is less than the default, controlling means sent control command and given the heating wire, make the heating wire begin to heat, thereby eliminate the outside snow of lamp body and the outside snow of solar cell panel, simultaneously the obstruction beacon sends the sound of reporting to the police when detecting that there is the object to be close to the obstruction beacon, and waterproof, function such as lightning-arrest, thereby extension obstruction beacon's life.
It will be apparent to those skilled in the art that, for convenience and brevity of description, only the above-described division of the functional modules is illustrated, and in practical application, the above-described functional allocation may be performed by different functional units or modules according to needs, i.e. the internal structure of the apparatus is divided into different functional units or modules to perform all or part of the above-described functions. In the embodiment, each unit may exist alone physically, or two or more units may be integrated in one unit, where the integrated unit may be implemented in a form of hardware or a form of a software functional unit. In addition, specific names of the functional units and modules are only for convenience of distinguishing from each other, and are not used for limiting the protection scope of the present application. The specific working process of the module in the foregoing embodiment may refer to the corresponding process in the foregoing embodiment, and will not be described herein.
Those of ordinary skill in the art will appreciate that the modules of the examples described in connection with the embodiments disclosed herein can be implemented as electronic hardware, or as a combination of computer software and electronic hardware. Whether such functionality is implemented as hardware or software depends upon the particular application and design constraints imposed on the solution. Skilled artisans may implement the described functionality in varying ways for each particular application, but such implementation decisions should not be interpreted as causing a departure from the scope of the present invention.
In the embodiments provided in the present invention, it should be understood that the disclosed apparatus may be implemented in other manners. For example, the apparatus embodiments described above are merely illustrative, and for example, the division of the modules is merely a logical function division, and there may be additional divisions when actually implemented, for example, multiple units or components may be combined or integrated into another system, or some features may be omitted or not performed. Alternatively, the coupling or direct coupling or communication connection shown or discussed may be an indirect coupling or communication connection via interfaces, devices or units, which may be in electrical, mechanical or other forms.
The units described as separate units may or may not be physically separate, and units shown as units may or may not be physical units, may be located in one place, or may be distributed on a plurality of network units. Some or all of the units may be selected according to actual needs to achieve the purpose of the solution of this embodiment.
In addition, in each embodiment of the invention, each unit may exist alone physically, or two or more units may be integrated into one unit. The integrated units may be implemented in hardware or in software functional units.
The above embodiments are only for illustrating the technical solution of the invention, and are not limiting; although the invention has been described in detail with reference to the foregoing embodiments, it will be understood by those of ordinary skill in the art that: the technical scheme described in the foregoing embodiments can be modified or some technical features thereof can be replaced by equivalents; such modifications and substitutions do not depart from the spirit and scope of the technical solutions of the embodiments of the present invention, and are intended to be included in the scope of the present invention.
Claims (7)
1. A solar energy aviation obstruction light comprising: the solar lamp comprises a lamp body base, a lamp body, a solar panel and a control device, wherein the lamp body is arranged above the lamp body base, the lamp body base is arranged above the control device, and the solar panel is arranged on one side of the control device;
the solar lamp is characterized by further comprising a light induction sensor, a temperature induction sensor and a heating wire, wherein the light induction sensor and the temperature induction sensor are arranged on a lamp body base, and the heating wire is arranged in the lamp body and on a solar cell panel;
the input end of the control device is connected with the light sensing sensor and the temperature sensing sensor, the output end of the control device is connected with the heating wire, and the control device is used for receiving the light information collected by the light sensing sensor and the temperature information collected by the temperature sensing sensor, sending out corresponding control instructions according to the received light information and temperature information and transmitting the corresponding control instructions to the heating wire;
the lamp body comprises a lamp shade and a light emitting diode, the lamp shade is arranged on the lamp body base, the light emitting diode is positioned in a cavity formed by the lamp shade and the lamp body base, and the heating wire is arranged on the lamp body base and positioned in the cavity; the output end of the control device is also connected with the light emitting diode, and the light emitting diode is used for receiving a control instruction sent by the control device;
the control device includes: a micro control unit and a storage battery; the input end of the micro control unit is connected with the light sensing sensor and the temperature sensing sensor, and the output end of the micro control unit is connected with the heating wire; the input end of the storage battery is connected with the solar cell panel, and the output end of the storage battery is respectively connected with the lamp body, the light sensing sensor, the temperature sensing sensor, the heating wire and the micro-control unit;
the light body is provided with a working mode of not twenty-four hours, and when the light body is in the working mode of not twenty-four hours, the micro control unit continuously receives a signal of no light emitted by the light sensing sensor, and meanwhile, when the temperature sensing sensor emits a signal of thirty ℃, the current environment is judged to stay near the obstacle lamp, and at the moment, the micro control unit emits a signal for driving the organism to the light emitting diode, so that the light emitting diode blinks for a certain period of time to drive the organism.
2. The solar aviation obstruction beacon of claim 1, wherein a waterproof sealing ring is arranged at the joint of the lamp shade and the lamp body base.
3. The solar-powered aircraft obstruction light of claim 1, wherein the solar panel comprises: the solar cell comprises a plurality of solar cells and toughened glass arranged above the solar cells, wherein the solar cells are horizontally arranged in parallel, gaps are reserved between adjacent edges of the solar cells, and the heating wires are arranged in the toughened glass corresponding to the gaps of the solar cells.
4. The solar aviation obstruction light of claim 1, wherein the heating filament is a low temperature filament of carbon fiber wire.
5. The solar aviation obstruction beacon of claim 1, further comprising a distance sensor disposed on the base of the beacon body, wherein an output of the distance sensor is coupled to the control device.
6. The solar aviation obstruction beacon of claim 1, further comprising a micro-alarm, wherein the micro-alarm is disposed on the base of the beacon, and wherein an input of the micro-alarm is connected to the control device.
7. A solar aviation obstruction beacon according to any one of claims 1 to 6, wherein a lightning arrester is provided above the lamp body.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201711490710.7A CN108105706B (en) | 2017-12-30 | 2017-12-30 | Solar aviation obstruction light |
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| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201711490710.7A CN108105706B (en) | 2017-12-30 | 2017-12-30 | Solar aviation obstruction light |
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| Publication Number | Publication Date |
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| CN108105706A CN108105706A (en) | 2018-06-01 |
| CN108105706B true CN108105706B (en) | 2024-04-05 |
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| Application Number | Title | Priority Date | Filing Date |
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| CN201711490710.7A Active CN108105706B (en) | 2017-12-30 | 2017-12-30 | Solar aviation obstruction light |
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Families Citing this family (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109927858A (en) * | 2019-03-28 | 2019-06-25 | 海星海事电气集团有限公司 | Naval light |
| CN110307510A (en) * | 2019-06-21 | 2019-10-08 | 深圳星标科技股份有限公司 | Solar energy aviation obstruction beacon |
| CN111120911B (en) * | 2019-12-17 | 2021-11-30 | 上海宙虹电子科技有限公司 | Multifunctional aviation obstruction beacon |
| CN112664890A (en) * | 2020-12-23 | 2021-04-16 | 王贵 | Solar street lamp convenient to clearance |
| CN113108252B (en) * | 2021-04-23 | 2022-09-02 | 李田方 | High-altitude obstacle lamp for high-rise building roof |
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|---|---|
| CN108105706A (en) | 2018-06-01 |
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