CN205979559U

CN205979559U - Novel solar energy aviation lamp

Info

Publication number: CN205979559U
Application number: CN201620893063.9U
Authority: CN
Inventors: 薛晨博
Original assignee: Individual
Current assignee: Individual
Priority date: 2016-08-17
Filing date: 2016-08-17
Publication date: 2017-02-22
Anticipated expiration: 2026-08-17

Abstract

The utility model discloses a novel solar energy aviation lamp sets up the aviation lamp on the aviation lamp stand, the aviation lamp stand sets up at the electric cabinet top, be provided with total controller in the electric cabinet box to reach dc -to -ac converter and the group battery be connected with total controller, the bottom of electric cabinet is provided with automatically controlled tank base, the box of electric cabinet is provided with solar power system outward. The utility model discloses simple structure, intelligent degree is high, and a large amount of energy losses that traditional long distance wire carried the electric energy to cause have been overcome in the wide accessible space in make full use of airport and integrated setting has been realized with aviation lamp and electric cabinet to the light energy at sunshine of the abundance that provides, simultaneously set up the solar power system that can carry out the angle modulation on the electric cabinet, realized the self -sufficiency or the partly self -supporting of aviation lamp power consumption, the setting of wireless receiving module has realized having improved the interior accurate control to the whole aviation lamp in airport of control tower to the remote control and control location of solar control cabinet, has ensured the safety of aviation operation.

Description

A kind of new type solar energy aeronautical light

Technical field

This utility model designs air equipment field, specially a kind of new type solar energy aeronautical light.

Background technology

With social develop rapidly and science and technology continuous progress, especially the vehicles develop rapidly so that Life radius in the effective time of people is increasing, and as the most efficiently air transportation, has had become as every country Emphasis is encouraged and is had the means of transportation in large development space.

In the evolution of aviation industry, the use face of electric power is quite varied, and usage amount ratio is larger, and various high-altitudes set Apply such as squarer, high-rise, beacon etc. to get more and more, for aviation safety, they are all to boat in a way Empty potentially dangerous barrier, aviation obstruction beacon, as a kind of often bright or flicker red safelight lamp, can effectively indicate High-altitude barrier, is the critical facility of aircraft navigation.

At present, traditional aeronautical light be all low-voltage power supply so energy consumption is very low, but need for being supplied to by electric wire Electric energy light, when mounted, be necessary for electric wire to be installed, and will also result in the loss of electricity in midway, cause lamp source Waste, on rainy day, rainwater can penetrate into power supply, cause aeronautical light cannot normal work, thus there is potential safety hazard so that boat The inadequate energy-conserving and environment-protective of empty lamp, uniformity of luminance is poor；And the aviation industry developing rapidly, for luminaire for air traffic usage amount increasingly Many, the electric power dependency for highly energy-consuming is more and more stronger, how enough for the electric energy of offer aeronautical light using aviation condition Provide safeguard, and increase service life and the use quality of aeronautical light, be a good problem to study.

Content of the invention

In order to overcome above-mentioned deficiency of the prior art, this utility model utilizes airport shelter few, cuts sunshine and adopts The sufficient strong natural environment of light, there is provided a kind of structure is simple, and generated energy is big, it is possible to achieve partial amount can clean self-sufficiency New type solar energy aeronautical light.

The purpose of this utility model is realized in：

A kind of new type solar energy aeronautical light, is arranged on the aeronautical light 4 on aviation lamp socket；Described aviation lamp socket is arranged on electricity Control box top；Be provided with master controller 19 in described automatically controlled box body, and the inverter 20 that is connected with master controller 19 and Set of cells 12；The bottom of described electric cabinet is provided with electric cabinet base 15；It is provided with solar electrical energy generation outside the casing of electric cabinet Device；

Described aviation lamp socket is liftable seat, including the lamp holder 2 being fixed on automatically controlled box top, described lamp holder 2 Inside it is provided with the elevating lever 5 being controlled by master controller 19；Aeronautical light 4 is fixed with described elevating lever 5, aeronautical light 4 is outer to be arranged There is the lampshade 3 being fixed on elevating lever 5；

It is provided with the radio receiving transmitting module 1 being connected with master controller 19 in described lamp holder 2；

The bottom of described electric cabinet base 15 is provided with universal wheel 16；By lifting hydraulic cylinder 17 with electric cabinet bottom even Connect；Described electric cabinet bottom is provided with moisture-proof heat-insulation insulating barrier 14；

Described device of solar generating includes the first TRT being arranged on automatically controlled box top, and is arranged on automatically controlled The second TRT on the wall of case side；

The first described TRT includes the first solar panels 7, is arranged on the first of the first solar panels 7 one end bottom Lifting support 6, and the directive wheel 8 being arranged on the first solar panels 7 other end bottom；Described directive wheel 8 is located at and is arranged on In the slideway of automatically controlled box top；

The second described TRT includes the second solar panels 10 being arranged on the wall of electric cabinet side；Described second is too The upper end of sun energy plate 10 is hinged with electric cabinet side wall upper part by jointed shaft 9, and lower end is passed through the second lifting and supported 13 and electric cabinet Side wall connects；

Blower fan 18 is provided with described electric cabinet side wall, the relative side wall of setting blower fan is provided with BAIYE air regulator 11.

Positive beneficial effect：This utility model structure is simple, and intelligence degree is high, makes full use of wide accessible in airport Space and the sunshine luminous energy of abundance that provides, aeronautical light and electric cabinet are achieved integrated setting, overcome traditional length away from Convey a large amount of electric energy losses that electric energy causes from wire；The solar energy that angular adjustment can be carried out is provided with electric cabinet simultaneously TRT is it is achieved that the self-sufficiency of aeronautical light electricity consumption or partly self-supporting；And the setting of the blower fan on the wall of electric cabinet side and shutter, Increased the result of ventilating heat dissipation in switch board, there is provided the safe handling of switch board, delay service life；Wireless receiving The setting of module, it is achieved that the distant control to solar control cabinet and monitoring positioning, improves whole to airport in control tower Being precisely controlled of body aeronautical light, has ensured the safety of aviation operation.

Brief description

Fig. 1 is structural representation one of the present utility model；

Fig. 2 is structural representation two of the present utility model；

Fig. 3 is structural representation three of the present utility model；

In figure is：Radio receiving transmitting module 1, lamp holder 2, lampshade 3, aeronautical light 4, elevating lever 5, first lifting support 6, first Solar panels 7, directive wheel 8, jointed shaft 9, the second solar panels 10, BAIYE air regulator 11, set of cells 12, second lifting support 13, Moisture-proof heat-insulation insulating barrier 14, electric cabinet base 15, universal wheel 16, lifting hydraulic cylinder 17, blower fan 18, master controller 19, inverter 20.

Specific embodiment

Below in conjunction with the accompanying drawings, this utility model is described further：

As shown in figure 1, a kind of new type solar energy aeronautical light, it is arranged on the aeronautical light 4 on aviation lamp socket；Described aeronautical light Seat is arranged on automatically controlled box top；It is provided with master controller 19 in described automatically controlled box body, and be connected with master controller 19 Inverter 20 and set of cells 12；The bottom of described electric cabinet is provided with electric cabinet base 15；It is provided with outside the casing of electric cabinet Device of solar generating；

Embodiment 1

As shown in Fig. 2 when oblique fire in sunlight, carrying out sending out in order to allow solar panels preferably absorb luminous energy Electricity, is supported 13 lifting, realizes the second solar panels with jointed shaft 9 as the center of circle, with the second solar panels be by the second lifting The regulation at the angle of inclination of radius, carries out realizing slanting the substantially vertical of angle with the sun.

Embodiment 2

As shown in Fig. 2 when oblique fire in sunlight, carrying out sending out in order to allow solar panels preferably absorb luminous energy Electricity, supports 6 lifting by the first lifting, and the one end realizing first solar panels setting the first lifting support is slowly risen, separately Then under directive wheel 8 is along the movement in slideway, slowly close to the first support 6, it is right to realize, and the first solar panels tilt for one end The regulation of angle, carries out realizing slanting the substantially vertical of angle with the sun.

Implement 3

Embodiment 1 is adjusted with the solar energy equipment in embodiment 2 simultaneously, is realized the first TRT and second Electric installation is vertical with while solar energy angle of inclination.

This utility model structure is simple, and intelligence degree is high, makes full use of the wide clear space in airport and provides Sufficient sunshine luminous energy, aeronautical light and electric cabinet are achieved integrated setting, overcome traditional distance wire conveying electricity The a large amount of electric energy losses that can cause；The device of solar generating that angular adjustment can be carried out is provided with electric cabinet simultaneously, real Self-sufficiency or the partly self-supporting of aeronautical light electricity consumption are showed；And the setting of the blower fan on the wall of electric cabinet side and shutter, increased control Result of ventilating heat dissipation in cabinet, there is provided the safe handling of switch board, delays service life；The setting of wireless receiving module Put it is achieved that the distant control to solar control cabinet and monitoring positioning, improve in control tower to airport entirety aeronautical light Be precisely controlled, ensured the safety of aviation operation.

Above-described embodiment is merely to illustrate the technical scheme that this utility model is embodied as rather than is limited, affiliated The those of ordinary skill of technical field it should be understood that without prejudice on the premise of this utility model objective, do not change its performance or Any equivalent substitute or obvious modification that purposes is carried out to embodiment of the present utility model, all should cover please in this utility model Ask in the range of protection.

Claims

1. a kind of new type solar energy aeronautical light, is arranged on the aeronautical light on aviation lamp socket；It is characterized in that：Described aviation lamp socket It is arranged on automatically controlled box top；It is provided with master controller, and the inverter being connected with master controller in described automatically controlled box body And set of cells；The bottom of described electric cabinet is provided with electric cabinet base；It is provided with solar electrical energy generation dress outside the casing of electric cabinet Put.

2. new type solar energy aeronautical light according to claim 1 it is characterised in that：Described aviation lamp socket is liftable Seat, including the lamp holder being fixed on automatically controlled box top, is provided with, in described lamp socket body, the elevating lever being controlled by master controller；Institute Aeronautical light is fixed with the elevating lever stated, outside aeronautical light, is provided with the lampshade being fixed on elevating lever.

3. new type solar energy aeronautical light according to claim 1 and 2 it is characterised in that：It is provided with described lamp socket body The radio receiving transmitting module being connected with master controller.

4. new type solar energy aeronautical light according to claim 1 it is characterised in that：The bottom of described electric cabinet base sets It is equipped with universal wheel；It is connected with electric cabinet bottom by lifting hydraulic cylinder；Described electric cabinet bottom is provided with moisture-proof heat-insulation insulation Layer.

5. new type solar energy aeronautical light according to claim 1 it is characterised in that：Described device of solar generating includes It is arranged on the first TRT of automatically controlled box top, and be arranged on the second TRT on the wall of electric cabinet side.

6. new type solar energy aeronautical light according to claim 5 it is characterised in that：The first described TRT includes One solar panels, the first lifting being arranged on first solar panels one end bottom supports, and it is another to be arranged on the first solar panels The directive wheel of one end bottom；Described directive wheel is located at and is arranged in the slideway of automatically controlled box top.

7. new type solar energy aeronautical light according to claim 5 it is characterised in that：The second described TRT includes setting Put the second solar panels on the wall of electric cabinet side；Jointed shaft and electric cabinet side wall are passed through in the upper end of the second described solar panels Upper articulation, lower end is passed through the second lifting support and is connected with electric cabinet side wall.

8. according to claim 1 or 5 new type solar energy aeronautical light it is characterised in that：Set on described electric cabinet side wall It is equipped with blower fan, the relative side wall of setting blower fan is provided with BAIYE air regulator.