CN215001353U

CN215001353U - Regulation type aviation obstruction beacon

Info

Publication number: CN215001353U
Application number: CN202121326601.3U
Authority: CN
Inventors: 甄如碧; 钟新春
Original assignee: CHENGDU JINHUA UTILITY ELECTRICAL APPARATUS RESEARCH INSTITUTE CO LTD
Current assignee: CHENGDU JINHUA UTILITY ELECTRICAL APPARATUS RESEARCH INSTITUTE CO LTD
Priority date: 2021-06-15
Filing date: 2021-06-15
Publication date: 2021-12-03
Anticipated expiration: 2031-06-15

Abstract

The utility model provides an adjustable aviation obstruction beacon, which comprises a sealed shell; the inside of the sealed shell is provided with a lighting rotating wheel component, a rotation adjusting motor, a driving wheel and a driven wheel, gear belts are sleeved outside the driving wheel and the driven wheel, and the output end of the rotation adjusting motor is connected with the center of the driving wheel; the center of the side end face of the illumination rotating wheel component is provided with an adjusting gear, the center of the illumination rotating wheel component is provided with three illuminating lamps, the three illuminating lamps are mutually separated by a reflecting plate, and the illumination rotating wheel component is composed of a front circular end face and a rear circular end face which are made of reflecting plates and a circular ring plate which is made of transparent materials. Through set up illumination runner part, adjusting gear, rotation accommodate motor, action wheel and follow the driving wheel in sealed shell inside to set up three light in illumination runner part, utilize the light to separate the light with three, just so can select the light of using as required to throw light on, thereby can realize low light intensity, well light intensity and three kinds of modes of low light intensity.

Description

Regulation type aviation obstruction beacon

Technical Field

The utility model particularly relates to a regulation type aviation obstruction beacon.

Background

The aviation obstruction light is one of navigation aid light equipment, and in order to be distinguished from a common light, the aviation obstruction light is not normally on but flashes, the low-light-intensity aviation obstruction light is normally on, and the medium-light-intensity aviation obstruction light and the high-light-intensity aviation obstruction light flash, and the aviation obstruction light has the function of displaying the outline of a structure, so that an aircraft operator can judge the height and the outline of an obstacle, and the warning function is achieved. The aviation obstruction light is mainly divided into three types of low light intensity, medium light intensity and low light intensity, most of the existing aviation obstruction lights can only realize one of the three types of lighting modes, and therefore, an adjustable aviation obstruction light capable of adjusting the three types of lighting modes is provided.

SUMMERY OF THE UTILITY MODEL

An object of the utility model is to prior art not enough, provide a regulation type aviation obstruction beacon, this regulation type aviation obstruction beacon can solve above-mentioned problem well.

In order to meet the above requirements, the utility model adopts the following technical scheme: the adjustable aviation obstruction light comprises a sealed shell; the inside of the sealed shell is provided with a lighting rotating wheel component, a rotation adjusting motor, a driving wheel and a driven wheel, gear belts are sleeved outside the driving wheel and the driven wheel, and the output end of the rotation adjusting motor is connected with the center of the driving wheel; the illumination rotating wheel component is characterized in that an adjusting gear is arranged at the center of the side end face of the illumination rotating wheel component, three illuminating lamps are arranged at the center of the illumination rotating wheel component and are separated from each other by a reflecting plate, and the illumination rotating wheel component is composed of a front circular end face and a rear circular end face which are made of reflecting plates and a circular ring plate which is made of a light-transmitting material.

The adjustable aviation obstruction light has the following advantages:

through at inside illumination runner part that sets up of sealed shell, adjusting gear, rotation accommodate motor, action wheel, installation base, gear belt and from the driving wheel to set up three light in illumination runner part, utilize the light to separate the light with the three, just so can select the light of using as required to throw light on, thereby can realize low light intensity, well light intensity and three kinds of modes of low light intensity.

Drawings

The accompanying drawings, which are included to provide a further understanding of the application and are incorporated in and constitute a part of this application, illustrate embodiment(s) of the application and together with the description serve to explain the application and not to limit the application. In the drawings:

fig. 1 schematically shows a structural view of a regulated aviation obstruction light according to one embodiment of the present application.

Fig. 2 schematically illustrates a top view of a tuned aviation obstruction light in accordance with one embodiment of the present application.

Fig. 3 schematically illustrates a structural view of an illuminated wheel component of a dimmable aircraft obstruction light according to an embodiment of the present application.

Wherein: 1. sealing the shell; 2. a solar panel; 3. an illumination wheel member; 4. an adjusting gear; 5. rotating the adjusting motor; 6. a driving wheel; 7. installing a base; 8. a gear belt; 9. a driven wheel; 10. installing a bolt; 11. a spindle member; 12. an illuminating lamp; 13. a reflector.

Detailed Description

In order to make the objects, technical solutions and advantages of the present application more apparent, the present application will be described in further detail with reference to the accompanying drawings and specific embodiments.

In the following description, references to "one embodiment," "an embodiment," "one example," "an example," etc., indicate that the embodiment or example so described may include a particular feature, structure, characteristic, property, element, or limitation, but every embodiment or example does not necessarily include the particular feature, structure, characteristic, property, element, or limitation. Moreover, repeated use of the phrase "in accordance with an embodiment of the present application" although it may possibly refer to the same embodiment, does not necessarily refer to the same embodiment.

Certain features that are well known to those skilled in the art have been omitted from the following description for the sake of simplicity.

According to an embodiment of the present application, there is provided a dimmable aircraft obstruction light, as shown in fig. 1-3, comprising a sealed envelope 1; the inside of the sealing shell 1 is provided with a lighting rotating wheel component 3, a rotation adjusting motor 5, a driving wheel 6 and a driven wheel 9, gear belts 8 are sleeved outside the driving wheel 6 and the driven wheel 9, and the output end of the rotation adjusting motor 5 is connected with the center of the driving wheel 6; the center of the side end face of the illumination rotating wheel component 3 is provided with an adjusting gear 4, the center of the illumination rotating wheel component 3 is provided with three illumination lamps 12, the three illumination lamps 12 are mutually separated by a reflector 13, and the illumination rotating wheel component 3 is composed of a front circular end face and a rear circular end face which are made of reflector plates and a circular ring plate which is made of transparent materials.

According to one embodiment of the application, the bottom of the sealed shell 1 of the adjustable aviation obstruction light is provided with a mounting base 7, and at least four mounting bolts 10 are inserted on the mounting base 7.

According to one embodiment of the application, the side end face of the sealed case 1 of the adjustment type aviation obstruction light is connected with the solar cell panel 2 through the rotating shaft part 11.

According to one embodiment of the application, the gear belt 8 of the adjusting type aviation obstruction light is provided with insections meshed with the adjusting gear 4.

According to an embodiment of the present application, three of the illumination lamps 12 of the adjustable aviation obstruction light are respectively a low-intensity illumination lamp, a medium-intensity illumination lamp and a high-intensity illumination lamp.

According to one embodiment of the application, the rotation adjusting motor 5 and the illumination rotating wheel component 3 of the adjusting type aviation obstruction light are fixedly connected to the inner end face of the sealing shell 1 through connecting rods.

According to one embodiment of the application, the adjusting gear 4, the driving wheel 6 and the driven wheel 9 of the adjusting type aviation obstruction light are rotatably connected to the inner end face of the sealing shell 1 through a rotating shaft structure.

According to one embodiment of the application, the sealed shell 1 of the adjustable aviation obstruction light is internally provided with an electric storage component which is electrically connected with the illuminating lamp 12, the rotation adjusting motor 5 and the solar cell panel 2.

According to one embodiment of the application, a control component electrically connected with the illuminating lamp 12 and the rotation adjusting motor 5 is arranged inside the sealed shell 1 of the adjusting type aviation obstruction light, and the control component is a single chip microcomputer.

According to an embodiment of the application, the adjustable aviation obstruction light can be used for fixedly mounting the device on the top of a building by using a mounting bolt 10, the structure of the sealing shell 1 is shown in figure 1, the middle part of the sealing shell can be an upward protruding round structure, the part of the structure can be made of transparent materials, the rotating adjusting motor 5 can drive the driving wheel 6 to rotate, thereby driving the gear belt 8 to move, thereby driving the adjusting gear 4 and the illumination wheel component 3 to rotate, so that the orientation of the illumination wheel component 3 can be changed, different illuminating lamps 12 can be used for illuminating upwards when needed, a sensor component can be arranged in the illuminating rotating wheel component 3, the illuminating lamps 12 can be powered on and emit light when each illuminating lamp 12 faces upwards, and a signal receiving and transmitting device electrically connected with the control component can be arranged in the sealing shell 1, so that the orientation of the illuminating rotating wheel component 3 can be remotely controlled. The structure is attractive and practical in overall structure, and meanwhile, the vent can be arranged on the sealing shell 1 to realize cooling.

According to an embodiment of the application, this regulation type aviation obstruction beacon is through setting up illumination runner part 3 in sealed shell 1 inside, adjusting gear 4, rotate accommodate motor 5, action wheel 6, installation base 7, gear belt 8 and follow driving wheel 9 to set up three light 12 in illumination runner part 3, utilize light 12 to separate light 12 with three, just so can select light 12 of using as required to throw light on, thereby can realize low light intensity, three kinds of modes of medium light intensity and low light intensity.

The above-described embodiments are merely illustrative of several embodiments of the present invention, which are described in detail and detail, but should not be construed as limiting the scope of the present invention. It should be noted that, for those skilled in the art, without departing from the spirit of the present invention, several variations and modifications can be made, which are within the scope of the present invention. Therefore, the protection scope of the present invention should be subject to the claims.

Claims

1. The utility model provides a regulation type aviation obstruction beacon which characterized in that: comprises a sealed shell;

the inside of the sealing shell is provided with a lighting rotating wheel component, a rotation adjusting motor, a driving wheel and a driven wheel, gear belts are sleeved outside the driving wheel and the driven wheel, and the output end of the rotation adjusting motor is connected with the center of the driving wheel;

the lighting rotating wheel component is characterized in that an adjusting gear is arranged at the center of the side end face of the lighting rotating wheel component, three lighting lamps are arranged at the center of the lighting rotating wheel component and are separated from each other by a reflecting plate, and the lighting rotating wheel component is composed of a front circular end face and a rear circular end face which are made of reflecting plates and a circular ring plate which is made of a light-transmitting material.

2. The adjustable aviation obstruction light of claim 1, wherein: the bottom of the sealing shell is provided with an installation base, and at least four installation bolts are inserted into the installation base.

3. The adjustable aviation obstruction light of claim 1, wherein: the side end face of the sealing shell is connected with the solar cell panel through the rotating shaft component.

4. The adjustable aviation obstruction light of claim 1, wherein: the gear belt is provided with insections meshed with the adjusting gear.

5. The adjustable aviation obstruction light of claim 1, wherein: the three illuminating lamps are respectively a low-light-intensity illuminating lamp, a medium-light-intensity illuminating lamp and a high-light-intensity illuminating lamp.

6. The adjustable aviation obstruction light of claim 1, wherein: the rotation adjusting motor and the illumination rotating wheel part are fixedly connected to the inner end face of the sealing shell through a connecting rod.

7. The adjustable aviation obstruction light of claim 1, wherein: the adjusting gear, the driving wheel and the driven wheel are rotatably connected to the inner end face of the sealing shell through a rotating shaft structure.

8. The adjustable aviation obstruction light of claim 1, wherein: the inside of the sealing shell is provided with a control part which is electrically connected with the illuminating lamp and the rotation adjusting motor, and the control part is a single chip microcomputer.