CN218819838U

CN218819838U - Open-air guarantee point aid to navigation lighting system

Info

Publication number: CN218819838U
Application number: CN202223182776.9U
Authority: CN
Inventors: 白筠; 何俊; 梁志军; 杨锐; 张书侨; 唐虎
Original assignee: Equipment Repairing Factory Chengdu Aviation Station No4 Air Force
Current assignee: Equipment Repairing Factory Chengdu Aviation Station No4 Air Force
Priority date: 2022-11-30
Filing date: 2022-11-30
Publication date: 2023-04-07
Anticipated expiration: 2032-11-30

Abstract

The utility model belongs to the technical field of navigation aid lighting, in particular to a field guarantee point navigation aid lighting system, which comprises a lighting bracket, wherein the lighting bracket is provided with a plurality of light brackets, the light brackets are provided with omnidirectional luminous ground beacon lamps, and the omnidirectional luminous ground beacon lamps are connected with a lighting controller and a power supply controller; the omnidirectional light-emitting ground beacon light comprises a light housing, wherein the light housing comprises a lower housing and an upper housing, a storage battery is arranged in the light housing, a switch is arranged on the surface of the light housing, a light-emitting diode is arranged in the spotlight cover, the storage battery is connected with the light-emitting diode, the inner wall of the spotlight cover is provided with a light band matched with the light-emitting diode correspondingly, and a reflecting film is arranged in the middle of the light housing. The application meets the airport navigation aid operation requirements of the lighting system, ensures the guidance of airplanes in the airport, indicates navigation aid light sources, improves the reliability, the safety and the luminous efficiency of the whole system, and overcomes the problem of poor display effect of light source of lighting system lamps.

Description

Open-air guarantee point aid to navigation lighting system

Technical Field

The utility model belongs to the technical field of aid to navigation light, concretely relates to open-air guarantee point aid to navigation lighting system.

Background

The navigation-aid lighting equipment is a special lamp for marking obstacles, belongs to the industry of navigation-aid lighting equipment, and is a range of lamp types under the seat of the navigation-aid lighting equipment.

In the prior art, for example, an invention patent with a patent number CN201510380444.7 and a name of "internet airport navigation light display and control system", a technical scheme thereof is as follows: the invention discloses an internet airport navigation aid light display and control system which comprises navigation aid light and a control center, wherein the navigation aid light is composed of a plurality of light groups.

In the light system of the above patent, although the GPRS module is added to the system, the overall light source effect of the lamp in the light system is not further improved.

Disclosure of Invention

In order to meet the airport navigation aid operation requirements of a lighting system, ensure the guidance and the indication of an airport airplane and overcome the problem of poor display effect of a light source of a lighting system lamp, the field support point navigation aid lighting system is provided, and the specific scheme is as follows:

a field guarantee point aid to navigation lighting system comprises a lighting fixture, wherein a plurality of light brackets are arranged on the lighting fixture, omnidirectional luminous ground beacon lights are arranged on the light brackets, and the omnidirectional luminous ground beacon lights are connected with a lighting controller and a power controller;

the omnidirectional light-emitting ground beacon light comprises a light housing, wherein the light housing comprises a lower housing and an upper housing, the bottom of the upper housing is provided with a spotlight cover, an antenna and a handle, a fixing ring is arranged between the spotlight cover and the upper housing, a storage battery is arranged in the light housing, a switch is arranged on the surface of the light housing, a light-emitting diode is arranged in the spotlight cover, the storage battery is connected with the light-emitting diode, the inner wall of the spotlight cover is provided with a light band which is correspondingly matched with the light-emitting diode, and a reflecting film is arranged in the middle of the light housing.

Furthermore, the light emitting diodes are arranged on the pentagonal cylinder light source seat, each pentagonal cylinder light source seat uses 6 light emitting diodes as light sources, 1 light emitting diode is arranged at the top end of the pentagonal cylinder light source seat, and the other 5 light emitting diodes are respectively arranged on five surfaces of the light source seat.

Furthermore, the spotlight cover is in a semicircular arc shape, the bottom of the spotlight cover is provided with a protruding edge, the upper part of the protruding edge is provided with an annular bulge, and the upper part of the spotlight cover is provided with a plurality of light bands distributed from top to bottom.

Furthermore, the upper shell and the lower shell are made of abs materials through injection molding.

Further, the reflective membrane is a 3M diamond-grade reflective membrane, and the area of the reflective membrane is 90cm ² -100cm ² 。

Furthermore, the lamp bracket comprises a bracket body and a charging electrode positioned at the rear end of the bracket body, an omnidirectional light-emitting ground beacon lamp is installed in each lamp bracket, and installation guide grooves which are obliquely arranged are formed in the inner walls of the two sides of the bracket body.

Further, the lighting fixture is multilayer frame construction, the lighting fixture includes the skeleton and is located the fixed foot spare of skeleton bottom, is provided with the aviation socket on every layer of lighting fixture.

Furthermore, a transmitting antenna is arranged on the light controller, a transmitter and a switch power supply are arranged in the light controller, a power switch, a first-level brightness button, a second-level brightness button, a third-level brightness button, a light-off button and corresponding working indicator lights are arranged on the front panel, the rear panel has three sockets, namely a high-frequency socket, an alternating current 220 volt input socket and a two-core aviation socket, wherein the high-frequency socket screws in a plug of the transmitting antenna.

Further, the power supply controller comprises an alternating current switch, an alternating current fuse holder, a charging output voltmeter and an ammeter which are arranged on a front panel, an alternating current 220-volt input socket is arranged in the middle of the back surface of the power supply controller, two 24V power output aviation sockets are arranged on two sides of the power supply controller, and the power supply controller is connected to the charging input aviation socket of the lamp holder through power lines of the double aviation plugs.

The application has the advantages that:

this application sets up lower shell and last shell through being provided with upper and lower structure to be provided with battery, emitting diode and light band in the lamp body, and the reflective membrane at cooperation lamp body middle part, satisfied lighting system airport navigation aid operation demand, guarantee airport aircraft guide, instruct navigation aid light source, improved entire system's reliability, security and luminous efficacy, overcome the not good problem of lighting system lamps and lanterns light source display effect.

Drawings

Fig. 1 is a schematic overall structure diagram of the present application.

Fig. 2 is a schematic structural view of the omnidirectional light-emitting ground beacon light of the present application.

Fig. 3 is a sectional view taken along line a of fig. 2.

Fig. 4 is a schematic view of a single lamp bracket structure.

In the drawings: the lamp comprises a lamp holder 1, a lamp bracket 2, a omnidirectional light emitting ground beacon lamp 3, a light controller 4, a power controller 5, a bracket body 21, a charging electrode 22, an installation guide groove 23, a lower shell 31, an upper shell 32, a condenser lamp shade 33, an antenna 34, a fixing ring 35, a storage battery 36, a light emitting diode 37, a lifting handle 38, a light band 39 and a reflecting film 310.

Detailed Description

In order to make the objects, technical solutions and advantages of the embodiments of the present application clearer, the technical solutions in the embodiments of the present application will be clearly and completely described below with reference to the drawings in the embodiments of the present application, and it is obvious that the described embodiments are some embodiments of the present application, but not all embodiments. The components of the embodiments of the present application, generally described and illustrated in the figures herein, can be arranged and designed in a wide variety of different configurations.

Thus, the following detailed description of the embodiments of the present application, as presented in the figures, is not intended to limit the scope of the claimed application, but is merely representative of selected embodiments of the application. All other embodiments, which can be derived by a person skilled in the art from the embodiments given herein without making any creative effort, shall fall within the protection scope of the present application.

It should be noted that: like reference numbers and letters refer to like items in the following figures, and thus, once an item is defined in one figure, it need not be further defined and explained in subsequent figures.

In the description of the present application, it should be noted that the terms "upper", "vertical", "inner", "outer", and the like indicate orientations or positional relationships based on the orientations or positional relationships shown in the drawings, or orientations or positional relationships that are conventionally arranged when products of the application are used, or orientations or positional relationships that are conventionally understood by those skilled in the art, and are used for convenience of description and simplification of the description, but do not indicate or imply that the devices or elements that are referred to must have a specific orientation, be constructed in a specific orientation, and be operated, and thus, should not be construed as limiting the application. Furthermore, the terms "first," "second," and the like are used merely to distinguish one description from another, and are not to be construed as indicating or implying relative importance.

In the description of the present application, it should also be noted that, unless expressly stated or limited otherwise, the terms "disposed," "mounted," and "connected" are to be construed broadly and can include, for example, fixed connections, detachable connections, or integral connections; 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 application can be understood in a specific case by those of ordinary skill in the art.

Example 1

As shown in fig. 1, 2 and 3, a field safeguard point navigation aid light system comprises a light holder 1, wherein a plurality of light brackets 2 are arranged on the light holder 1, an omnidirectional light-emitting ground beacon light 3 is arranged on the light brackets 2, and the omnidirectional light-emitting ground beacon light 3 is connected with a light controller 4 and a power controller 5; the omnidirectional light-emitting ground beacon light 3 comprises a light shell, the light shell comprises a lower shell 31 and an upper shell 32, the bottom of the upper shell 32 is provided with a spotlight cover 33, an antenna 34 and a lifting handle 38, a fixing ring 35 is arranged between the spotlight cover 33 and the upper shell 32, a storage battery 36 is arranged inside the light shell, a switch is arranged on the surface of the light shell, a light-emitting diode 37 is arranged in the spotlight cover 33, the storage battery 36 is connected with the light-emitting diode 37, the inner wall of the spotlight cover 33 is provided with a light band 39 which is matched with the light-emitting diode 37 in a corresponding mode, and a reflective film 310 is arranged in the middle of the light shell. The lower shell 31 and the last shell 32 of structure about being provided with are set up to this application to be provided with battery 36, emitting diode 37 and light band 39 in the lamp body, and the reflective membrane 310 at cooperation lamp body middle part, satisfied lighting system airport navigation aid operation demand, guarantee airport aircraft guide, instruct navigation aid light source, improved entire system's reliability, security and luminous efficiency, overcome the not good problem of lighting system lamps and lanterns light source display effect.

Example 2

As shown in fig. 1, 2 and 3, a field safeguard point navigation aid light system comprises a light holder 1, wherein a plurality of light brackets 2 are arranged on the light holder 1, an omnidirectional light-emitting ground beacon light 3 is arranged on the light brackets 2, and the omnidirectional light-emitting ground beacon light 3 is connected with a light controller 4 and a power controller 5; the omnidirectional light-emitting ground beacon light 3 comprises a light shell, the light shell comprises a lower shell 31 and an upper shell 32, the bottom of the upper shell 32 is provided with a spotlight cover 33, an antenna 34 and a lifting handle 38, a fixing ring 35 is arranged between the spotlight cover 33 and the upper shell 32, a storage battery 36 is arranged inside the light shell, a switch is arranged on the surface of the light shell, a light-emitting diode 37 is arranged in the spotlight cover 33, the storage battery 36 is connected with the light-emitting diode 37, the inner wall of the spotlight cover 33 is provided with a light band 39 corresponding to and matched with the light-emitting diode 37, and a reflective film 310 is arranged in the middle of the light shell.

The light emitting diodes 37 are arranged on the pentagonal cylinder light source seat, each pentagonal cylinder light source seat uses 6 light emitting diodes 37 as light sources, 1 light emitting diode 37 is arranged at the top end of the pentagonal cylinder light source seat, and the other 5 light emitting diodes 37 are respectively arranged on five surfaces of the light source seat. The light emitting diode 37 light source penetrates through the omnidirectional lamp condenser lamp cover 33 to ensure that the maximum light intensity value emitted within the range of 360 degrees horizontally and 3 degrees to 5 degrees vertically meets the index requirement. Especially in the range of the main beam vertical to about 4.5 degrees, the light intensity of the rest various colors can reach more than 80 cd.

The condenser lamp shade 33 is in a semi-circular arc shape, the bottom of the condenser lamp shade is provided with a protruding edge, the upper part of the protruding edge is provided with an annular bulge, and the upper part of the condenser lamp shade 33 is provided with a plurality of light bands 39 distributed from top to bottom.

The upper housing 32 and the lower housing 31 are made of abs material by injection molding. The composite material has the characteristics of impact resistance, scratch resistance, stable size and the like, and also has the characteristics of moisture resistance, corrosion resistance, easiness in processing and the like.

The reflective membrane 310 is a 3M diamond-grade reflective membrane 310, and the area of the reflective membrane 310 is 90cm2-100cm2. The reflective film 310 protection is a special protection mode, and is suitable for realizing ground no-light protection by irradiating the reflective film 310 with an aircraft landing lamp under the conditions of power supply damage, line fault, blocked control, ground light control and the like under wartime and emergency conditions. The diamond grade reflective film 310 adopts the latest reflection technology of the microcrystal cube corner body, so that incident light forms total internal reflection, and the base reflection performance is several times of that of the traditional engineering grade and high-strength reflective film 310. Considering the structural characteristics of the lamp, the reflecting area is set to be 90cm2-100cm2. The test shows that the reflecting effect is excellent, and the reflecting effect is clear when the car light is used as a light source for irradiation beyond 1 kilometer.

As shown in fig. 4, the lamp bracket 2 includes a bracket body 21 and a charging electrode 22 at the rear end of the bracket body 21, an omnidirectional light-emitting floor marker lamp 3 is installed in each lamp bracket 2, and the inner walls of both sides of the bracket body 21 are provided with installation guide grooves 23 arranged obliquely. The lamp bracket 2 is an injection molding and is arranged on the lamp bracket 1, one omnidirectional light-emitting ground beacon light 3 is arranged in each bracket, and the omnidirectional light-emitting ground beacon light 3 can be fixed on the lamp bracket 1 through the brackets. In order to meet the charging requirement of the navigation aid lamp, a charging electrode 22 is arranged at the rear part of the bracket, and a DC24V charging power supply is led to the lamp on the charging electrode 22 through a charging circuit for charging. For improving safety, the lamp bracket 2 is provided with a mounting guide groove 23 inclined by 10 degrees, and the charging electrode 22 is used for positioning, so that the lamp can be firmly mounted on the lamp holder 1. In order to fully utilize the limited space, all the lamp holders 1 are uniformly arranged on the left and right lamp holders 1 at a certain interval, and the lamps can be interchangeably arranged in the lamp bracket 2.

The lamp holder 1 is of a multi-layer frame structure, the lamp holder 1 comprises a framework and fixing foot pieces located at the bottom of the framework, and each layer of the lamp holder 1 is provided with an aviation socket. For example, the lamp holders 1 need to store 36 lamps, the lamp holders 1 are designed into 6 independent units with the same structure, each lamp holder 1 can meet the storage and charging requirements of 6 lamps, and the lamp holders have universality and can be exchanged randomly when in use. For guaranteeing that lighting fixture 1 quality satisfies lightweight designing requirement, lighting fixture 1 piles up lightly portably, and lighting fixture 1 designs to frame construction, and is formed by the high and light section bar steel pipe welding of intensity, and the surface is handled through the plastic-blasting, installs annexes such as fixed foot spare, electric appliance aviation socket in the lamp on the lighting fixture 1 skeleton, and the power cord of the two aviation plugs of aviation socket accessible between upper and lower lighting fixture 1 is connected, and the aviation socket on bottommost layer or upper strata can be connected to charging source. The charging power supply is connected with a 220V mains supply, and the lamp can be charged by turning on the charging power supply.

The light controller 4 is provided with a transmitting antenna 34, a transmitter and a switching power supply are arranged in the light controller 4, a power switch, a first-level brightness, a second-level brightness, a third-level brightness, a light-off button and corresponding working indicator lights are arranged on the front panel, three sockets are arranged on the rear panel, namely a high-frequency socket, an alternating-current power supply 220 volt input socket and a two-core aviation socket, and a plug of the transmitting antenna 34 is screwed in by the high-frequency socket. The SLR-1625E transmitter selected by the light controller 4 has the characteristics of long signal transmitting distance, accurate and stable signal, and effectively ensures that the wireless control of the light system is not less than 3 kilometers. In order to improve the applicability and the security of the lighting system, a lithium battery and a corresponding charging circuit are arranged in the lighting controller 4 and are controlled by a switching power supply, and the lighting system can be fixedly or portably used as required when in use. Meanwhile, two transmitting antennas 34 are arranged according to the use condition of the light controller 4, one transmitting antenna is a small antenna 34 which can be used in a portable mode, and the remote control distance is relatively short and is about 1 kilometer; one is a sucker type large antenna 34 which can be fixed for use and has a longer remote control distance which is not less than 3 kilometers. Both the two can be fixed on the high-frequency socket of the case and can be selected according to the guarantee requirement.

The power supply controller 5 comprises an alternating current switch, an alternating current fuse holder, a charging output voltmeter and an ammeter which are arranged on a front panel, wherein an alternating current 220-volt input socket is arranged in the middle of the back surface of the power supply controller 5, two 24V power output aviation sockets are arranged on two sides of the back surface of the power supply controller, and a power line of the double aviation plugs is connected to the charging input aviation socket of the lamp holder 1. The power controller 5 is internally provided with a switching power supply which can convert an input alternating current power supply into a direct current power supply to charge the lamps of the whole system. The charging requirements of the operation lamps are guaranteed by combining airfield aid lamplight, two aviation sockets with 24V input are arranged on each side plate of each lamp bracket 1 of the lighting system in parallel and are connected through a long connecting wire provided with an aviation plug. After the lamp holders 1 are stacked together, the lamp holders 1 and the lamp holders 1 are connected in parallel through short connecting lines. Meanwhile, two aviation sockets with 24V output are mounted on the rear panel of the power controller 5, and when charging is conducted, only after the power controller 5 is switched on, a lamp mounted on the lamp holder 1 can be charged. And meanwhile, all charging interfaces are designed to be in the same type, and all connecting wires can be interchanged.

This application sets up lower shell 31 and last shell 32 through being provided with upper and lower structure to be provided with battery 36, emitting diode 37 and light band 39 in the lamp body, and the reflective membrane 310 at cooperation lamp body middle part, satisfied lighting system airport navigation aid operation demand, guarantee airport aircraft guide, instruct navigation aid light source, improved entire system's reliability, security and luminous efficacy, overcome the not good problem of lighting system lamps and lanterns light source display effect.

Claims

1. The utility model provides a light system assists in navigation is ordered to open-air guarantee, includes lighting fixture (1), its characterized in that: the lamp bracket (1) is provided with a plurality of lamp brackets (2), the lamp brackets (2) are provided with omnidirectional light-emitting ground beacon lamps (3), and the omnidirectional light-emitting ground beacon lamps (3) are connected with a light controller (4) and a power supply controller (5);

luminous ground beacon light of qxcomm technology (3) includes the lamp body, the lamp body is including lower shell (31) and last shell (32), the bottom of going up shell (32) is provided with spotlight cover (33), antenna (34) and handle (38), spotlight cover (33) and last shell (32) between be provided with retainer plate (35), the inside battery (36) that is provided with of lamp body, the surface is provided with the switch, be provided with emitting diode (37) in spotlight cover (33), battery (36) link to each other with emitting diode (37), spotlight cover (33) inner wall is provided with and corresponds light band (39) of matching with emitting diode (37), the lamp body middle part is provided with reflective membrane (310).

2. The field security point navigation lighting system of claim 1, wherein: the light emitting diodes (37) are arranged on the pentagonal cylinder light source seat, each pentagonal cylinder light source seat uses 6 light emitting diodes (37) as light sources, 1 light emitting diode (37) is arranged at the top end of the pentagonal cylinder light source seat, and the other 5 light emitting diodes (37) are respectively arranged on five surfaces of the light source seat.

3. The field security point navigational lighting system of claim 1, wherein: the spotlight cover (33) is in a semicircular arc shape, the bottom of the spotlight cover is provided with a protruding edge, the upper part of the protruding edge is provided with an annular bulge, and the upper part of the spotlight cover (33) is provided with a plurality of light bands (39) distributed from top to bottom.

4. The field security point navigational lighting system of claim 1, wherein: the upper shell (32) and the lower shell (31) are made of abs materials in an injection molding mode.

5. The field security point navigational lighting system of claim 1, wherein: the reflective film (310) is a 3M diamond-grade reflective film (310), and the area of the reflective film (310) is 90cm2-100cm2.

6. The field security point navigational lighting system of claim 1, wherein: the lamp bracket (2) comprises a bracket body (21) and a charging electrode (22) positioned at the rear end of the bracket body (21), an omnidirectional light-emitting ground beacon light (3) is installed in each lamp bracket (2), and installation guide grooves (23) which are obliquely arranged are formed in the inner walls of the two sides of the bracket body (21).

7. The field security point navigational lighting system of claim 1, wherein: the lamp holder (1) is of a multi-layer frame structure, the lamp holder (1) comprises a framework and fixing foot pieces located at the bottom of the framework, and an aviation socket is arranged on each layer of the lamp holder (1).

8. The field security point navigational lighting system of claim 1, wherein: the lighting control device is characterized in that a transmitting antenna (34) is arranged on the lighting controller (4), a transmitter and a switching power supply are installed inside the lighting controller (4), a power switch, a first-level brightness, a second-level brightness, a third-level brightness and a lamp turning-off button and corresponding working indicator lamps are arranged on the front panel, three sockets are arranged on the rear panel, namely a high-frequency socket, an alternating-current power supply 220 volt input socket and a two-core aviation socket, and a plug of the transmitting antenna (34) is screwed in by the high-frequency socket.

9. The field security point navigational lighting system of claim 1, wherein: the power supply controller (5) comprises an alternating current switch, an alternating current fuse holder, a charging output voltmeter and an ammeter which are arranged on a front panel, wherein an alternating current 220-volt input socket is arranged in the middle of the back face of the power supply controller (5), two 24V power supply output aviation sockets are arranged on two sides of the power supply controller, and the power supply controller is connected to the charging input aviation socket of the lamp holder (1) through power lines of the two aviation plugs.