CN104421812A - Airport parking apron light - Google Patents

Airport parking apron light Download PDF

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Publication number
CN104421812A
CN104421812A CN201310393389.6A CN201310393389A CN104421812A CN 104421812 A CN104421812 A CN 104421812A CN 201310393389 A CN201310393389 A CN 201310393389A CN 104421812 A CN104421812 A CN 104421812A
Authority
CN
China
Prior art keywords
lower casing
circuit board
lamp
battery
component
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Pending
Application number
CN201310393389.6A
Other languages
Chinese (zh)
Inventor
周明杰
李林忠
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Oceans King Lighting Science and Technology Co Ltd
Shenzhen Oceans King Lighting Engineering Co Ltd
Original Assignee
Oceans King Lighting Science and Technology Co Ltd
Shenzhen Oceans King Lighting Engineering Co Ltd
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Oceans King Lighting Science and Technology Co Ltd, Shenzhen Oceans King Lighting Engineering Co Ltd filed Critical Oceans King Lighting Science and Technology Co Ltd
Priority to CN201310393389.6A priority Critical patent/CN104421812A/en
Publication of CN104421812A publication Critical patent/CN104421812A/en
Pending legal-status Critical Current

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Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F21LIGHTING
    • F21SNON-PORTABLE LIGHTING DEVICES; SYSTEMS THEREOF; VEHICLE LIGHTING DEVICES SPECIALLY ADAPTED FOR VEHICLE EXTERIORS
    • F21S9/00Lighting devices with a built-in power supply; Systems employing lighting devices with a built-in power supply
    • F21S9/02Lighting 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
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F21LIGHTING
    • F21VFUNCTIONAL FEATURES OR DETAILS OF LIGHTING DEVICES OR SYSTEMS THEREOF; STRUCTURAL COMBINATIONS OF LIGHTING DEVICES WITH OTHER ARTICLES, NOT OTHERWISE PROVIDED FOR
    • F21V23/00Arrangement of electric circuit elements in or on lighting devices
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F21LIGHTING
    • F21VFUNCTIONAL FEATURES OR DETAILS OF LIGHTING DEVICES OR SYSTEMS THEREOF; STRUCTURAL COMBINATIONS OF LIGHTING DEVICES WITH OTHER ARTICLES, NOT OTHERWISE PROVIDED FOR
    • F21V23/00Arrangement of electric circuit elements in or on lighting devices
    • F21V23/04Arrangement of electric circuit elements in or on lighting devices the elements being switches
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F21LIGHTING
    • F21VFUNCTIONAL FEATURES OR DETAILS OF LIGHTING DEVICES OR SYSTEMS THEREOF; STRUCTURAL COMBINATIONS OF LIGHTING DEVICES WITH OTHER ARTICLES, NOT OTHERWISE PROVIDED FOR
    • F21V3/00Globes; Bowls; Cover glasses
    • F21V3/02Globes; Bowls; Cover glasses characterised by the shape
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F21LIGHTING
    • F21WINDEXING SCHEME ASSOCIATED WITH SUBCLASSES F21K, F21L, F21S and F21V, RELATING TO USES OR APPLICATIONS OF LIGHTING DEVICES OR SYSTEMS
    • F21W2111/00Use or application of lighting devices or systems for signalling, marking or indicating, not provided for in codes F21W2102/00 – F21W2107/00
    • F21W2111/06Use or application of lighting devices or systems for signalling, marking or indicating, not provided for in codes F21W2102/00 – F21W2107/00 for aircraft runways or the like
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F21LIGHTING
    • F21YINDEXING SCHEME ASSOCIATED WITH SUBCLASSES F21K, F21L, F21S and F21V, RELATING TO THE FORM OR THE KIND OF THE LIGHT SOURCES OR OF THE COLOUR OF THE LIGHT EMITTED
    • F21Y2101/00Point-like light sources

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  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Arrangement Of Elements, Cooling, Sealing, Or The Like Of Lighting Devices (AREA)

Abstract

The invention is applicable to the technical field of airport indicator lamps and discloses an airport parking apron light. The airport parking apron light comprises a shell component, a lighting component, an electric control component and a rigid handle. The electric control component comprises a circuit board, the circuit board is connected with a signal receiving antenna used for receiving wireless remote control signals, and the signal receiving antenna extends out of the shell component. The circuit board is provided with a wireless module, and the wireless module is used for controlling the lighting component and is electrically connected with the signal receiving antenna. The rigid handle is connected on the outer side of the shell component through metal fasteners. The airport parking apron light is powered by a battery; by the aid of the signal receiving antenna, operators can operate far away from the parking apron, high safety and reliability are realized; by the aid of the rigid handle, the airport parking apron light is convenient to carry and high in applicability and is applicable to the environment such as the open field without complete supporting facilities.

Description

Airport hardstand lamp
Technical field
The invention belongs to airport indicating lamp technical field, particularly relate to a kind of airport hardstand lamp.
Background technology
In helicopter landing, all need lamplight pointing, can margin line etc. to indicate to pilot and ground crew, for pilot with reference to whether being applicable to landing.
Because helicopter flexibility is strong, landing convenient, it lands when light is bad when field or simple and easy ground, does not have fixing lamplight pointing, be unfavorable for the landing of helicopter because these are local.
Airport hardstand lamp of the prior art, needs the hand-held airport hardstand lamp of ground crew to operate, uses inconvenience.
Summary of the invention
The object of the invention is to overcome above-mentioned the deficiencies in the prior art, provide a kind of airport hardstand lamp, it carries, easy to use.
Technical scheme of the present invention is: a kind of airport hardstand lamp, comprise housing unit, luminescence component, electrically-controlled component and rigid handle, described housing unit has for the automatically controlled chamber of accommodating described luminescence component, described electrically-controlled component and the battery cavities for set battery, and described luminescence component and electrically-controlled component are arranged in described automatically controlled chamber; Described electrically-controlled component comprises circuit board, and described circuit board is connected with the signal receiving antenna for receiving wireless remote control signals, described signal receiving antenna stretches out in described housing unit; Described circuit board is provided with for controlling described luminescence component and the wireless module be electrically connected with described signal receiving antenna; Described rigid handle is connected to the outside of described housing unit by metal buckle.
Alternatively, the sidewall of described housing unit is provided with reinforcement, and described reinforcement is provided with the perforation for passing for described connecting ring, described connecting ring is actively located in described perforation.
Alternatively, described housing unit comprises upper casing, lower casing and bottom, and the upper/lower terminal of described lower casing is set to opening, and described upper casing comprises transmittance section and is connected to the upper end of described lower casing and closes described automatically controlled chamber; Described bottom is connected to the lower end of described lower casing by locking member and closes described battery cavities, and described automatically controlled chamber is positioned at the top of described lower casing, and described battery cavities is positioned at the bottom of described lower casing.
Alternatively, described lower casing is fixedly installed fixed leg, described circuit board offers the through hole be placed on described fixed leg, described luminescence component also comprises aluminium alloy base plate, drive circuit board, main light emission part and indicator lamp, described main light emission part comprises and is arranged at LED illuminating part on described aluminium alloy base plate and infraluminescence part, described drive circuit board is positioned at the below of described aluminium alloy base plate, described indicator lamp is straw hat head indicator lamp and is directly connected in described drive circuit board, described aluminium alloy base plate and described drive circuit board are fixed on the upper end of described post by locking member.
Alternatively, the first O-ring seal is provided with between described upper casing and described lower casing upper end, the second O-ring seal is provided with between described lower casing lower end and described bottom, the lower end of described upper casing or/and the upper end of described lower casing is provided with the first annular groove for holding described first O-ring seal, the bottom of described lower casing or/and described bottom upper end between be provided with the second annular groove for holding described second O-ring seal.
Alternatively, described electrically-controlled component is provided with socket, described main light emission part and indicator lamp are plugged in described socket by the first binding post and the second binding post respectively, be provided with the electric-conductor connected for battery plus-negative plate in described battery cavities, described electric-conductor is plugged in described socket by the 3rd binding post.
Alternatively, be provided with rechargeable battery in described battery cavities, described lower casing or bottom are connected with charging inlet, described charging inlet is connected to described battery or described circuit board by wire.
Alternatively, described lower casing is also connected with the clip for fixing described rechargeable battery, described clip is in " several " font, and the two ends of described clip are connected to described lower casing by connector.
Alternatively, described upper casing or described lower casing are connected with the frequent flashing control switch for controlling described luminescence component flicker frequency and the shift switch for controlling the luminous bright-dark degree of described luminescence component, described frequent flashing control switch and shift switch all lock onto described upper casing or lower casing by locking member, and described frequent flashing control switch and shift switch are connected to described socket respectively by the 4th binding post and the 5th binding post.
Alternatively, described lower casing is connected with the breathing equipment be communicated with described battery cavities.
Airport hardstand lamp provided by the invention; it can adopt powered battery; and by signalization reception antenna; operating personnel can operate away from aircraft gate; security reliability is good, by arranging rigid handle, is convenient to carrying of product; the adaptation of product is good, can be adapted in the incomplete environment of the auxiliary facilities such as field.
Accompanying drawing explanation
Fig. 1 is the solid assembling schematic diagram of the airport hardstand lamp that the embodiment of the present invention provides;
Fig. 2 is another the three-dimensional assembling schematic diagram of the airport hardstand lamp that the embodiment of the present invention provides;
Fig. 3 is the perspective exploded view of the airport hardstand lamp that the embodiment of the present invention provides;
Fig. 4 is the schematic perspective view of luminescence component and Control Component in the airport hardstand lamp that provides of the embodiment of the present invention;
Fig. 5 is the generalized section of the middle breathing equipment of the airport hardstand lamp that the embodiment of the present invention provides.
Detailed description of the invention
In order to make object of the present invention, technical scheme and advantage clearly understand, below in conjunction with drawings and Examples, the present invention is further elaborated.Should be appreciated that specific embodiment described herein only in order to explain the present invention, be not intended to limit the present invention.
As depicted in figs. 1 and 2, a kind of airport hardstand lamp that the embodiment of the present invention that the embodiment of the present invention provides provides, can be applicable to helicopter and shuts down in the wild or shutdown in particular cases, such as, in the special circumstances such as power interruption.
As shown in FIG. 1 to 3, above-mentioned airport hardstand lamp comprises housing unit 1, luminescence component 2, electrically-controlled component 3 and rigid handle 81, housing unit 1 has for the automatically controlled chamber (not marking in figure) of accommodating luminescence component 2, electrically-controlled component 3 and the battery cavities (not shown) for set battery 9, and luminescence component 2 and electrically-controlled component 3 are arranged in automatically controlled chamber; Light fixture is powered by battery 9, can normally use in the wild, in particular cases.Automatically controlled chamber and battery cavities can be split type or integral type.In split type structure, automatically controlled chamber and battery cavities separate, and the heat of the generation such as driving component, luminescence component 2 that amount of sending out in automatically controlled chamber is large can not affect the reliability of battery 9, and product safety performance is good.The hydrogen produced when simultaneously also avoiding battery operated in battery cavities is lighted due to high temperature, and security reliability is high.
As shown in FIG. 1 to 3, electrically-controlled component 3 comprises circuit board 31, and circuit board 31 is connected with the signal receiving antenna 4 for receiving wireless remote control signals, signal receiving antenna 4 stretches out in housing unit 1; Circuit board 31 is provided with for controlling luminescence component 2 and the wireless module be electrically connected with signal receiving antenna 4, the working condition of light fixture can be controlled by supporting Digiplex, ground crew can away from light fixture, security is high, and a people can control to overlap light fixture by remote controller more, applies very convenient.Digiplex can shake control luminescence component 2 glow color, brightness, whether glimmer and flicker frequency etc.
Particularly, described rigid handle 81 is connected to the outside of described housing unit 1 by metal buckle 82, and rigid handle 81 is the ring-type or open arcuation closed, and it is located on the outside of housing unit 1, and rigid handle 81 and housing unit 1 spacing are arranged.In the present embodiment, rigid handle 81 is provided with one, and it can by steel pipe or reinforcing bar one bending and molding, and structural reliability is high.The outside of rigid handle 81 can be arranged with pipe box, and pipe box has the functions such as anti-skidding, anticorrosion.
Particularly, described rigid handle 81 is curved, and described metal buckle 82 is L-shaped, and its one end is by the side of screw lock in described housing unit 1, and the other end is fastened in described rigid handle 81.Metal buckle 82 is fastened in one end of rigid handle 81, is provided with cutting ferrule portion 821, and cutting ferrule portion 821 is curved, and its lower end is provided with opening near housing unit 1 side place, and the caliber being less than rigid handle 81 of the distance of opening.The cutting ferrule portion 821 of metal buckle 82 has certain elasticity; during assembling; easily rigid handle 81 can be snapped in from below the cutting ferrule portion 821 of metal buckle 82; when moving airport hardstand lamp by rigid handle 81; rigid handle 81 can reliably support airport hardstand lamp; structural reliability is high, and the dismounting of rigid handle 81 is very convenient.In the present embodiment, metal buckle 82 is provided with two and lays respectively at the both sides of housing unit 1, simple and reliable for structure.
Particularly, inside housing unit 1 or outside can be connected with for the solar panel charged to the battery 9 in battery cavities or power to luminescence component 2; Solar panel is electrically connected on circuit board 31 or luminescence component 2.By arranging the solar panel being used for solar energy being converted to electric energy, the time of the use of battery can be extended, even if when battery-depletion does not have again rechargeable battery or a new battery altering, solar energy can be relied on to power to luminescence component or charge to battery 9, the adaptation of product is good, can be adapted in the incomplete environment of the auxiliary facilities such as field.And owing to have employed solar panel, extending the working time of luminescence component 2, the maintenance period of light fixture is extended.
Particularly, as shown in FIG. 1 to 3, housing unit 1 comprises upper casing 11, lower casing 12 and bottom 13, and the upper/lower terminal of lower casing 12 is set to opening, and battery 9 can put into the battery cavities of lower casing 12 from the lower end of lower casing 12.Certainly, also the sidewall of lower casing 12 opening can be set with fetching battery 9.
Particularly, as shown in FIG. 1 to 3, upper casing 11 comprises diffuser, and diffuser is connected to the upper end of lower casing 12 and closes automatically controlled chamber; Luminescence component 2 to be positioned on electrically-controlled component 3 direction towards diffuser.Its visible angle is large.Bottom 13 is connected to the lower end of lower casing 12 and closing battery chamber by locking member, and automatically controlled chamber is positioned at the top of lower casing 12, and battery cavities is positioned at the bottom of lower casing 12.
In embody rule, the lower end of bottom 13 or the periphery wall of lower casing 12 can be provided with foot rest (not shown), and foot rest can be triangle corner bracket, to be firmly supported in ground, foot rest lower end can be set to pointed, to insert in soft terrain, is specially adapted to irregular field landform.
Particularly, as shown in Figure 1 to 4, lower casing 12 is fixedly installed fixed leg 121, and fixed leg 121 can be shaped in the automatically controlled chamber of lower casing 12.Circuit board 31 offers the through hole 311 be placed on fixed leg 121, like this, circuit board 31 can directly be placed on fixed leg 121, saves the time that location is aimed at, is convenient to the installation and maintenance of product.Luminescence component 2 also comprises aluminium alloy base plate 21, drive circuit board 22, main light emission part (not shown) and indicator lamp 23, and drive circuit board 22 can be electrically connected on circuit board 31, and drive circuit board 22 is for driving the luminescence etc. of luminescence component 2.Main light emission part comprises and is arranged at LED illuminating part on aluminium alloy base plate 21 and infraluminescence part, and LED illuminating part and infraluminescence part can separately control.When the hidden landing of needs, can open separately infraluminescence part, now helicopter pilot can observe the infrared light of lamp luminescence by relevant device on machine, owing to not having visible ray, therefore reaches hidden object.Normal condition can open visible ray, and helicopter pilot can observe the situation of light intuitively.
Particularly, as shown in Figure 1 to 4, drive circuit board 22 is positioned at the below of aluminium alloy base plate 21, aluminium alloy base plate 21 its adopt aluminum alloy materials to make, its thermal conductivity is good, and the heat produced when LED illuminating part can be worked is discharged fast, makes the operating temperature that LED illuminating part can keep suitable, avoid Yin Wendu too high and cause the LED illuminating part life-span greatly to shorten, product reliability is high.
Particularly, as shown in Figure 1 to 4, indicator lamp 23 is straw hat head indicator lamp and is directly connected in drive circuit board 22, indicator lamp 23, for observing the duty of light fixture, such as, when light fixture breaks down, can coordinate judgement lamp failure, indicator lamp 23 also can be used for the electricity of pilot cell 9, when battery 9 electricity is not enough, corresponding indicator lamp 23 can glimmer or variable color, changes battery 9 in time to provide attendant.
Particularly, as shown in Figure 1 to 4, aluminium alloy base plate 21 and drive circuit board 22 are fixed on the upper end of post by locking member.Drive circuit board 22 and circuit board 31 separate, and avoid both interference mutually, and it are of good reliability to dispel the heat.
Particularly, as shown in Figure 1 to 4, be provided with felt pad 26 between circuit board 31 and lower casing 12, felt pad 26 can be red thick stick paper or rubber cushion etc.
Particularly, packing ring 27 is provided with between circuit board 31 and felt pad 26.
Particularly, as shown in Figure 1 to 4, the first O-ring seal 51 is provided with between upper casing 11 and lower casing 12 upper end, the second O-ring seal 52 is provided with between lower casing 12 lower end and bottom 13, the lower end of upper casing 11 or/and the upper end of lower casing 12 is provided with the first annular groove (not shown) for holding the first O-ring seal 51, the bottom of lower casing 12 or/and bottom 13 upper end between be provided with the second annular groove (not shown) for holding the second O-ring seal 52.
Particularly, as shown in Figure 1 to 4, the first O-ring seal 51 is stuck in the first annular groove, and is subject to the compression of upper casing 11 and lower casing 12, and the first O-ring seal 51 produces certain elastic deformation, makes to keep between upper casing 11 and lower casing 12 sealing, with dustproof and waterproof.Similarly, the second O-ring seal 52 is stuck in the second annular groove, and is subject to the compression of lower casing 12 and bottom 13, and the second O-ring seal 52 produces certain elastic deformation, makes to keep between lower casing 12 and bottom 13 sealing, with dustproof and waterproof.
Particularly, as shown in Figure 1 to 4, the upper end of the first O-ring seal 51 or/and lower end is convexly equipped with the first convex tendon (not shown), the first convex tendon cross section can triangular in shape and drift angle rounding, further enhancing sealing effectiveness.Similarly, the upper end of the second O-ring seal 52 or/and lower end is convexly equipped with the second convex tendon (not shown), the first convex tendon cross section can triangular in shape and drift angle rounding, further enhancing sealing effectiveness.
Particularly, as shown in Figure 1 to 4, electrically-controlled component 3 is provided with for the socket (not shown) that be connected pluggable with terminal, luminescence component 2 comprises main light emission part and indicator lamp 23, main light emission part and indicator lamp 23 are plugged in socket by the first binding post (not shown) and the second binding post (not shown) respectively, main light emission part and indicator lamp 23 are all by modular design, if main light emission part, indicator lamp 23 damages, attendant can immediately by the first binding post, second binding post is extracted from socket, and the main light emission part more renewed, indicator lamp 23, only need by the first binding post, second binding post inserts in socket, without the need to using screwdriver, the aids such as electric iron, improve the assembling of light fixture, maintenance efficiency, helicopter flight safety can be ensured better.
Particularly, as shown in Figure 1 to 4, be provided with the electric-conductor (not shown) connected for battery 9 both positive and negative polarity in battery cavities, electric-conductor is plugged in socket by the 3rd binding post (not shown).When electric-conductor damages, 3rd binding post can be extracted from socket by attendant immediately, and the electric-conductor more renewed, only the 3rd binding post need be inserted in socket, without the need to using the aid such as screwdriver, electric iron, improve the assembling of light fixture, maintenance efficiency, helicopter flight safety can be ensured better
Particularly, as shown in Figure 1 to 4, main light emission part is covered with the lens 25 for realizing secondary light-distribution, to make the brightness of light, angle etc. meet the requirements, lens 25 to be lock onto on aluminium alloy base plate 21 by connector and cover on main light emission part.Connector can be screw etc.
Particularly, as shown in Figure 1 to 4, upper casing 11 comprises diffuser 111 and cover 112.Diffuser 111 is fixedly connected on cover 112, and cover 112 is fixedly connected on the upper end of lower casing 12 by securing member 83.Diffuser 111 can be threaded with cover 112, can be provided with sealing ring between diffuser 111 and cover 112, to improve the sealing effectiveness between diffuser 111 and cover 112.Or, also can be coated with marine glue between diffuser 111 and cover 112, also can reach the effect of water proof and dust proof.Diffuser 111 can adopt the light transmissive materials such as lucite to make.
Particularly, as shown in Figure 1 to 4, the cover 112 of upper casing 11 is provided with the perforation (not shown) for passing for signal receiving antenna 4, circuit board 31 is fixedly connected with, perforation place is arranged with the sealing ring 43 be placed on outside signal receiving antenna 4, the root of signal receiving antenna is locked by nut 44 and is connected to antenna terminal 42, and structural reliability is high.
Particularly, can be covered with protection steel mesh cover (not shown) outside diffuser 111, blown afloat the foreign matters such as stone to avoid diffuser 111 by helicopter and crash, structural reliability is high.
Particularly, be provided with battery in battery cavities, battery can be rechargeable battery, charger can be adopted to charge to rechargeable battery, use very convenient.Certainly, also can be provided with common batteries in battery cavities, its versatility is good, is easy to buying.
Particularly, as shown in FIG. 1 to 3, lower casing 12 or bottom 13 are connected with charging inlet 61, charging inlet 61 is connected to battery 9 or circuit board 31 by wire, charger can be adopted to be plugged in charging inlet 61 pairs of rechargeable batteries and charge.
Particularly, as shown in FIG. 1 to 3, charging inlet 61 place is also provided with the Capsule 611 for shutoff charging inlet 61, with water proof and dust proof.
Particularly, as shown in FIG. 1 to 3, lower casing 12 is also connected with the clip 91 for fixing rechargeable battery, clip 91 is in " several " font, and the two ends of clip 91 are connected to lower casing 12 by connector.Connector can be screw, and to make battery 9 firmly be fixed in the battery cavities of lower casing 12, structural reliability is high.
Particularly, as shown in FIG. 1 to 3, upper casing 11 or lower casing 12 are connected with frequent flashing control switch 71 for controlling luminescence component 2 flicker frequency and the shift switch 72 for the switch that controls luminescence component 2 and luminous bright-dark degree, also can be provided with the color controlling switch (not shown) for controlling luminescence component 2 glow color, frequent flashing control switch 71, shift switch 72 and color controlling switch can be push button or knob etc.When environment exists electromagnetic interference, be difficult to by remote signal control luminescence component 2 luminous time, directly control by frequent flashing control switch 71 and shift switch 72, color controlling switch.Frequent flashing control switch 71, color controlling switch and shift switch 72 all lock onto upper casing 11 or lower casing 12 by locking member, and locking member can be screw.Frequent flashing control switch 71, color controlling switch and shift switch 72 can be arranged side by side.
Particularly, as shown in FIG. 1 to 3, frequent flashing control switch 71 and shift switch 72, color controlling switch are connected to socket respectively by the 4th binding post (not shown) and the 5th binding post (not shown), the 6th binding post (not shown).So that the assembling of product and maintenance.
Particularly, the outside of upper casing 11 or lower casing 12 can be provided with solar panels (not shown), and solar panels can be electrically connected on circuit board 31, is stored in battery 9 solar energy to be converted to chemical energy.
Particularly, as shown in FIG. 1 to 3, between battery 9 and battery cavities, be provided with rubber blanket 92, damage to prevent battery 9.
Particularly, as shown in Fig. 1 ~ Fig. 5, lower casing 12 is connected with the breathing equipment 62 be communicated with battery cavities, in breathing equipment 62, is provided with filter medium 200.Breathing equipment 62 can discharge the hydrogen that battery 9 produces, and to prevent hydrogen from accumulating in battery cavities, has stopped the hidden danger of hydrogen explosion.Or breathing equipment 62 also can be labyrinth type breathing equipment 62.
In the present embodiment, as shown in Fig. 1 ~ Fig. 5, breathing equipment 62 comprises a breathing cylinder 101, and the sidewall of lower casing 12 offers screwed hole, breathes cylinder 101 and can be threaded connection with in screwed hole.Breathe cylinder 101 inner chamber and be equiped with some filter mediums 200 absorbing water dust-proof, breathing equipment 62 also comprises the pressed component 201 that could compress or unclamp filter medium 200, and pressed component 201 is removably connected to be breathed on cylinder 101.By such design, the heat that battery 9 is produced under the duty continued and hydrogen can discharge battery cavities with air by breathing equipment 62 in time; After light fixture quits work, the temperature of battery cavities declines, the Air flow of battery cavities makes volume of air reduce simultaneously, the pressure opposite outer of battery cavities is in negative pressure state, outside air will enter battery cavities by breathing equipment 62, under the suction-operated of filter medium 200, can avoid the steam in air, dust enters battery cavities, battery 9 can be worked under rational humidity environment, be conducive to improving service life.And, can according to different environments for use, can be regulated the elasticity that filter medium 200 compresses easily and reliably by pressed component 201, more clammy or many dirt and environment under or after filter medium 200 uses certain time limit, pressed component 201 pairs of filter mediums 200 can be compressed relatively, reduce the gap between filter medium 200, make steam, dust is difficult to enter battery cavities; Under drier or that air purity is higher environment, pressed component 201 pairs of filter mediums 200 can be unclamped relatively, increase the gap between filter medium 200, be conducive to the heat of battery cavities, hydrogen in time, quickly move through the filter medium 200 stated in breathing equipment 62 and drain into outside, be conducive to the reliability improving product.
Particularly, as shown in Fig. 1 ~ Fig. 5, breathing cylinder 101 also can be shaping with lower casing 12 integrated die-casting, can number of molds be reduced and be conducive to reducing small product size, breathe cylinder 101 one end and offer the first passage 1011 that can be communicated with battery cavities and breathe cylinder 101 inner chamber, battery cavities by first passage 1011 can with ft connection.Additionally, also by welding, bonding, screw locking, buckle connection etc. are fixed, breathing cylinder 101 can be fixedly connected with lower casing 12, all belong to the scope that the present invention protects.
More specifically, as shown in Fig. 1 ~ Fig. 5, pressed component 201 is located at and is breathed cylinder 101 other end, offer one in the middle of pressed component 201 and can be communicated with the second channel 2011 breathing cylinder 101 inner chamber and outside, make battery cavities can with ft connection, be threaded between pressed component 201 with breathing cylinder 101, the elasticity that pressed component 201 pairs of filter mediums 200 compress can be adjusted easily.
Further, as shown in Fig. 1 ~ Fig. 5, breathe in cylinder 101 and be provided with two waterproof ventilative pads 202, filter medium 200 two ends are located at respectively by two pads 202, the appearance and size of pad 202 matches with breathing cylinder 101 cavity shape size, can prevent filter medium 200 from leaking from first passage 1011 and second channel 2011.
Further, as shown in Fig. 1 ~ Fig. 5, breathe between cylinder 101 and pressed component 201 and be also provided with one " O " shape sealing ring 203, improve the sealing property of breathing between cylinder 101 and pressed component 201, prevent rainwater, dust from entering battery cavities from the gap of breathing between cylinder 101 and pressed component 201.
Preferably, as shown in Fig. 1 ~ Fig. 5, filter medium 200 adopts active carbon material manufacture; its water suction anti-dust performance is good, the reliability of product is improved, additionally; filter medium 200 also can adopt the suitable material manufactures such as quartz sand, all belongs to protection scope of the present invention.
Preferably, the employing felt materials of pad 202 manufactures, the good and low price of its water proof and dust proof performance; be conducive to the cost reducing product; additionally, pad 202 also can adopt the material manufactures such as active carbon particle packing ring, non-woven fabrics, all belongs to protection scope of the present invention.
Preferably, sealing ring 203 adopts elastomeric material manufacture, the good and low price of its ability of elastic-plastic deformation, makes can reliably seal between breathing cylinder 101 and pressed component 201 and can reduce the cost of product.
After the certain time limit of use, filter medium 200 will lose efficacy, when filter medium 200 changed by needs, only need pressed component 201 is screwed out and takes out a pad 202, then new filter medium 200 is again loaded again after removing failed filter medium 200, again the pad 202 of taking-up is put into and breathe cylinder 101, finally pressed component 201 is screwed in and breathe cylinder 101.Maintenance process is convenient, does not need light fixture to pull down from lamppost, and does not need the parts scrapping other, only need refill active carbon particle, is conducive to the maintenance, the use cost that reduce user.
Airport hardstand lamp provided by the invention, be convenient to set up the airplane parking area that can supply helicopter landing fast, it can adopt powered battery, and by signalization reception antenna 4, operating personnel can wireless remote control airport hardstand lamp, remote control distance is far away, easy to use and security reliability is good for arranging the solar panel being used for solar energy being converted to electric energy, the time of the use of battery can be extended, even if when battery-depletion does not have again rechargeable battery or a new battery altering, solar energy can be relied on to power to luminescence component or charge to battery 9, the adaptation of product is good, can be adapted in the incomplete environment of the auxiliary facilities such as field.
And; airport hardstand lamp provided by the invention; main light emission part is all be connected with socket by binding post with the connection of parts such as indicator lamp 23 grade; not only efficiency of assembling is high for it; and also easily change after parts damages, do not need to use the instrument such as screwdriver, electric iron, operation is simple; normal operating condition can be recovered by quick-replaceable corresponding component after damage of product, be more conducive to ensure helicopter landing safety.
By arranging infrared illuminants, need can see by infrared identification equipment, add the crypticity of airplane parking area, security reliability is able to further raising.
These are only preferred embodiment of the present invention, not in order to limit the present invention, all any amendments done within the spirit and principles in the present invention, equivalent replacement or improvement etc., all should be included within protection scope of the present invention.

Claims (10)

1. an airport hardstand lamp, it is characterized in that, comprise housing unit, luminescence component, electrically-controlled component and rigid handle, described housing unit has for the automatically controlled chamber of accommodating described luminescence component, described electrically-controlled component and the battery cavities for set battery, and described luminescence component and electrically-controlled component are arranged in described automatically controlled chamber;
Described electrically-controlled component comprises circuit board, and described circuit board is connected with the signal receiving antenna for receiving wireless remote control signals, described signal receiving antenna stretches out in described housing unit; Described circuit board is provided with for controlling described luminescence component and the wireless module be electrically connected with described signal receiving antenna;
Described rigid handle is connected to the outside of described housing unit by metal buckle.
2. airport hardstand lamp as claimed in claim 1, it is characterized in that, described rigid handle is curved, and described metal buckle is L-shaped, and its one end lock onto the side of described housing unit, and the other end is fastened in described rigid handle.
3. airport hardstand lamp as claimed in claim 1, it is characterized in that, described housing unit comprises upper casing, lower casing and bottom, and the upper/lower terminal of described lower casing is set to opening, and described upper casing comprises transmittance section and is connected to the upper end of described lower casing and closes described automatically controlled chamber; Described bottom is connected to the lower end of described lower casing by locking member and closes described battery cavities, and described automatically controlled chamber is positioned at the top of described lower casing, and described battery cavities is positioned at the bottom of described lower casing.
4. airport hardstand lamp as claimed in claim 3, it is characterized in that, described lower casing is fixedly installed fixed leg, described circuit board offers the through hole be placed on described fixed leg, described luminescence component also comprises aluminium alloy base plate, drive circuit board, main light emission part and indicator lamp, described main light emission part comprises and is arranged at LED illuminating part on described aluminium alloy base plate and infraluminescence part, described drive circuit board is positioned at the below of described aluminium alloy base plate, described indicator lamp is straw hat head indicator lamp and is directly connected in described drive circuit board, described aluminium alloy base plate and described drive circuit board are fixed on the upper end of described post by locking member.
5. airport hardstand lamp as claimed in claim 3; it is characterized in that; the first O-ring seal is provided with between described upper casing and described lower casing upper end; the second O-ring seal is provided with between described lower casing lower end and described bottom; the lower end of described upper casing or/and the upper end of described lower casing is provided with the first annular groove for holding described first O-ring seal, the bottom of described lower casing or/and described bottom upper end between be provided with the second annular groove for holding described second O-ring seal.
6. airport hardstand lamp as claimed in claim 3; it is characterized in that; described electrically-controlled component is provided with socket; described main light emission part and indicator lamp are plugged in described socket by the first binding post and the second binding post respectively; be provided with the electric-conductor connected for battery plus-negative plate in described battery cavities, described electric-conductor is plugged in described socket by the 3rd binding post.
7. airport hardstand lamp as claimed in claim 3, it is characterized in that, be provided with rechargeable battery in described battery cavities, described lower casing or bottom are connected with charging inlet, described charging inlet is connected to described battery or described circuit board by wire.
8. airport hardstand lamp as claimed in claim 7, is characterized in that, described lower casing being also connected with the clip for fixing described rechargeable battery, and described clip is in " several " font, and the two ends of described clip are connected to described lower casing by connector.
9. the airport hardstand lamp according to any one of claim 3 to 8; it is characterized in that; described upper casing or described lower casing are connected with the frequent flashing control switch for controlling described luminescence component flicker frequency and the shift switch for controlling the luminous bright-dark degree of described luminescence component; described frequent flashing control switch and shift switch all lock onto described upper casing or lower casing by locking member, and described frequent flashing control switch and shift switch are connected to described socket respectively by the 4th binding post and the 5th binding post.
10. the airport hardstand lamp according to any one of claim 3 to 8, is characterized in that, described lower casing is connected with the breathing equipment be communicated with described battery cavities.
CN201310393389.6A 2013-09-02 2013-09-02 Airport parking apron light Pending CN104421812A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201310393389.6A CN104421812A (en) 2013-09-02 2013-09-02 Airport parking apron light

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201310393389.6A CN104421812A (en) 2013-09-02 2013-09-02 Airport parking apron light

Publications (1)

Publication Number Publication Date
CN104421812A true CN104421812A (en) 2015-03-18

Family

ID=52971560

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201310393389.6A Pending CN104421812A (en) 2013-09-02 2013-09-02 Airport parking apron light

Country Status (1)

Country Link
CN (1) CN104421812A (en)

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Application publication date: 20150318