CN104071350B - Helicopter field landing indicator lamp - Google Patents
Helicopter field landing indicator lamp Download PDFInfo
- Publication number
- CN104071350B CN104071350B CN201310106325.3A CN201310106325A CN104071350B CN 104071350 B CN104071350 B CN 104071350B CN 201310106325 A CN201310106325 A CN 201310106325A CN 104071350 B CN104071350 B CN 104071350B
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- Prior art keywords
- indicator lamp
- housing
- battery
- control circuit
- helicopter
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- Illuminated Signs And Luminous Advertising (AREA)
Abstract
A kind of helicopter field landing indicator lamp, including housing, luminescence component, control circuit plate, reception antenna and transparent upper cover.After loading onto battery, luminescence component can be luminous under the control of control circuit plate.Wherein, owing to reception antenna can receive remote signal, and by antenna terminal, described remote signal is sent to control circuit plate, it is luminous that control circuit buttress controls described luminescence component according to institute's remote signal, therefore above-mentioned helicopter field landing indicator lamp remotely can be controlled by operating personnel in the place away from landing place, thus it is constantly in landing place without operating personnel when indicating helicopter landing.Therefore, above-mentioned helicopter field landing indicator lamp can effectively avoid helicopter to damage operating personnel when landing, eliminates potential safety hazard.
Description
Technical field
The present invention relates to portable lighting technology, particularly relate to a kind of helicopter field landing indicator lamp.
Background technology
The advantages such as helicopter is strong with its flexibility, landing is convenient, are widely used to speedily carry out rescue work, transport, promptly
The fields such as assistance.What due to the specific demand to helicopter, therefore need to go straight up to function environment, Ren Heshi in office
Between land.
When helicopter needs land in the wild night, owing to not having cue mark, and surface state is unintelligible,
May result in helicopter landing difficulty.The most general way is in previously selected landing by ground staff
Position hand-hold lamp fitting makes marks.But, ground staff needs to be in all the time during instruction helicopter landing
In helicopter depression area, when there is deviation in helicopter landing, it is possible to operating personnel are damaged,
There is potential safety hazard.
Summary of the invention
Based on this, it is necessary to provide a kind of be prevented effectively from personnel are damaged helicopter field landing refer to
Show lamp.
A kind of helicopter field landing indicator lamp, including:
Housing, for the tubular structure of hollow, one end of described housing offers light-emitting window, in described housing also
It is provided with battery container chamber；
Luminescence component, houses and is fixed in described housing, goes out described in the exiting surface sensing of described luminescence component
Light mouth, described luminescence component includes infrared emitter and VISIBLE LIGHT EMISSION body；
Control circuit plate, houses and is fixed in described housing, described control circuit plate and described luminescence component
Electrical connection, is used for controlling described luminescence component luminous, described control circuit plate is additionally provided with antenna terminal；
Reception antenna, electrically connects with described antenna terminal, and described reception antenna can receive remote signal, and leads to
Cross described antenna terminal and described remote signal is sent to described control circuit plate, described control circuit buttress evidence
It is luminous that described remote signal controls described luminescence component, and described reception antenna includes the most sheathed multiple sleeve pipe,
So that described reception antenna is scalable；And
Transparent upper cover, is fixed on described housing and covers described light-emitting window.
Wherein in an embodiment, one end that described housing is relative with described light-emitting window is further opened with battery hole,
Described battery hole connects with described battery container chamber, can realize battery taking and placing by described battery hole, described directly
Rise machine field landing indicator lamp and also include that bottom, described bottom are fixed on described housing and cover described battery hole.
Wherein in an embodiment, described transparent upper cover offers the first ring near one end of described light-emitting window
Shape groove, the edge of described battery hole has the second cannelure, described helicopter field landing indicator lamp also to wrap
Include:
First sealing ring, is contained in described first annular groove and is held on described transparent upper cover and described housing
Between；
Second sealing ring, is contained in described second cannelure and is held between described housing and described bottom.
Wherein in an embodiment, also include that lens, described lens house and are fixed in described housing,
Described lens between described luminescence component and described transparent upper cover, the light that described luminescence component can be sent
Line carries out luminous intensity distribution.
Wherein in an embodiment, described housing is provided with:
Stroboscopic switchs, and is arranged at the sidewall of described housing and electrically connects with described control circuit plate, described stroboscopic
Switch is for controlling the switching of described infrared emitter；
Shift switch, is arranged at the sidewall of described housing and electrically connects with described control circuit plate, described gearshift
Switch lights degree for control described VISIBLE LIGHT EMISSION body.
Wherein in an embodiment, described transparent upper cover includes:
Lid, it offers through hole, and the inwall of described through hole is provided with internal thread, and described lid passes through screw
It is fixed on described housing；
Translucent cover, for the cup-like structure of one end open, the edge of its openend is provided with external screw thread, described outside
Screw thread and described screw-internal thread fit, to be installed on described lid by described translucent cover.
Wherein in an embodiment, also include battery, described battery container in described battery container chamber also
Electrically connecting with described control circuit plate, described battery can be the landing indicator lamp energy supply of described helicopter field.
Wherein in an embodiment, being provided with battery clip in described battery container chamber, described Battery Card is held in
In described battery clip.
Wherein in an embodiment, described battery is secondary cell, and the sidewall of described housing is provided with charging
Mouthful, by described charging inlet, described battery can be charged.
Wherein in an embodiment, also include that respirator, described respirator are arranged in the sidewall of described housing,
So that described housing and external UNICOM, described respirator is discharged for the hydrogen produced by described battery.
Compared with the mode of tradition instruction helicopter landing, above-mentioned helicopter field landing indicator lamp has at least
Advantages below:
1, remote signal can be received due to reception antenna, and be sent to control by remote signal by antenna terminal
Circuit board, it is luminous that control circuit buttress controls luminescence component according to remote signal, therefore operating personnel can be away from fall
Above-mentioned helicopter field landing indicator lamp is remotely controlled by the place that dropping place is put, thus without operating personnel
It is constantly in landing place when indicating helicopter landing.Therefore, above-mentioned helicopter field landing indicator lamp energy
Helicopter is effectively avoided when landing, operating personnel to be damaged；
2, reception antenna includes the most sheathed multiple sleeve pipe, so that reception antenna is scalable.Work as operating personnel
When distance landing place is too remote, reception antenna can be stretched out, to increase the area receiving signal, thus improve
The receiving efficiency of reception antenna.Additionally, when transport, reception antenna can be retracted, to reduce volume, and
Avoid fractureing reception antenna in transportation；
3, infrared light needs to be equipped with specific equipment and just can observe, thus can avoid stating helicopter field landing
Indicator lamp is found by other people.Additionally, luminescence component and control circuit plate are contained in by housing and transparent upper cover
Assemble in the host cavity formed so that the landing of above-mentioned helicopter field indicating lamp structure is compact, volume relatively
Little, it is difficult in the wild be found.Therefore, above-mentioned helicopter field landing indicator lamp effectively raises hidden
Property.
Accompanying drawing explanation
Fig. 1 is the structural representation of helicopter field landing indicator lamp in present pre-ferred embodiments；
Fig. 2 is the assembling figure of the landing indicator lamp of helicopter field shown in Fig. 1.
Detailed description of the invention
For the ease of understanding the present invention, below with reference to relevant drawings, the present invention is described more fully.
Accompanying drawing gives presently preferred embodiments of the present invention.But, the present invention can come real in many different forms
Existing, however it is not limited to embodiment described herein.On the contrary, providing the purpose of these embodiments is to make this
The understanding of disclosure of the invention content is more thorough comprehensively.
It should be noted that when element is referred to as " being fixed on " another element, and it can be directly at another yuan
On part or element placed in the middle can also be there is.When an element is considered as " connection " another element, and it can
To be directly to another element or to may be simultaneously present centering elements.
Unless otherwise defined, all of technology used herein and scientific terminology and the technology belonging to the present invention
The implication that the technical staff in field is generally understood that is identical.The art used the most in the description of the invention
Language is intended merely to describe the purpose of specific embodiment, it is not intended that in limiting the present invention.Used herein
Term " and/or " include the arbitrary and all of combination of one or more relevant Listed Items.
Referring to Fig. 1 and Fig. 2, in present pre-ferred embodiments, helicopter field landing indicator lamp 100 includes shell
Body 110, luminescence component 120, control circuit plate 130, reception antenna 140, transparent upper cover 150, bottom
160, lens 170 and battery 180.
Housing 110 is the tubular structure of hollow.The shape of housing 110 can be rounded cylindrical, rectangular drum like etc.,
Can be made up of the material that metal material or other mechanical strengths are high.The one end open of housing 110, this opening is
Light-emitting window 111, light can be by light-emitting window 111 outgoing.Battery container chamber (not shown) it is additionally provided with in housing 110.
Concrete, battery container chamber is positioned at housing 110 one end away from light-emitting window 111, and battery container chamber is used for housing
Battery for helicopter field landing indicator lamp 100 energy supply.
In the present embodiment, one end that housing 110 is relative with light-emitting window 111 is further opened with battery hole 113, electricity
Hole, pond 113 connects with battery container chamber.When battery needs to change, just electricity can be realized by battery hole 113
Pond picks and places.Bottom 160 is fixed on housing 110 and covers battery hole 113, thus is closed in battery container chamber.
Concrete, bottom 160 is detachably secured on housing 110 by screw.Further, bottom 160
For rectangular plate-like, its bottom flat.Therefore, helicopter field landing indicator lamp 100 can be made directly to stand on ground
Face and need not adopt and be fixed in other ways, thus convenient it is dismounted, improves helicopter field
The mobility of landing indicator lamp 100.
It is pointed out that in other embodiments, one end that housing 110 is relative with light-emitting window 111 can be envelope
Closed end, omits bottom 160 simultaneously.When battery needs to change, light-emitting window 111 fetching battery can be passed through.
In the present embodiment, in battery container chamber, it is provided with battery clip 112, when battery container is in battery container chamber
Time interior, battery clip 112 is for clamping battery, thus is fixed by battery.It is pointed out that at other
In embodiment, battery clip 112 can be replaced by draw-in groove, thread gluing etc..
In the present embodiment, housing 110 being additionally provided with respirator 114, respirator 114 is arranged in housing 110
Sidewall so that housing 110 and external UNICOM.Respirator 114 is discharged for the hydrogen produced by battery.
It is therefore possible to prevent hydrogen accumulates within the case 110, thus avoid helicopter field landing indicator lamp 100
Raw blast.
Luminescence component 120 houses and is fixed in housing 110, and the exiting surface of luminescence component 120 points to out
Light mouth 111.Luminescence component 120 includes substrate 121 and the illuminator 123 being fixed on substrate 121, substrate
The inwall of housing 110 it is fixed on by modes such as screw threads for fastening.Illuminator 123 includes infrared emitter (figure
Do not mark) and multiple light emitter (figure is not marked).Wherein, infrared emitter sends infrared ray, and infrared ray exists
Helicopter descent plays indicative function.And just can observe owing to infrared ray needs to be equipped with specific equipment.
Therefore, utilize infrared ray to carry out instruction and can prevent the landing place of helicopter from exposing, thus improve disguise.
VISIBLE LIGHT EMISSION body is used for sending visible ray, such as infrared and gold-tinted, it is seen that light can be that helicopter provides illumination.
Control circuit plate 130 houses and is fixed in housing 110.Control circuit plate 130 and luminescence component 120
Electrical connection, is used for controlling luminescence component 120 luminous.Additionally, when housing 110 is metal, control circuit
Plate 130 need to insulate with housing 110.Concrete, between control circuit plate 130 and housing 110, pad sets one layer
Red thick stick paper (figure is not marked).Control circuit plate 130 can control luminescence component 120 middle infrared (Mid-IR) emitter logical,
Disconnected, and the luminous degree (number being lit in the most multiple visible light emitters) of visible light emitters.This
Outward, control circuit plate 130 being additionally provided with status indicator lamp 131, control circuit plate 130 is according to luminescence component
The luminance state of a control indicator lamp 131 of 120, so that status indicator lamp 131 demonstrates that helicopter field drops
Fall the duty of indicator lamp 100.
Control circuit plate 130 is provided with antenna terminal 133, and reception antenna 140 electrically connects with antenna terminal 133.
Reception antenna 140 can receive remote signal, and is sent to control electricity by remote signal by antenna terminal 133
Road plate 130, it is luminous that control circuit plate 130 controls luminescence component 120 according to remote signal.Pass through reception antenna
140, helicopter field landing indicator lamp 100 can be realized remotely controlling by operating personnel.Operating personnel can be prior
The indicator lamp 100 that landed by helicopter field is positioned over somewhere, is the most remotely controlled when helicopter is to be landed to go straight up to
Machine field landing indicator lamp 100 works.Therefore, operation operating personnel away from landing place, thus can prevent
Operating personnel are damaged in descent by helicopter, eliminate potential safety hazard.
Additionally, reception antenna 140 includes the most sheathed multiple sleeve pipe 141.Multiple sleeve pipes 141 are the most sheathed,
Form Telescopic rod structure, so that reception antenna 140 is scalable.When operating personnel distance landing place too
Time remote, reception antenna 140 can be stretched out, to increase the area receiving signal, thus improve reception antenna 140
Receiving efficiency.Additionally, when transport, reception antenna 140 can be retracted, to reduce volume, and avoid
Fracture in transportation reception antenna 140.
In the present embodiment, housing 110 is provided with stroboscopic switch 115 and shift switch 117.Wherein:
Stroboscopic switch 115 is arranged at the sidewall of housing 110 and electrically connects with control circuit plate 130.Concrete,
Stroboscopic switch 115 is provided with "off", the gear of " connection ".Operating personnel can be as required at two gears
Between switch over.Control circuit plate 130 just can control infrared ray according to the gear stages of stroboscopic switch 115
The switching of emitter.
Shift switch 117 is arranged at the sidewall of housing 110 and electrically connects with control circuit plate 130, and gearshift is opened
Close 117 and light degree for control VISIBLE LIGHT EMISSION body.Concrete, shift switch 117 is provided with multiple
Gear, such as 20%, 40%, 60%, 80% and 100%.When shift switch 117 lays respectively at above-mentioned gear
Time, control circuit plate 130 control successively 20% in multiple visible light emitters, 40%, 60%, 80% and
The most luminous.When environment exists electromagnetic interference, it is difficult to when controlling luminescence component 120 luminescence by remote signal,
The work of helicopter field landing indicator lamp 100 can be directly controlled by stroboscopic switch 115 and shift switch 117
Make state.
Transparent upper cover 150 is fixed on housing 110 and covers light-emitting window 111.The most in the present embodiment, transparent
Upper cover 150 is removably connected with housing 110 by screw, thus when needing the electronics unit in housing 110
When part is safeguarded, transparent upper cover 150 can be taken off.Transparent upper cover 150 can have polyester material, glass,
The transparent materials such as plastics are made so that transparent upper cover 150 transparent go out light.Transparent upper cover 150 and the end
Lid 160 cooperation, seals housing 110, thus the electronic component housed in protective housing 110.
The most in the present embodiment, transparent upper cover 150 includes lid 151 and translucent cover 153.Reception antenna
140 are arranged on lid 151.Further, in the present embodiment, reception antenna 140 is arranged with rubber
Circle 143.Rubber ring 143 is held between reception antenna 140 and transparent upper cover 150, so that receive sky
Line 140 contacts with transparent upper cover 150 closely, improves the sealing of helicopter field landing indicator lamp 100.
It is pointed out that in other embodiments, the mode of welding also can be used to be fixed on by reception antenna 140
On transparent upper cover 150, thus avoid there is gap between reception antenna 140 and transparent upper cover 150.
Lid 151 is fixed on housing 110 by screw.Lid 151 offers through hole (figure is not marked), logical
The inwall in hole is provided with interior spiral shell.Translucent cover 153 is the cup-like structure of one end open, translucent cover 153 openend
Edge is provided with external screw thread.External screw thread and screw-internal thread fit, to be installed on lid 151 by translucent cover 153.Cause
This, is when needing the electronic component in housing 110 is safeguarded, only need to be by translucent cover 153 from lid 151
Upper back-out, screw, without repeatedly twisting the operation of screw, thus improve maintenance efficiency.
In the present embodiment, transparent upper cover 150 offers first annular groove (figure near one end of light-emitting window 111
Do not show), the edge of battery hole 113 has the second cannelure (not shown).Helicopter field landing instruction
Lamp 100 also includes the first sealing ring 190A and the second sealing ring 190B.Wherein:
First sealing ring 190A be contained in first annular groove and be held on transparent upper cover 150 and housing 110 it
Between, closely leave no gaps so that contact between transparent upper cover 150 with housing 110.Second sealing ring 190B
Be contained in the second cannelure and be held between housing 110 and bottom 160 so that housing 110 with
Between bottom 160, contact is closely.Therefore, the first sealing ring 190A and the second sealing ring 190B carries further
High helicopter field landing indicator lamp 100 sealing property, thus preferably protect its inner member, and then
Improve quality and the service life of helicopter field landing indicator lamp 100.
Lens 170 house and are fixed in housing 110.The shape of lens 161 and the shape of housing 110 opening
Shape is consistent.Lens 170, can be to luminescence component 120 between luminescence component 120 and transparent upper cover 150
The light sent carries out luminous intensity distribution.After lens 170 luminous intensity distribution, the light that luminescence component 120 can be made to send goes out
Optic angle is big, light distribution is more uniform, thus promotes instruction and the photograph of helicopter field landing indicator lamp 100
Obvious results fruit.It is pointed out that in other embodiments, lens 170 also can omit.
Electrically connect in battery 180 is contained in battery container chamber and with control circuit plate 130. specifically at the present embodiment
In, battery 180 is fastened in battery clip 112, thus is fixed in housing 110.Battery 180 can be to go straight up to
Landing indicator lamp 100 energy supply of machine field.It is pointed out that in other embodiments, battery 180 can save
Slightly.Before helicopter field landing indicator lamp 100 uses, battery is encased in battery container chamber.
In the present embodiment, battery 180 is secondary cell, and the sidewall of housing 110 is provided with charging inlet 119.
Charging inlet 119 electrically connects with control circuit plate 130, and control circuit plate 130 can convert electrical energy into battery
The chemical energy of 180 stores.Therefore, by charging inlet 119, battery 180 can be charged.Need
It is noted that in other embodiments, battery 180 can be also dry cell.Can lead to after dry cell electric discharge completely
Cross battery hole 113 to be replaced, without arranging charging inlet 119 on housing 110.
Helicopter field landing indicator lamp 100 has an at least advantages below:
1, remote signal can be received due to reception antenna 140, and by antenna terminal 133, remote signal be passed
Delivering to control circuit plate 130, it is luminous that control circuit plate 130 controls luminescence component 120 according to remote signal, therefore
Above-mentioned helicopter field landing indicator lamp 100 can be carried out remotely by operating personnel in the place away from landing place
Control, thus be constantly in landing place without operating personnel when indicating helicopter landing.Therefore, go straight up to
Machine field landing indicator lamp 100 can effectively avoid helicopter to damage operating personnel when landing；
2, reception antenna 140 includes the most sheathed multiple sleeve pipe 141, so that reception antenna 140 is scalable.
When operating personnel's distance landing place is too remote, reception antenna 140 can be stretched out, receive signal to increase
Area, thus improve the receiving efficiency of reception antenna 140.Additionally, when transport, can be by reception antenna 140
Retract, to reduce volume, and avoid the reception antenna 140 that fractures in transportation；
3, infrared light needs to be equipped with specific equipment and just can observe, thus can avoid stating helicopter field landing
Indicator lamp 100 is found by other people.Additionally, luminescence component 120 and control circuit plate 130 are contained in by shell
Body 110 assembles in the host cavity formed with transparent upper cover 150, so that helicopter field landing indicator lamp
100 compact conformations, small volume, be difficult to be found in the wild.Therefore, helicopter field landing indicator lamp
100 effectively raise disguise.
Embodiment described above only have expressed the several embodiments of the present invention, and it describes more concrete and detailed,
But therefore can not be interpreted as the restriction to the scope of the claims of the present invention.It should be pointed out that, for this area
Those of ordinary skill for, without departing from the inventive concept of the premise, it is also possible to make some deformation and
Improving, these broadly fall into protection scope of the present invention.Therefore, the protection domain of patent of the present invention should be with appended
Claim is as the criterion.
Claims (9)
1. a helicopter field landing indicator lamp, including:
Housing, for the tubular structure of hollow, one end of described housing offers light-emitting window, in described housing also
It is provided with battery container chamber；
Luminescence component, houses and is fixed in described housing, goes out described in the exiting surface sensing of described luminescence component
Light mouth, described luminescence component includes infrared emitter and VISIBLE LIGHT EMISSION body；
Control circuit plate, houses and is fixed in described housing, described control circuit plate and described luminescence component
Electrical connection, is used for controlling described luminescence component luminous, described control circuit plate is additionally provided with antenna terminal；
Reception antenna, electrically connects with described antenna terminal, and described reception antenna can receive remote signal, and leads to
Cross described antenna terminal and described remote signal is sent to described control circuit plate, described control circuit buttress evidence
It is luminous that described remote signal controls described luminescence component, and described reception antenna includes the most sheathed multiple sleeve pipe,
So that described reception antenna is scalable；And
Transparent upper cover, is fixed on described housing and covers described light-emitting window；
It is characterized in that, described housing is provided with:
Stroboscopic switchs, and is arranged at the sidewall of described housing and electrically connects with described control circuit plate, described stroboscopic
Switch is for controlling the switching of described infrared emitter；
Shift switch, is arranged at the sidewall of described housing and electrically connects with described control circuit plate, described gearshift
Switch lights degree for control described VISIBLE LIGHT EMISSION body.
Helicopter field the most according to claim 1 landing indicator lamp, it is characterised in that described housing
One end relative with described light-emitting window is further opened with battery hole, and described battery hole connects with described battery container chamber,
Can realize battery taking and placing by described battery hole, described helicopter field landing indicator lamp also includes bottom, institute
State bottom be fixed on described housing and cover described battery hole.
Helicopter field the most according to claim 2 landing indicator lamp, it is characterised in that described transparent
Upper cover offers first annular groove near one end of described light-emitting window, and the edge of described battery hole has second
Cannelure, described helicopter field landing indicator lamp also includes:
First sealing ring, is contained in described first annular groove and is held on described transparent upper cover and described housing
Between；
Second sealing ring, is contained in described second cannelure and is held between described housing and described bottom.
Helicopter field the most according to claim 1 landing indicator lamp, it is characterised in that also include
Mirror, described lens house and are fixed in described housing, and described lens are positioned at described luminescence component with described
Between bright upper cover, the light that can send described luminescence component carries out luminous intensity distribution.
Helicopter field the most according to claim 1 landing indicator lamp, it is characterised in that described transparent
Upper cover includes:
Lid, it offers through hole, and the inwall of described through hole is provided with internal thread, and described lid passes through screw
It is fixed on described housing；
Translucent cover, for the cup-like structure of one end open, the edge of its openend is provided with external screw thread, described outside
Screw thread and described screw-internal thread fit, to be installed on described lid by described translucent cover.
Helicopter field the most according to claim 1 landing indicator lamp, it is characterised in that also include electricity
Pond, described battery container electrically connects in described battery container chamber and with described control circuit plate, described battery
It can be the landing indicator lamp energy supply of described helicopter field.
Helicopter field the most according to claim 6 landing indicator lamp, it is characterised in that described battery
Being provided with battery clip in host cavity, described Battery Card is held in described battery clip.
Helicopter field the most according to claim 6 landing indicator lamp, it is characterised in that described battery
For secondary cell, the sidewall of described housing is provided with charging inlet, can be by described charging inlet to described battery
It is charged.
Helicopter field the most according to claim 6 landing indicator lamp, it is characterised in that also include exhaling
Haustorium, described respirator is arranged in the sidewall of described housing so that described housing and extraneous UNICOM, described in exhale
Haustorium is discharged for the hydrogen produced by described battery.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201310106325.3A CN104071350B (en) | 2013-03-28 | 2013-03-28 | Helicopter field landing indicator lamp |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201310106325.3A CN104071350B (en) | 2013-03-28 | 2013-03-28 | Helicopter field landing indicator lamp |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN104071350A CN104071350A (en) | 2014-10-01 |
| CN104071350B true CN104071350B (en) | 2016-09-07 |
Family
ID=51593033
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201310106325.3A Expired - Fee Related CN104071350B (en) | 2013-03-28 | 2013-03-28 | Helicopter field landing indicator lamp |
Country Status (1)
| Country | Link |
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| CN (1) | CN104071350B (en) |
Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN1337542A (en) * | 2000-08-04 | 2002-02-27 | 东芝照明技术株式会社 | Marker lamp system |
| EP1140626B1 (en) * | 1998-12-21 | 2003-03-05 | AlliedSignal Inc. | Ir diode based high intensity light |
| US6567248B1 (en) * | 2002-02-01 | 2003-05-20 | Ronald M. Schmidt | Tri-spectrum aircraft landing light |
| CN102666281A (en) * | 2009-09-30 | 2012-09-12 | Adb有限责任公司 | Lighting unit for lighting airfields |
| CN202769445U (en) * | 2011-09-26 | 2013-03-06 | 东芝照明技术株式会社 | Aviation identification lamp |
-
2013
- 2013-03-28 CN CN201310106325.3A patent/CN104071350B/en not_active Expired - Fee Related
Patent Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| EP1140626B1 (en) * | 1998-12-21 | 2003-03-05 | AlliedSignal Inc. | Ir diode based high intensity light |
| CN1337542A (en) * | 2000-08-04 | 2002-02-27 | 东芝照明技术株式会社 | Marker lamp system |
| US6567248B1 (en) * | 2002-02-01 | 2003-05-20 | Ronald M. Schmidt | Tri-spectrum aircraft landing light |
| CN102666281A (en) * | 2009-09-30 | 2012-09-12 | Adb有限责任公司 | Lighting unit for lighting airfields |
| CN202769445U (en) * | 2011-09-26 | 2013-03-06 | 东芝照明技术株式会社 | Aviation identification lamp |
Also Published As
| Publication number | Publication date |
|---|---|
| CN104071350A (en) | 2014-10-01 |
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Granted publication date: 20160907 Termination date: 20190328 |