CN207051580U - Lens cone for telescope, telescope and unmanned plane laser snipe system - Google Patents
Lens cone for telescope, telescope and unmanned plane laser snipe system Download PDFInfo
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- CN207051580U CN207051580U CN201720704121.3U CN201720704121U CN207051580U CN 207051580 U CN207051580 U CN 207051580U CN 201720704121 U CN201720704121 U CN 201720704121U CN 207051580 U CN207051580 U CN 207051580U
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- laser
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- transmission channel
- laser transmission
- lens barrel
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Abstract
It the utility model is related to a kind of lens cone for telescope, telescope and unmanned plane laser and snipe system, the lens cone for telescope, lens barrel body including straight pipe type, the side of the lens barrel body is provided with through hole, the through hole is connected with first laser transmission channel, and the first laser transmission channel is connected by the through hole with lens barrel body.The utility model in the side of lens barrel body by setting first laser transmission channel, the first rotary part can be utilized to drive first laser transmission channel and the rotation of lens barrel body, strike laser can be allowd to follow the movement of target and accordingly move, realize that targeting accuracy is hit.
Description
Technical field
It the utility model is related to unmanned plane counter field, particularly a kind of lens cone for telescope, telescope and unmanned plane laser
Snipe system.
Background technology
Flight can constitute a threat to safely unmanned plane to the even air defence of national public safety, flight safety in violation of rules and regulations.Such as profit
Taken on the sly with unmanned plane and steal information, carry the material to endanger public security, for another example, certain airport occurs that unmanned plane is black to fly
Event, cause a large amount of flights to be delayed, generate heavy losses.
Unmanned plane laser snipes system, is a kind of system for utilizing laser hits target (unmanned plane), and laser cell produces
Strike laser need to be transmitted by the module of optical system that is made up of various optical frames, and launched by telescopic system
Go.Accurately to hit home, it is necessary to carry out real-time tracking to target, and target be at any time all mobile, and can it is horizontal,
Pitching all directions move, it is therefore desirable to which the movement of target will also be followed and move by hitting laser, but current telescope can not
Meet this requirement.
Utility model content
The purpose of this utility model is to provide a kind of lens cone for telescope and telescope, and the application telescope nobody
Machine laser snipes system.
First problem to be solved in the utility model is that the optical axis for how realizing strike laser follows target mobile and moved
It is dynamic, therefore, the utility model embodiment provides following technical scheme：
A kind of lens cone for telescope, include the lens barrel body of straight pipe type, the side of the lens barrel body is provided with through hole, described logical
First laser transmission channel is connected with hole, the first laser transmission channel is connected by the through hole with lens barrel body.Enter
One step, the first laser transmission channel is provided with the first rotary part, for driving first laser transmission channel and lens barrel
Body rotates.
Second Problem to be solved in the utility model is how to realize the optical axis of strike laser in the horizontal direction and vertically
Change while direction, therefore, according to the utility model embodiment, the other end of the first laser transmission channel is connected with
Dual-laser transmission channel, and the first laser transmission channel is perpendicular to the second laser transmission channel.Further, second
Laser transmission channel is provided with the second rotary part, for driving second laser transmission channel, first laser transmission channel and mirror
Cylinder body rotation, and the rotary shaft of the first rotary part is perpendicular to the rotary shaft of the second rotary part.
3rd problem to be solved in the utility model is how to ensure laser transmission environment in lens cone for telescope clear
It is clean, therefore, according to the utility model embodiment, the laser output of the lens barrel body is provided with optical window mouth mirror, the light
The optical axis of the normal and strike laser beam of learning window mirror preferably has angle, and the angle is more than 0 ° and less than 20 °.
The utility model embodiment provide telescope, including in the utility model embodiment either type telescope
Cylinder, in addition to module of optical system, are arranged in lens cone for telescope, and laser is hit for transmitting.
The unmanned plane laser provided in the utility model embodiment snipes system, including：
Laser cell, for launching the strike laser to strike target；
Telescope in the utility model embodiment described in any embodiment, for strike Laser emission to be gone out.
According to the utility model embodiment, above-mentioned unmanned plane snipes system, in addition to target imaging unit, the optical system
System component includes at least one target following executive component, for changing beam direction in real time to track target, from target
Tracking light is incident in lens cone for telescope, after module of optical system transmits, in target imaging cell imaging, realize target with
Track.Target following light path shares a set of optical system with Laser emission light path, after target tracked locking, along same paths pair
It is launched laser and hit, and can ensure that target is met, and avoids accidentally injuring third party.
Compared with prior art, the beneficial effects of the utility model：The utility model in the side of lens barrel body by setting
First laser transmission channel is put, the first rotary part can be utilized to drive first laser transmission channel and the rotation of lens barrel body, made
The optical axis of laser, which must be hit, can follow the movement of target and accordingly move, and realize that targeting accuracy is hit.
Brief description of the drawings
, below will be to required use in embodiment in order to illustrate more clearly of the technical scheme of the utility model embodiment
Accompanying drawing be briefly described, it will be appreciated that the following drawings illustrate only some embodiments of the present utility model, therefore should not be by
Regard the restriction to scope as, for those of ordinary skill in the art, on the premise of not paying creative work, may be used also
To obtain other related accompanying drawings according to these accompanying drawings.
Fig. 1 is a kind of schematic diagram of the telescope of structure described in the utility model embodiment 1.
Fig. 2 is the schematic diagram of the telescope of another structure described in the utility model embodiment 1.
Fig. 3 is that optical window mouth mirror shows in the installation of the laser output of lens barrel body described in the utility model embodiment 1
It is intended to.
Fig. 4 is the structural representation that unmanned plane laser snipes system described in the utility model embodiment 2.
Description of symbols in figure
10- laser cells；20- target imaging units；30- optical window mouth mirrors；40- lens barrel bodies；50- trunnion axis；60- is erected
D-axis；70- second laser transmission channels；80- base frame casings；90- first laser transmission channels；The method of 100- optical window mouth mirrors
Line；311- telescope primary mirrors；312- telescope secondary mirrors；313-45 ° of speculum；314- spectroscopes.
Embodiment
Below in conjunction with accompanying drawing in the utility model embodiment, the technical scheme in the embodiment of the utility model is carried out clear
Chu, it is fully described by, it is clear that described embodiment is only the utility model part of the embodiment, rather than whole realities
Apply example.The component of the utility model embodiment being generally described and illustrated herein in the accompanying drawings can be come with a variety of configurations
Arrangement and design.Therefore, the detailed description of the embodiment of the present utility model to providing in the accompanying drawings is not intended to limit below
Claimed the scope of the utility model, but it is merely representative of selected embodiment of the present utility model.Based on the utility model
Embodiment, the every other embodiment that those skilled in the art are obtained on the premise of creative work is not made, all
Belong to the scope of the utility model protection.
Embodiment 1
Fig. 1-3 are referred to, provide a kind of telescope in the present embodiment, including lens cone for telescope and are arranged at telescope
Module of optical system in cylinder, wherein, lens cone for telescope includes the lens barrel body 40 of straight pipe type, and the side of lens barrel body 40 is provided with
Through hole, the through hole are connected with first laser transmission channel 90, and first laser transmission channel 90 passes through through hole and lens barrel body
40 connections.During implementation, preferably first laser transmission channel 90 is easy to assemble and keep lens cone for telescope perpendicular to lens barrel body 40
Good appearance.First laser transmission channel 90 and the size of through hole can be set according to the strike laser beam demand of transmission.
Can first laser transmission channel 90 set the first rotary part, for drive first laser transmission channel 90 and
Lens barrel body 40 rotates, and then realizes that strike laser follows the rotation of lens cone for telescope and rotated, or is interpreted as realizing strike
The transmission light path of laser will not change because of the motion of lens barrel, that is, keep strike laser alignment target all the time, realize essence
Quasi- strike.First rotary part can be arranged at the inner side of first laser transmission channel 90, but in order to not hinder to hit laser
Transmission, preferably the first rotary part is arranged at the outside of first laser transmission channel 90.As a kind of embodiment, the first rotation
Part can be hollow bearing.
In further perfect scheme, the other end of first laser transmission channel 90 is connected with second laser transmission channel
70, and first laser transmission channel 90 is perpendicular to second laser transmission channel 70.It can be set in second laser transmission channel 70
Second rotary part, for driving second laser transmission channel 70, first laser transmission channel 90 and lens barrel body 40 to rotate, and
Rotary shaft of the rotary shaft of first rotary part perpendicular to the second rotary part so that whole lens cone for telescope can be realized arbitrarily
The motion of orientation angle, realize that laser is comprehensive hits the mark for strike.
Module of optical system includes various optical frames, such as telescope primary mirror 311,312,45 ° of speculums of telescope secondary mirror
313 (being not necessarily 45 ° of speculums certainly, select with specific reference to system layout), sharing transmitting light path and receiving light path
In telescopic system, it is also possible to including spectroscope 314, target following executive component.Various optical frames are clear to its building ring mirror
Cleanliness requires higher, and the optical frames especially under the conditions of Laser emission requires higher, and dust, vapor in air etc. hold very much
Optical frames damage is easily caused, and the price of optical frames is relatively expensive, therefore, swashs to ensure that unmanned plane laser is sniped in system
Cleannes in light transmitter-telescope lens barrel, in this embodiment scheme, the laser output of lens barrel body 40 is provided with optics
Window mirror 30, optical window mouth mirror 30 are arranged at the laser output face of lens barrel body 40 by mounting seat.Mounting seat can be with
The mounting groove for being disposed on the inner side of lens barrel body 40 or the mounting collar for being arranged at the outside of lens barrel body 40, certainly
Can be other structures.Seal can also be set in optical window mouth mirror 30 and the contact site of mounting seat, make telescope
Air insulated inside and outside cylinder.
Optical window mouth mirror 30 is set by the laser output in lens cone for telescope, and then can be kept in lens cone for telescope
The cleaning of optical frames, deposition and condensation of the dust, water vapour in the outer air of lens cone for telescope on optical mirror plane are reduced, is extended
The service life of optical frames, especially extend service life of the optical frames under the conditions of Laser emission.
Material, machining and the plated film of optical window mouth mirror 30 are, it is necessary to meet to hit laser and the tracking light from target
High transmittance requirement, and required using stress.Two transparent surfaces of optical window mouth mirror 30 can be designed with an angle, with
When avoiding hitting laser light optical window mouth mirror 30, the light beam reflected from two transparent surfaces forms interference.
In embodiment shown in Fig. 3, optical window mouth mirror 30 is obliquely installed in the laser output of lens barrel body 40, optics
There is angle in window mirror 30 so that the normal 100 of optical window mouth mirror is with hitting the optical axis of laser beam not with laser output face
Overlap, there is certain angle, the preferably angle is more than 0 ° and less than 20 °, to avoid the two of optical window mouth mirror 30 surface reflections
The strike laser returned is caused to damage or disturbed to lens barrel internal optics or sensor.
In embodiment shown in Fig. 1, projection phase of the telescope secondary mirror 312 in the place plane of telescope primary mirror 311
Overlap, i.e. Cassegrain's formula telescope.In embodiment shown in Fig. 2, telescope secondary mirror 312 is in the telescope primary mirror
The projection of 311 place planes is misaligned, and telescope secondary mirror 312 can be avoided to hinder the transmitting of strike laser and weaken strike laser
Beating Strength.
Embodiment 2
Referring to Fig. 4, a kind of unmanned plane laser is provided in the present embodiment snipes system, including laser cell, telescope
And target imaging unit 20, telescope are any embodiment telescope in embodiment 1.
Laser cell 10, including laser, for launching the strike laser to strike target.
Telescope, the strike Laser emission for laser cell 10 to be launched are gone out.
Module of optical system in lens cone for telescope is applied not only to transmission strike laser, it may also be used for transmission is from target
Light is tracked, in order to realize the reliable tracking of target, module of optical system includes at least one target following executive component, uses
Change beam direction in real-time to track target.Tracking light from target is incident to lens cone for telescope through optical window mouth mirror 30
It is interior, after module of optical system transmits, it is imaged in target imaging unit 20, realizes target following.
Unmanned plane laser described in the present embodiment is sniped in system, and target following light path shares a set of with Laser emission light path
Light path system, after target tracked locking, laser is launched to it along same paths and hit, can ensure that target is accurate
Hit, avoid accidentally injuring third party.
Unmanned plane laser as shown in Figure 4 is sniped in system, and lens cone for telescope is installed in frame, in the drive of drive device
Under dynamic, frame drives the part or all of optical frames formed in lens cone for telescope and module of optical system that it is supported around level
Axle 50 rotates and/or vertical axes 60 rotate.
For example, partial optical mirror (telescope primary mirror 311, the telescope secondary mirror 312, one in the module of optical system
45 ° of speculums 313) in lens barrel body, partial optical mirror is together with laser cell 10, imaging unit 20, spectrophotometric unit 33
It is integrated in base frame casing 80.
Telescope described in embodiment one can cause the transmitting beam position between telescope secondary mirror 312 and spectroscope 314
In trunnion axis 50 (also referred to as horizontal axis, horizontal axis of rotation) and vertical axes 60 (also referred to as vertical axis, vertical rotation
Axis), such as 45 ° of speculums are located in vertical axes 60, and 45 ° of speculums are respectively positioned on water with another 45 ° of speculums
On flat axle 50, as shown in figure 4, to ensure the real-time transmission side for changing light beam during frame drives lens cone for telescope rotation
To realizing target by real-time lock, and then target is met.
It is described above, only specific embodiment of the present utility model, but the scope of protection of the utility model is not limited to
In this, any one skilled in the art can readily occur in change in the technical scope that the utility model discloses
Or replace, it should all cover within the scope of protection of the utility model.
Claims (9)
1. a kind of lens cone for telescope, include the lens barrel body of straight pipe type, it is characterised in that the side of the lens barrel body is provided with logical
Hole, the through hole are connected with first laser transmission channel, and the first laser transmission channel passes through the through hole and lens barrel sheet
Body connects；The first laser transmission channel is provided with the first rotary part, for driving first laser transmission channel and lens barrel
Body rotates.
2. lens cone for telescope according to claim 1, it is characterised in that first rotary part is arranged at first laser
The outside of transmission channel.
3. lens cone for telescope according to claim 1, it is characterised in that the first laser transmission channel is perpendicular to described
Lens barrel body.
4. according to any described lens cone for telescope of claim 1-3, it is characterised in that the first laser transmission channel it is another
One end is connected with second laser transmission channel, and the first laser transmission channel is perpendicular to the second laser transmission channel.
5. lens cone for telescope according to claim 4, it is characterised in that second laser transmission channel is provided with the second rotation
Part, for driving second laser transmission channel, first laser transmission channel and lens barrel body to rotate, and the first rotary part
Rotary shaft of the rotary shaft perpendicular to the second rotary part.
6. lens cone for telescope according to claim 4, it is characterised in that the laser output of the lens barrel body is provided with
Optical window mouth mirror, the optical axis of the normal and strike laser beam of the optical window mouth mirror have angle, and the angle is more than 0 ° and is less than
20°。
7. a kind of telescope, it is characterised in that including any described lens cone for telescope of claim 1-6, in addition to optical system
System component, is arranged in lens cone for telescope, and laser is hit for transmitting.
8. a kind of unmanned plane laser snipes system, it is characterised in that including：
Laser cell, for launching the strike laser to strike target；
Telescope described in claim 7, for the strike Laser emission to be gone out.
9. unmanned plane laser according to claim 8 snipes system, it is characterised in that also including target imaging unit, institute
Stating module of optical system includes at least one target following executive component, for changing beam direction in real time to track target, comes
It is incident to from the tracking light of target in lens cone for telescope, it is real in target imaging cell imaging after module of optical system transmits
Existing target following.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720704121.3U CN207051580U (en) | 2017-06-16 | 2017-06-16 | Lens cone for telescope, telescope and unmanned plane laser snipe system |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720704121.3U CN207051580U (en) | 2017-06-16 | 2017-06-16 | Lens cone for telescope, telescope and unmanned plane laser snipe system |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN207051580U true CN207051580U (en) | 2018-02-27 |
Family
ID=61493271
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201720704121.3U Active CN207051580U (en) | 2017-06-16 | 2017-06-16 | Lens cone for telescope, telescope and unmanned plane laser snipe system |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN207051580U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107065165A (en) * | 2017-06-16 | 2017-08-18 | 成都安的光电科技有限公司 | Lens cone for telescope, telescope and unmanned plane laser snipe system |
-
2017
- 2017-06-16 CN CN201720704121.3U patent/CN207051580U/en active Active
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107065165A (en) * | 2017-06-16 | 2017-08-18 | 成都安的光电科技有限公司 | Lens cone for telescope, telescope and unmanned plane laser snipe system |
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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: 20210611 Address after: No.25, unit 1, building 2, No.21 Fanghua street, high tech Zone, Chengdu, Sichuan 610041 Patentee after: Yang Wei Address before: 1 / F, 124 Zhuojin North Road, high tech Zone, Chengdu, Sichuan 610041 Patentee before: CHENGDU ANTI PHOTOELECTRIC TECHNOLOGY Co.,Ltd. |
|
| TR01 | Transfer of patent right | ||
| TR01 | Transfer of patent right |
Effective date of registration: 20220629 Address after: 215600 ground floor, building C, Dongcheng science and Technology Pioneer Park, Miaoqiao Kechuang Road, Tangqiao town, Zhangjiagang City, Suzhou City, Jiangsu Province Patentee after: Zhongkezhuoxin semiconductor technology (Suzhou) Co.,Ltd. Address before: No.25, unit 1, building 2, No.21 Fanghua street, high tech Zone, Chengdu, Sichuan 610041 Patentee before: Yang Wei |