CN104071344B - Helicopter field landing indicator lamp - Google Patents
Helicopter field landing indicator lamp Download PDFInfo
- Publication number
- CN104071344B CN104071344B CN201310106341.2A CN201310106341A CN104071344B CN 104071344 B CN104071344 B CN 104071344B CN 201310106341 A CN201310106341 A CN 201310106341A CN 104071344 B CN104071344 B CN 104071344B
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- China
- Prior art keywords
- indicator lamp
- housing
- landing indicator
- helicopter field
- control circuit
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- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T50/00—Aeronautics or air transport
- Y02T50/50—On board measures aiming to increase energy efficiency
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- Arrangement Of Elements, Cooling, Sealing, Or The Like Of Lighting Devices (AREA)
Abstract
A kind of helicopter field landing indicator lamp, comprises housing, luminescence component, control circuit board and transparent upper cover. Load onto after battery, luminescence component can be luminous under the control of control circuit board. Wherein, the light that VISIBLE LIGHT EMISSION body sends is for illumination, and the infrared light that infrared emitter sends is used to indicate position. Just can observe because infrared light need to be equipped with specific equipment, be found by other people thereby can avoid stating helicopter field landing indicator lamp. In addition, luminescence component and control circuit board are contained in by housing and transparent upper cover and assemble in the host cavity forming, thereby make above-mentioned helicopter field landing indicating lamp structure compactness, small volume, are difficult for being in the wild found. Therefore, above-mentioned helicopter field landing indicator lamp effectively raises disguise.
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, have been widely used in speedily carrying out rescue work, have transported, promptlyThe fields such as assistance. Due to the specific demand to helicopter, therefore need to go straight up to function what environment in office, Ren HeshiBetween landing.
In the time that helicopter needs land night in the wild, owing to there is no cue mark, and surface state is unintelligible,May cause helicopter landing difficulty. General way is in previously selected landing by ground staff at presentPosition hand-hold lamp fitting makes marks. But, because people's target is larger, thereby easily expose the landing of helicopterPosition.
Summary of the invention
Based on this, be necessary to provide one can improve concealed helicopter field landing indicator lamp.
A kind of helicopter field landing indicator lamp, comprising:
Housing, is the tubular structure of hollow, and one end of described housing offers light-emitting window, in described housing, goes backBe provided with battery container chamber;
Luminescence component, accommodates and is fixed in described housing, described in the exiting surface of described luminescence component points to, goes outLight mouth, described luminescence component comprises infrared emitter and VISIBLE LIGHT EMISSION body;
Control circuit board, accommodates and is fixed in described housing, described control circuit board and with described luminous groupPart electrical connection, luminous for controlling described luminescence component;
Transparent upper cover, is fixed on described housing and covers described light-emitting window; And
Solar panels, are attached at the inwall of described transparent upper cover and are electrically connected with described control circuit board, described inSolar panels can convert solar energy into electrical energy, and think the energy supply of described helicopter field landing indicator lamp.
In an embodiment, one end that described housing is relative with described light-emitting window also offers battery hole therein,Described battery hole is communicated with described battery container chamber, can realize battery taking and placing by described battery hole, described straightRise machine field landing indicator lamp and also comprise bottom, described bottom is fixed on described housing and covers described battery hole.
In an embodiment, described transparent upper cover offers first ring near one end of described light-emitting window thereinShape groove, the edge of described battery hole offers the second cannelure, and described helicopter field landing indicator lamp also wrapsDraw together:
The first sealing ring, is contained in described the first cannelure and is held on described transparent upper cover and described housingBetween;
The second sealing ring, is contained in described the second cannelure and is held between described housing and described bottom.
In an embodiment, also comprise lens therein, described lens are accommodated and are fixed in described housing,Described lens between described luminescence component and described transparent upper cover, the light that can send described luminescence componentLine carries out luminous intensity distribution.
In an embodiment, described housing is provided with therein:
Stroboscopic switch, is arranged at the sidewall of described housing and is electrically connected described stroboscopic with described control circuit boardSwitch is for controlling the switching of described infrared emitter;
Shift switch, is arranged at the sidewall of described housing and is electrically connected described gearshift with described control circuit boardSwitch is for controlling the degree of lighting of described VISIBLE LIGHT EMISSION body.
In an embodiment, described control circuit board is provided with antenna terminal, described helicopter field thereinLanding indicator lamp also comprise reception antenna, described reception antenna be arranged in described transparent upper cover and with described antennaJoint electrical connection, described reception antenna can receive remote signal, and by described antenna terminal by described remote controlSignal is sent to described control circuit board, and described control circuit board is according to luminous described in described remote signal controlAssembly is luminous.
In an embodiment, also comprise battery therein, described battery container in described battery container chamber alsoBe electrically connected with described control circuit board, described battery can be the energy supply of described helicopter field landing indicator lamp.
In an embodiment, described battery is secondary cell therein, and described control circuit board can be by too describedThe power storage that sun energy plate produces is in described battery.
In an embodiment, the sidewall of described housing is provided with charging inlet therein, can be by described chargingMouth charges to described battery.
In an embodiment, also comprise respirator therein, described respirator is arranged in the sidewall of described housing,So that described housing and extraneous UNICOM, described respirator is discharged for the hydrogen that described battery is produced.
Above-mentioned helicopter field landing indicator lamp, comprise housing, luminescence component, control circuit board and transparent onLid. Load onto after battery, luminescence component can be luminous under the control of control circuit board. Wherein, VISIBLE LIGHT EMISSIONThe light that body sends is for illumination, and the infrared light that infrared emitter sends is used to indicate position. Due to infraredLight need to be equipped with specific equipment and just can observe, thereby can avoid stating helicopter field landing indicator lamp by itOther people find. In addition, luminescence component and control circuit board are contained in and are formed by the assembling of housing and transparent upper coverIn host cavity, thereby make above-mentioned helicopter field landing indicating lamp structure compactness, small volume, in the wildBe difficult for being found. Therefore, above-mentioned helicopter field landing indicator lamp effectively raises disguise.
Brief description of the drawings
Fig. 1 is the structural representation of helicopter field landing indicator lamp in preferred embodiment of the present invention;
Fig. 2 is the assembly drawing of the landing of helicopter field shown in Fig. 1 indicator lamp.
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.In accompanying drawing, provide preferred embodiment of the present invention. But the present invention can come real in many different formsExisting, be not limited to embodiment described herein. On the contrary, providing the object of these embodiment is to make thisThe understanding of disclosure of an invention content is more comprehensively thorough.
It should be noted that, when element is called as " being fixed on " another element, it can be directly at another yuanOn part or also can have an element placed in the middle. When an element is considered to " connection " another element, it canBeing be directly connected to another element or may have centering elements simultaneously.
Unless otherwise defined, all technology and the scientific terminology using herein and belong to technology of the present inventionThe implication that the technical staff in field understands is conventionally identical. The art using in description of the present invention hereinLanguage, just in order to describe the object of specific embodiment, is not intended to be restriction the present invention. Use hereinTerm " and/or " comprise one or more relevant Listed Items arbitrarily with all combinations.
Refer to Fig. 1 and Fig. 2, in preferred embodiment of the present invention, helicopter field landing indicator lamp 100 comprises shellBody 110, luminescence component 120, control circuit board 130, transparent upper cover 140, solar panels 141, bottom150, lens 160, reception antenna 170 and battery 180.
The tubular structure that housing 110 is hollow. The shape of housing 110 can be rounded cylindrical, rectangular drum like etc.,Can be made by metal material or the high material of other mechanical strengths. One end opening of housing 110, this opening isLight-emitting window 111, light can be by light-emitting window 111 outgoing. In housing 110, be also provided with battery container chamber (not shown).Concrete, battery container chamber is positioned at housing 110 one end away from light-emitting window 111, and battery container chamber is used for accommodatingFor the battery of helicopter field landing indicator lamp 100 energy supplies.
In the present embodiment, one end that housing 110 is relative with light-emitting window 111 also offers battery hole 113, electricityHole, pond 113 is communicated with battery container chamber. In the time that battery need to be changed, just can realize electricity by battery hole 113Pond picks and places. Bottom 150 is fixed on housing 110 clad battery hole 113, thereby battery container chamber is sealed.Concrete, bottom 150 is fixed on housing 110 by screw is dismountable. Further, bottom 150For rectangular plate shape, its bottom flat. Therefore, can make helicopter field landing indicator lamp 100 directly stand on groundFace and need not adopt other modes to be fixed, thus convenient it is carried out to dismounting, improve helicopter fieldThe 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 envelopeClosed end omits bottom 150 simultaneously. In the time that battery need to be changed, can pass through light-emitting window 111 fetching batteries.
In the present embodiment, in battery container chamber, be provided with battery clip 112, when battery container is in battery container chamberWhen interior, battery clip 112 is for holding battery, thereby battery is fixed. It is pointed out that at otherIn embodiment, battery clip 112 can be by the replacement such as draw-in groove, thread gluing.
In the present embodiment, be also provided with respirator 114 on housing 110, respirator 114 is arranged in housing 110Sidewall so that housing 110 and extraneous UNICOM. Respirator 114 is discharged for the hydrogen that battery is produced.Therefore, can prevent that hydrogen from accumulating in housing 110, thereby avoid 100 of helicopter field landing indicator lampsRaw blast.
Luminescence component 120 is accommodated and is fixed in housing 110, and the exiting surface of luminescence component 120 points to outLight mouth 111. Luminescence component 120 comprises substrate 121 and is fixed on the illuminator 123 on substrate 121, substrateBe fixed on the inwall of housing 110 by modes such as screw threads for fastening. Illuminator 123 comprises infrared emitter (figureNot mark) and multiple light emitter (figure is mark not). Wherein, infrared emitter sends infrared ray, and infrared ray existsIn helicopter landing process, play indicative function. And just can observe because infrared ray need to be equipped with specific equipment.Therefore, utilize infrared ray to indicate and can prevent that the landing place of helicopter from exposing, thereby improve disguised.VISIBLE LIGHT EMISSION body is used for sending visible ray, and as infrared and gold-tinted, visible ray can be helicopter illumination is provided.
Control circuit board 130 is accommodated and is fixed in housing 110. Control circuit board 130 and luminescence component 120Electrical connection, luminous for controlling luminescence component 120. In addition, in the time that housing 110 is metal, control circuitPlate 130 need insulate with housing 110. Concrete, between control circuit board 130 and housing 110, pad is established one deckRed thick stick paper (figure is mark not). Control circuit board 130 can control luminescence component 120 middle infrared (Mid-IR) emitters logical,Disconnected, and the luminous degree of visible light emitters (being the number being lit in multiple visible light emitters). This, be also provided with status indicator lamp 131 on control circuit board 130 outward, control circuit board 130 is according to luminescence component120 luminance state of a control indicator lamp 131, falls so that status indicator lamp 131 demonstrates helicopter fieldThe duty of indicator lamp 100 falls.
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 is electrically connected with control circuit board 130. Concrete,Stroboscopic switch 115 is provided with the gear of "off", " connection ". Operating personnel can be as required at two gearsBetween switch. Control circuit board 130 just can be according to the gear stages control infrared ray of stroboscopic switch 115The switching of emitter.
Shift switch 117 is arranged at the sidewall of housing 110 and is electrically connected with control circuit board 130, and gearshift is openedClose 117 for controlling the degree of lighting of VISIBLE LIGHT EMISSION body. Concrete, shift switch 117 is provided with multipleGear, as 20%, 40%, 60%, 80% and 100%. When shift switch 117 lays respectively at above-mentioned gearTime, control circuit board 130 control successively 20%, 40%, 60%, 80% in multiple visible light emitters andAll luminous.
Transparent upper cover 140 is fixed on housing 110 and covers light-emitting window 111. Specifically in the present embodiment, transparentUpper cover 140 removably connects by screw and housing 110, need to be to the electronics unit in housing 110 thereby work asWhen part is safeguarded, transparent upper cover 140 can be taken off. Transparent upper cover 140 can have polyester material, glass,The transparent materials such as plastics are made, thereby making that transparent upper cover 140 is transparent can bright dipping. Transparent upper cover 140 and the endLid 150 coordinates, housing 110 sealed, thus the electronic component of accommodating in protection housing 110.
In the present embodiment, transparent upper cover 140 offers the first cannelure (figure near one end of light-emitting window 111Do not show), the edge of battery hole 113 offers the second cannelure (not shown). Helicopter field landing instructionLamp 100 also comprises the first sealing ring 190A and the second sealing ring 190B. Wherein:
The first sealing ring 190A be contained in the first cannelure and be held on transparent upper cover 140 and housing 110 itBetween, thereby make to contact and closely do not stay gap between transparent upper cover 140 and housing 110. The second sealing ring 190BBe contained in the second cannelure and be held between housing 110 and bottom 150, thus make housing 110 andBetween bottom 150, contact closely. Therefore, the first sealing ring 190A and the second sealing ring 190B further carryHigh helicopter field landing indicator lamp 100 sealing properties, thus its inner member better protected, and thenImprove quality and the service life of helicopter field landing indicator lamp 100.
Solar panels 141 can convert solar energy into electrical energy. Solar panels 141 are laminated structure, generally byHighly purified silicon is made. Solar panels 141 are attached at the inwall of transparent upper cover 140. In the present embodiment,The top of transparent upper cover 140 is for tiltedly splitting shape. Therefore, the inwall of transparent upper cover 140 is plane, thereby can makeSolar panels 141 are attached at the inwall of transparent upper cover 140 more closely. Solar panels 141 and control electricityRoad plate 130 is electrically connected, and the electric energy that control circuit board 130 produces solar panels 141 is through over commutation, voltage stabilizingAfter processing, be used to luminescence component 120 energy supplies.
Because helicopter field landing indicator lamp 100 generally uses in the wild, after being finished, battery may not haveBattery is changed in time, also there is no outlet for charging. And solar panels 141 can effectively utilize the sunCan be 100 energy supplies of helicopter field landing indicator lamp, thereby make to have expanded helicopter field landing indicator lamp 100The scope of application and extend its duration.
Lens 160 are accommodated and are fixed in housing 110. The shape of the shape of lens 161 and housing 110 openingsShape is consistent. Lens 160, can be to luminescence component 120 between luminescence component 120 and transparent upper cover 140The light sending carries out luminous intensity distribution. After lens 160 luminous intensity distributions, the light that can make luminescence component 120 sendOptic angle is large, light distribution is more even, thereby promotes instruction and the photograph of helicopter field landing indicator lamp 100Obvious results fruit. It is pointed out that in other embodiments, lens 160 also can omit.
In the present embodiment, control circuit board 130 is provided with antenna terminal 133, and reception antenna 170 is arranged inTransparent upper cover 140 is also electrically connected with antenna terminal 133. Reception antenna 170 can receive remote signal, and logicalCross antenna terminal 133 remote signal is sent to control circuit board 130, control circuit board 130 is believed according to remote controlNumber control luminescence component 120 luminous. By reception antenna 170, operating personnel can refer to helicopter field landingShow that lamp 100 realizes Long-distance Control. Therefore, operating personnel's indicator lamp 100 that can in advance helicopter field be landedBe positioned over somewhere, in the time that helicopter will land, Long-distance Control helicopter field landing indicator lamp 100 is worked,Thereby make operating personnel away from scene, thereby further improve disguised.
Further, on reception antenna 170, be arranged with rubber ring 171. Rubber ring 171 is held on reception antenna170 and transparent upper cover 140 between, thereby reception antenna 170 is contacted closely with transparent upper cover 140, enterOne step improves the sealing of helicopter field landing indicator lamp 100. It is pointed out that at other embodimentIn, also can adopt the mode of welding that reception antenna 170 is fixed on transparent upper cover 140, thereby avoid connecingReceive between antenna 170 and transparent upper cover 140 and have gap.
Battery 180 is contained in battery container chamber and with control circuit board 130 and is electrically connected. specifically at the present embodimentIn, battery 180 is fastened in battery clip 112, thereby is fixed in housing 110. Battery 180 can be goes straight up to100 energy supplies of machine field landing indicator lamp. It is pointed out that in other embodiments, battery 180 can be economizedSlightly. 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 control circuit board 130 can be by solar panels 141The power storage producing is in battery. The electric energy producing when solar panels 141 is to meet luminescence component 120 luminousTime also have residue, can utilize remaining electric energy to charge for battery 180, thereby improve solar panels 141Utilization rate.
Further, the sidewall of housing 110 is provided with charging inlet 119. Charging inlet 119 and control circuit board130 electrical connections, control circuit board 130 can be that the chemical energy of battery 180 is stored by electric energy conversion. Therefore,Can charge to battery 180 by charging inlet 119. It is pointed out that in other embodiments,Battery 180 also can be dry cell. After dry cell electric discharge completely, can change by battery hole 113, and notCharging inlet 119 must be set on housing 110.
Helicopter field landing indicator lamp 100, comprises housing 110, luminescence component 120, control circuit board 130And transparent upper cover 140. Load onto after battery, luminescence component 120 can be luminous under the control of control circuit board 130.Wherein, the light that VISIBLE LIGHT EMISSION body sends is for illumination, and the infrared light that infrared emitter sends is used in reference toShow position. Just can observe because infrared light need to be equipped with specific equipment, thereby can avoid stating helicopter open countryOuter landing indicator lamp 100 is found by other people. In addition, luminescence component 120 and control circuit board 130 are accommodatedIn being assembled in the host cavity forming by housing 110 and transparent upper cover 140, thereby make helicopter field landingIndicator lamp 100 compact conformations, small volume, be difficult for being found in the wild. Therefore, helicopter field landingIndicator lamp 100 effectively raises disguise.
The above embodiment has only expressed several embodiment of the present invention, and it describes comparatively concrete and detailed,But can not therefore be interpreted as the restriction to the scope of the claims of the present invention. It should be pointed out that for this areaThose of ordinary skill, without departing from the inventive concept of the premise, can also make some distortion andImprove, these all belong to protection scope of the present invention. Therefore, the protection domain of patent of the present invention should be with appendedClaim is as the criterion.
Claims (10)
1. a helicopter field landing indicator lamp, is characterized in that, comprising:
Housing, is the tubular structure of hollow, and one end of described housing offers light-emitting window, in described housing, goes backBe provided with battery container chamber;
Luminescence component, accommodates and is fixed in described housing, described in the exiting surface of described luminescence component points to, goes outLight mouth, described luminescence component comprises infrared emitter and VISIBLE LIGHT EMISSION body;
Control circuit board, accommodates and is fixed in described housing, described control circuit board and with described luminous groupPart electrical connection, luminous for controlling described luminescence component;
Transparent upper cover, is fixed on described housing and covers described light-emitting window, and the top of described transparent upper cover is obliqueSplit shape; And
Solar panels, are attached at the inwall of described transparent upper cover and are electrically connected with described control circuit board, described inSolar panels can convert solar energy into electrical energy, and think the energy supply of described helicopter field landing indicator lamp.
2. helicopter field landing indicator lamp according to claim 1, is characterized in that described housingOne end relative with described light-emitting window also offers battery hole, and described battery hole is communicated with described battery container chamber,Can realize battery taking and placing by described battery hole, described helicopter field landing indicator lamp also comprises bottom, instituteStating bottom is fixed on described housing and covers described battery hole.
3. helicopter field landing indicator lamp according to claim 2, is characterized in that, described transparentUpper cover offers the first cannelure near one end of described light-emitting window, and the edge of described battery hole offers secondCannelure, described helicopter field landing indicator lamp also comprises:
The first sealing ring, is contained in described the first cannelure and is held on described transparent upper cover and described housingBetween;
The second sealing ring, is contained in described the second cannelure and is held between described housing and described bottom.
4. helicopter field landing indicator lamp according to claim 1, is characterized in that, also comprisesMirror, described lens are accommodated and are fixed in described housing, and described lens are positioned at described luminescence component and describedBetween bright upper cover, the light that can send described luminescence component carries out luminous intensity distribution.
5. helicopter field landing indicator lamp according to claim 1, is characterized in that described housingBe provided with:
Stroboscopic switch, is arranged at the sidewall of described housing and is electrically connected described stroboscopic with described control circuit boardSwitch is for controlling the switching of described infrared emitter;
Shift switch, is arranged at the sidewall of described housing and is electrically connected described gearshift with described control circuit boardSwitch is for controlling the degree of lighting of described VISIBLE LIGHT EMISSION body.
6. helicopter field landing indicator lamp according to claim 1, is characterized in that described controlCircuit board is provided with antenna terminal, and described helicopter field landing indicator lamp also comprises reception antenna, described in connectReceive antenna and be arranged in described transparent upper cover and be electrically connected with described antenna terminal, described reception antenna can receive distantControl signal, and by described antenna terminal, described remote signal is sent to described control circuit board, described controlCircuit board processed is luminous according to luminescence component described in described remote signal control.
7. helicopter field landing indicator lamp according to claim 1, is characterized in that, also comprises electricityPond, described battery container is electrically connected in described battery container chamber and with described control circuit board, described batteryCan be the energy supply of described helicopter field landing indicator lamp.
8. helicopter field landing indicator lamp according to claim 7, is characterized in that described batteryFor secondary cell, the power storage that described control circuit board can produce described solar panels is in described battery.
9. helicopter field landing indicator lamp according to claim 8, is characterized in that described housingSidewall be provided with charging inlet, can charge to described battery by described charging inlet.
10. helicopter field landing indicator lamp according to claim 7, is characterized in that, also comprisesRespirator, described respirator is arranged in the sidewall of described housing, so that described housing and extraneous UNICOM, described inRespirator is discharged for the hydrogen that described battery is produced.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201310106341.2A CN104071344B (en) | 2013-03-28 | 2013-03-28 | Helicopter field landing indicator lamp |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201310106341.2A CN104071344B (en) | 2013-03-28 | 2013-03-28 | Helicopter field landing indicator lamp |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN104071344A CN104071344A (en) | 2014-10-01 |
| CN104071344B true CN104071344B (en) | 2016-05-18 |
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| Application Number | Title | Priority Date | Filing Date |
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| CN201310106341.2A Expired - Fee Related CN104071344B (en) | 2013-03-28 | 2013-03-28 | Helicopter field landing indicator lamp |
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Families Citing this family (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104633475A (en) * | 2013-11-07 | 2015-05-20 | 海洋王（东莞）照明科技有限公司 | Solar energy parking apron lamp |
| CN110382352A (en) * | 2018-01-19 | 2019-10-25 | 深圳市大疆创新科技有限公司 | Horn component and unmanned plane |
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| WO1993013984A1 (en) * | 1992-01-10 | 1993-07-22 | Guiding Star Pty, Ltd. | Pilot activated runway lighting system |
| WO1994025890A1 (en) * | 1993-04-30 | 1994-11-10 | Northrop Corporation | Holographic laser scanner and rangefinder |
| CN2243596Y (en) * | 1996-06-25 | 1996-12-25 | 郭玉坤 | All weather photoelectric optic fiber beacon light |
| JPH11245896A (en) * | 1998-03-02 | 1999-09-14 | Elna Co Ltd | Lamp for helicopter takeoff/landing site and lighting system using the same |
| US6567248B1 (en) * | 2002-02-01 | 2003-05-20 | Ronald M. Schmidt | Tri-spectrum aircraft landing light |
| CN202419414U (en) * | 2011-12-16 | 2012-09-05 | 安徽华东光电技术研究所 | Combined dual-mode airplane search lamp |
| CN102666281A (en) * | 2009-09-30 | 2012-09-12 | Adb有限责任公司 | Lighting unit for lighting airfields |
| BRMU9101495U2 (en) * | 2010-07-16 | 2012-12-04 | Comb And Energy S R L | light beacon |
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2013
- 2013-03-28 CN CN201310106341.2A patent/CN104071344B/en not_active Expired - Fee Related
Patent Citations (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO1993013984A1 (en) * | 1992-01-10 | 1993-07-22 | Guiding Star Pty, Ltd. | Pilot activated runway lighting system |
| WO1994025890A1 (en) * | 1993-04-30 | 1994-11-10 | Northrop Corporation | Holographic laser scanner and rangefinder |
| CN2243596Y (en) * | 1996-06-25 | 1996-12-25 | 郭玉坤 | All weather photoelectric optic fiber beacon light |
| JPH11245896A (en) * | 1998-03-02 | 1999-09-14 | Elna Co Ltd | Lamp for helicopter takeoff/landing site and lighting system using the same |
| 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 |
| BRMU9101495U2 (en) * | 2010-07-16 | 2012-12-04 | Comb And Energy S R L | light beacon |
| CN202419414U (en) * | 2011-12-16 | 2012-09-05 | 安徽华东光电技术研究所 | Combined dual-mode airplane search lamp |
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| CN104071344A (en) | 2014-10-01 |
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