CN206669546U - A kind of antiaircraft headlamp - Google Patents
A kind of antiaircraft headlamp Download PDFInfo
- Publication number
- CN206669546U CN206669546U CN201720199819.4U CN201720199819U CN206669546U CN 206669546 U CN206669546 U CN 206669546U CN 201720199819 U CN201720199819 U CN 201720199819U CN 206669546 U CN206669546 U CN 206669546U
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- CN
- China
- Prior art keywords
- lower house
- antiaircraft
- installation portion
- upper shell
- headlamp
- 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.)
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Abstract
The utility model provides a kind of antiaircraft headlamp, including：Light source, lens, lampshade, upper shell, lower house, tube face and reflection bowl structure；Wherein, upper shell is fixedly connected with lower house；Lampshade and lens are fixed on upper shell；Reflection bowl structure, tube face are fixed on lower house；Light source is arranged on tube face, and the enclosure interior that the light that light source is sent is formed towards upper shell and lower house, reverberation bowl structure is located at enclosure interior, and is located at the same side of housing with light source；Lens is located at the enclosure interior side relative with reflecting bowl structure.This antiaircraft headlamp small volume, it is simple in construction, be easily installed and dismantle；The redundance of reverberation bowl is eliminated, manufacturing cost is reduced, improves the utilization rate of reverberation bowl.Solve that military vehicle air defense headlamp volume is small, illuminating effect is well and reliable and stable, the problem of driving vision will not be found by other side air force again be able to can be provided at night.
Description
Technical field
Automotive field is the utility model is related to, more particularly to a kind of antiaircraft headlamp.
Background technology
Antiaircraft headlamp is a kind of indispensable configuration of military vehicle, it is contemplated that its functional characteristic, is regarded according to laws and regulations requirement for front
Wild illuminator, in order that providing driving vision and not found by other side air force, this requires that antiaircraft headlamp volume is small, shines
Obvious results fruit is well and reliable and stable.Left side front before vehicle is arranged according to laws and regulations requirement, according to moulding and customer requirement, determined
Appearance on vehicle.
Utility model content
The utility model embodiment technical problems to be solved are to provide a kind of antiaircraft headlamp, to realize anti-unprecedented photograph
Lamp small volume, good illumination effect and reliable and stable, meet military vehicle during night running with the same of good driving vision
When and do not found by other side air force.
In order to solve the above technical problems, the utility model embodiment provides a kind of antiaircraft headlamp, including：Light source, match somebody with somebody
Light microscopic, lampshade, upper shell, lower house, tube face and reflection bowl structure；
Wherein, the upper shell is fixedly connected with the lower house；
The lampshade and the lens are fixed on the upper shell；
The reflection bowl structure, the tube face are fixed on the lower house；
The light source is arranged on the tube face, and light that the light source is sent is towards the upper shell and the lower casing
The enclosure interior that body is formed, the reverberation bowl structure is located at the enclosure interior, and is located at the same of the housing with the light source
Side；The lens is located at the enclosure interior side relative with the reflection bowl structure.
The tube face is fixed with the lower house by rotary clamping.
Wherein, antiaircraft headlamp also includes：The ventilating component being fixedly connected with the lower house, the ventilating component pass through
Rubber ring is fixedly clamped with the ventilative post on the lower house.
Wherein, the upper shell and the lower house are Nian Jie and/or limit rib connects and fixes by cold glue.
Wherein, the lens is fixed with the upper shell by ultrasonic bonding.
Wherein, the lampshade and the upper shell are spirally connected fixation by screw.
Wherein, the reflection bowl structure includes：
Reflecting surface, the first limit rib, the second limit rib, the first installation portion and the second installation portion；
Wherein, first installation portion is connected with the first end of the reflecting surface, second installation portion and the reflection
The second end connection in face；
First limit rib is arranged between first installation portion and second installation portion, and positioned at close to described
The first end of reflecting surface；
Second limit rib is arranged between first installation portion and second installation portion, and positioned at close to described
Second end of reflecting surface.
Wherein, first installation portion has the first mounting surface and the first mounting hole, and passes through first mounting hole
It is fixedly connected with the lower house.
Second installation portion has the second mounting surface and the second mounting hole, and by second mounting hole with it is described
Lower house is fixedly connected.
Wherein, the reflection bowl structure is consolidated by first limit rib and the second limit rib with the lower house clamping
It is fixed.
Wherein, there is frame structure between first installation portion, second installation portion, four of the frame structure
The connection side in face is equipped with knuckle, and the reflecting surface 9 is arranged on the frame structure towards a face in the housing
On.
Compared with prior art, the antiaircraft headlamp and antiaircraft headlamp reverberation bowl knot that the utility model embodiment provides
Structure, at least have the advantages that：
1. an antiaircraft headlamp reflection bowl structure does simple and exquisite, unnecessary part is eliminated, alleviates weight, drop
Low manufacturing cost, the service efficiency for improving antiaircraft headlamp reflection bowl structure.
2. an antiaircraft headlamp reflection bowl structure is spirally connected and the dual fixation of limit rib clamping using screw, assembling is improved
Stability.
3. an antiaircraft headlamp small volume, it is simple in construction, be easily installed and dismantle, good illumination effect, meet national military standard electricity
Device system requirements and luminous intensity distribution laws and regulations requirement.
Brief description of the drawings
Fig. 1 is antiaircraft headlamp schematic diagram；
Fig. 2 is antiaircraft headlamp reverberation bowl structural representation；
Fig. 3 is that antiaircraft headlamp reflects another schematic diagram of bowl structure；
Fig. 4 is that antiaircraft headlamp reflects another schematic views of bowl structure；
Fig. 5 is the another schematic diagram that antiaircraft headlamp reflects bowl structure.
【Description of reference numerals】
1st, light source；2nd, lens；3rd, lampshade；4th, upper shell；5th, bowl structure is reflected；6th, ventilating component；7th, lower house；8th, lamp
Steep seat；9th, reflecting surface；101st, the first limit rib；102nd, the second limit rib；111st, the first installation portion；112nd, the second installation portion.
Embodiment
To make the technical problems to be solved in the utility model, technical scheme and advantage clearer, below in conjunction with accompanying drawing
And specific embodiment is described in detail.
Referring to Fig. 2 to Fig. 5, a kind of antiaircraft headlamp is present embodiments provided, including：Light source 1, lens 2, lampshade 3, on
Housing 4, lower house 7, tube face 8 and reflection bowl structure 5；
Wherein, upper shell 4 is fixedly connected with lower house 7；Lampshade 3 and lens 2 are fixed on upper shell 4；Reverberation bowl knot
Structure 5, tube face 8 are fixed on lower house 7；
Preferably, light source 1 is arranged on tube face 8, and the light that light source 1 is sent is formed towards upper shell 4 and lower house 7
Enclosure interior, reflection bowl structure 5 is located at enclosure interior, and is located at the same side of housing with light source 1；Lens 2 is located in housing
The portion side relative with reflection bowl structure 5.
Preferably, tube face 8 is fixed with lower house 7 by rotary clamping；Tube face 8 is integrated connector, and one end spins
Light source 1, the other end is to inserting body harness.Specifically, the rotary clamping of light source 1 is on tube face 8, be easy to the installation of light source 1 with more
Change, while ensure that the Assembly stability of light source 1；Connection is facilitated to inserting body harness, avoids the complicated labor of wiring
It is dynamic；Tube face 8 is fixed on lower house 7 by the way of rotary clamping, limits all frees degree, improves the stabilization of assembling
Property, while facilitate the installation and removal of tube face 8.
In a preferred embodiment of the present utility model, in addition to：The ventilating component 6 being fixedly connected with lower house 7.Specifically
Ground, ventilating component 6 are fixedly clamped by rubber ring and the ventilative post on lower house 7, on the one hand, the presence of ventilating component 6 can be with
Prevent from hazing in antiaircraft headlamp, influence illuminating effect；On the other hand processing can be saved to fix with rubber ring, while can also protected
Demonstrate,proving it has good stability, convenient installation.
In another embodiment of the present utility model, upper shell 4 and lower house 7 are by the way that cold glue is Nian Jie and/or limit rib clamping
It is fixed；Limit rib can be such that upper shell 4 is accurately positioned with lower house 7 as guiding mechanism, convenient installation；The letter of cold glue technique for sticking
Just, it is not necessary to complicated process equipment, infringement will not be produced to housing, ensure that the luminous intensity distribution performance of lens 2, and have housing
There is good sealing, can prevent from being exposed to light accidentally, in order to avoid cause the attention of other side air force.
In another embodiment of the present utility model, lens 2 is fixed with upper shell 4 by ultrasonic bonding；Supersonic welding
The welding of multiple combinations material is applicable to, and the high temperature of material will not be caused to pollute and damage, so using ultrasonic wave herein
Weldering may insure that the original structure of lens 2 is constant, it is ensured that it reaches the photometric standards of national military standard；Make lens 2 firm simultaneously
Be arranged on upper shell 4 on, it is ensured that the stability of installation.
In another embodiment of the present utility model, lampshade 3 and upper shell 4 are spirally connected fixation by screw；Lampshade 3 can block
Light, prevent light is launched upwards from being found by other side air force；Meanwhile lampshade 3 can also protect lens 2, ensure lens 2
Precision；The mode that screw is spirally connected can facilitate the installation and removal of lampshade 3.
In another preferred embodiment of the present utility model, reflection bowl structure 5 includes：Reflecting surface 9, the first limit rib 101,
Two limit ribs 102, the first installation portion 111 and the second installation portion 112；
Wherein, the first installation portion 111 is connected with the first end of reflecting surface 9, the second installation portion 112 and the second of reflecting surface 9
End connection；
Specifically, the first limit rib 101 is arranged between the first installation portion 111 and the second installation portion 112, and positioned at close
The first end of reflecting surface 9；
Second limit rib 102 is arranged between the first installation portion 111 and the second installation portion 112, and positioned at close to reflecting surface 9
The second end.
Further, the first installation portion 111 has the first mounting surface and the first mounting hole, and by the first mounting hole with
Lower house 7 is spirally connected fixation using screw；
Second installation portion 112 has the second mounting surface and the second mounting hole, and passes through the second mounting hole and the profit of lower house 7
It is spirally connected fixation with screw.
Preferably, reflection bowl structure 5 is connected and fixed by the first limit rib 101 and the second limit rib 102 with lower house 7；
Limit rib 101 and limit rib 102 can be used as guide frame, reflection bowl structure 5 is accurately positioned when mounted, convenient
Worker installs, and saves man-hour.
Reflection bowl structure 5 is spirally connected using screw, the clamping of limit rib 101 and the multiple fixation of the clamping of limit rib 102, is defined anti-
Penetrate all frees degree of bowl structure 5, it is ensured that the Assembly stability of reflection bowl structure 5, while facilitate the peace of reflection bowl structure 5
Assembly and disassembly.
Preferably, there is frame structure between the first installation portion 111, the second installation portion 112, four faces of frame structure
Connection side is equipped with knuckle；The reflecting surface 9 is arranged on the frame structure towards on a face in the housing；Cross
The design for crossing fillet adds the aesthetic property of reflection bowl structure 5, while the corner angle for avoiding four sides cause to installer master worker
Injury.
Described above is preferred embodiment of the present utility model, it is noted that for the ordinary skill of the art
For personnel, on the premise of principle described in the utility model is not departed from, some improvements and modifications can also be made, these improvement
The scope of protection of the utility model is also should be regarded as with retouching.
Claims (10)
- A kind of 1. antiaircraft headlamp, it is characterised in that including：Light source (1), lens (2), lampshade (3), upper shell (4), lower house (7), tube face (8) and reflection bowl structure (5)；Wherein, the upper shell (4) is fixedly connected with the lower house (7)；The lampshade (3) and the lens (2) are fixed on the upper shell (4)；The reflection bowl structure (5), the tube face (8) are fixed on the lower house (7)；The light source (1) is arranged on the tube face (8), light that the light source (1) sends towards the upper shell (4) and The enclosure interior that the lower house (7) is formed, the reflection bowl structure (5) are located at the enclosure interior, and with the light source (1) Positioned at the same side of the housing；The lens (2) is located at one relative with the reflection bowl structure (5) of the enclosure interior Side.
- 2. antiaircraft headlamp according to claim 1, it is characterised in that the tube face (8) is logical with the lower house (7) Rotation is crossed to connect and fix.
- 3. antiaircraft headlamp according to claim 1, it is characterised in that also include：It is fixedly connected with the lower house (7) Ventilating component (6), the ventilating component (6) is fixedly clamped by rubber ring and the ventilative post on the lower house (7).
- 4. antiaircraft headlamp according to claim 1, it is characterised in that the upper shell (4) is logical with the lower house (7) Supercooling glue sticking and/or limit rib connect and fix.
- 5. antiaircraft headlamp according to claim 1, it is characterised in that the lens (2) is logical with the upper shell (4) Ultrasonic bonding is crossed to fix.
- 6. antiaircraft headlamp according to claim 1, it is characterised in that the lampshade (3) passes through with the upper shell (4) Screw is spirally connected fixation.
- 7. antiaircraft headlamp according to claim 1, it is characterised in that the reflection bowl structure (5) includes：Reflecting surface (9), the first limit rib (101), the second limit rib (102), the first installation portion (111) and the second installation portion (112)；Wherein, first installation portion (111) is connected with the first end of the reflecting surface (9), second installation portion (112) with The second end connection of the reflecting surface (9)；First limit rib (101) is arranged between first installation portion (111) and second installation portion (112), and Positioned at the first end close to the reflecting surface (9)；Second limit rib (102) is arranged between first installation portion (111) and second installation portion (112), and Positioned at close to the second end of the reflecting surface (9).
- 8. antiaircraft headlamp according to claim 7, it is characterised in that first installation portion (111) has the first peace Dress face and the first mounting hole, and be fixedly connected by first mounting hole with the lower house (7)；Second installation portion (112) has the second mounting surface and the second mounting hole, and passes through second mounting hole and institute Lower house (7) is stated to be fixedly connected.
- 9. antiaircraft headlamp according to claim 7, it is characterised in that the reflection bowl structure (5) passes through described first Limit rib (101) and the second limit rib (102) connect and fix with the lower house (7).
- 10. antiaircraft headlamp according to claim 7, it is characterised in that first installation portion (111), described second There is frame structure, the connection side in four faces of the frame structure is equipped with knuckle, described anti-between installation portion (112) Penetrate face (9) and be arranged on the frame structure towards on a face in the housing.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720199819.4U CN206669546U (en) | 2017-03-02 | 2017-03-02 | A kind of antiaircraft headlamp |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720199819.4U CN206669546U (en) | 2017-03-02 | 2017-03-02 | A kind of antiaircraft headlamp |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN206669546U true CN206669546U (en) | 2017-11-24 |
Family
ID=60379919
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201720199819.4U Active CN206669546U (en) | 2017-03-02 | 2017-03-02 | A kind of antiaircraft headlamp |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN206669546U (en) |
-
2017
- 2017-03-02 CN CN201720199819.4U patent/CN206669546U/en active Active
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| TR01 | Transfer of patent right | ||
| TR01 | Transfer of patent right |
Effective date of registration: 20200806 Address after: 101300 Zhaofeng Town, Shunyi District, Beijing Zhaofeng industrial base Tongxin Road No. 1 Patentee after: BAIC GROUP ORV Co.,Ltd. Address before: 101300, 99, Shuanghe Avenue, Renhe Town, Beijing, Shunyi District Patentee before: BEIJING AUTOMOBILE RESEARCH GENERAL INSTITUTE Co.,Ltd. |