CN107783257A - Big scene depth space radioresistance camera lens - Google Patents

Big scene depth space radioresistance camera lens Download PDF

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Publication number
CN107783257A
CN107783257A CN201711013863.2A CN201711013863A CN107783257A CN 107783257 A CN107783257 A CN 107783257A CN 201711013863 A CN201711013863 A CN 201711013863A CN 107783257 A CN107783257 A CN 107783257A
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CN
China
Prior art keywords
lens
positive lens
group
airspace
radioresistance
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Granted
Application number
CN201711013863.2A
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Chinese (zh)
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CN107783257B (en
Inventor
刘辉
钟兆铨
林春生
康哲恺
黄剑峰
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Fujian Forecam Optics Co Ltd
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Fujian Forecam Optics Co Ltd
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Priority to CN201711013863.2A priority Critical patent/CN107783257B/en
Publication of CN107783257A publication Critical patent/CN107783257A/en
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    • GPHYSICS
    • G02OPTICS
    • G02BOPTICAL ELEMENTS, SYSTEMS OR APPARATUS
    • G02B13/00Optical objectives specially designed for the purposes specified below
    • GPHYSICS
    • G02OPTICS
    • G02BOPTICAL ELEMENTS, SYSTEMS OR APPARATUS
    • G02B1/00Optical elements characterised by the material of which they are made; Optical coatings for optical elements

Abstract

The present invention relates to a kind of big scene depth space radioresistance camera lens, along light, incident direction is sequentially provided with preceding group of microscope group A, light bar B, rear group microscope group C from left to right in the optical system of the camera lens, group microscope group A is made up of negative lens A 1, positive lens A 2, negative lens A 3 successively from left to right before described, group microscope group C is made up of positive lens C 1, biconcave lens C 2, positive lens C 3, positive lens C 4 successively from left to right after described, simple in construction.

Description

Big scene depth space radioresistance camera lens
Technical field
The present invention relates to a kind of big scene depth space radioresistance camera lens, it is related to the optical camera field of photoelectric video technology.
Background technology
Irradiation space environment includes:Electronics, proton and a small amount of high energy cosmic-ray particle.Flouride-resistani acid phesphatase technology typically has passively Guard technology and active defense technology.Passive protection technology is to protect optical device with tantalum piece etc., to increase its capability of resistance to radiation, but This will greatly increase load weight, and aircraft is quite harsh to the weight demands of load, because load weight increases 1kg, hair The system of penetrating will increase by hundreds of kilograms, costly.With the development of space technology, for ensure aerospace craft functional reliability and Long-life, so preferred will improve the capability of resistance to radiation of optical device in itself, this proposes higher requirement to radiation resistance.
The content of the invention
The purpose of the present invention is to be directed to above weak point, there is provided a kind of big scene depth space radioresistance mirror simple in construction Head.
The technical scheme is that a kind of big scene depth space radioresistance camera lens, along light in the optical system of the camera lens Incident direction is sequentially provided with preceding group of microscope group A, light bar B, rear group microscope group C to line from left to right, and microscope group A is organized before described from left to right successively It is made up of negative lens A-1, positive lens A-2, negative lens A-3, microscope group C is organized after described from left to right successively by positive lens C-1, concave-concave Lens C-2, positive lens C-3, positive lens C-4 compositions.
Further, the airspace between the preceding group microscope group A and light bar B is 1.36mm, the light bar B and rear group mirror Airspace between group C is 0.47mm.
Further, the airspace between the negative lens A-1 and positive lens A-2 is 4.15mm;Positive lens A-2 and negative Airspace between lens A-3 is 1.78mm.
Further, the airspace between the positive lens C-1 and biconcave lens C-2 is 2.53mm;Biconcave lens C-2 Airspace between positive lens C-3 is 0.27mm;Airspace between positive lens C-3 and positive lens C-4 is 0.09mm.
Further, the negative lens A-1, positive lens A-2, negative lens A-3, positive lens C-1 use radiation resistant glass LAK9G15, BK7G18 are made.
Compared with prior art, the invention has the advantages that:(1)The structure of the big scene depth space radioresistance camera lens Simply, compact, using 7 fully separating spheric glasses, total transmissivity formula optical texture, there is the larger angle of visual field, very well Ground corrects various aberrations, in 0.2m to infinity scope good imaging quality, high resolution;(2)Capability of resistance to radiation is strong, anti-spoke Penetrate dosage 1000Krad(Si), possess and reliablely and stablely run in radiation environment for a long time;(3)Light-weight design, reduce system Volume and weight;(4)By being combined from rational glass material, realize the optics of system without thermalized design, -40 DEG C~ MTF and disc of confusion size significantly decline with not occurring under normal temperature state in+60 DEG C of temperature ranges, meet the big temperature difference environment in space Under requirement.
Brief description of the drawings
Patent of the present invention is further illustrated below in conjunction with the accompanying drawings.
Fig. 1 is the optical system diagram of the embodiment of the present invention.
Fig. 2 is the distortion figure of the embodiment of the present invention.
Fig. 3 is that the MTF that object distance of the embodiment of the present invention is infinity schemes;
Fig. 4 is that the MTF that object distance of the embodiment of the present invention is 0.2m schemes;
Fig. 5 is the mechanical structure schematic diagram of the embodiment of the present invention.
In figure:
Microscope group C, A-1 negative lens A-1, A-2 positive lens A-2, A-3 negative lens A-3, C- are organized after microscope group A, B- light bar B, C- are organized before A- 1 positive lens C-1, C-2 biconcave lens C-2, C-3 positive lens C-3, C-4 positive lens C-4,1- body tube, 2-A piece trim rings, 3-AB every Circle, 4-BC spacer rings, 5-G piece trim rings, 6-DE spacer rings, 7-EF spacer rings, 8-FG spacer rings.
Embodiment
The present invention is further described with reference to the accompanying drawings and detailed description.
As shown in Fig. 1~5, a kind of big scene depth space radioresistance camera lens, along light from a left side in the optical system of the camera lens Incident direction is sequentially provided with preceding group of microscope group A, light bar B, rear group microscope group C to the right, and microscope group A is organized before described from left to right successively by negative saturating Mirror A-1, positive lens A-2, negative lens A-3 compositions, microscope group C is organized after described from left to right successively by positive lens C-1, biconcave lens C- 2nd, positive lens C-3, positive lens C-4 are formed.
In the present embodiment, the airspace between the preceding group microscope group A and light bar B is 1.36mm, and the light bar B is with after Airspace between group microscope group C is 0.47mm.
In the present embodiment, the airspace between the negative lens A-1 and positive lens A-2 is 4.15mm;Positive lens A-2 Airspace between negative lens A-3 is 1.78mm.
In the present embodiment, the airspace between the positive lens C-1 and biconcave lens C-2 is 2.53mm;Concave-concave is saturating Airspace between mirror C-2 and positive lens C-3 is 0.27mm;Airspace between positive lens C-3 and positive lens C-4 is 0.09mm。
In the present embodiment, the negative lens A-1, positive lens A-2, negative lens A-3, positive lens C-1 use radiation hardness Glass LAK9G15, BK7G18 are made, and can greatly reduce the radiation of space high-energy ray, particle to optical mirror slip and rear end The damage of imaging sensor, extend the service life of whole system.
In the present embodiment, the optical system being made up of above-mentioned lens set has reached following optical index:
Focal length:f′=3.9mm;
The angle of visual field:60°×45°;
Blur-free imaging scope:The infinity of 0.2m~7;
Spectral region:450nm~700nm;
6 μm of 6 μ m of pixel dimension;
Weight:≤20g;
In the present embodiment, the parameter of each eyeglass is as shown in the table:
In the present embodiment, the negative lens A-1, positive lens A-2, negative lens A-3 are set in sequence in the front end of body tube 1 successively And compressed with A pieces trim ring 2, AB spacer rings 3 are provided between the negative lens A-1 and positive lens A-2, the positive lens A-2 is saturating with bearing BC spacer rings 4 are provided between mirror A-3;The positive lens C-1, biconcave lens C-2, positive lens C-3, positive lens C-4 are sequentially set successively Put in primary mirror tube rear end and compressed with G pieces trim ring 5, DE spacer rings 6 are provided between the positive lens C-1 and biconcave lens C-2, EF spacer rings 7 are provided between the biconcave lens C-2 and positive lens C-3, are set between the positive lens C-3 and positive lens C-4 There are FG spacer rings 8.
In the present embodiment, group microscope group A, light bar B, rear group microscope group C are imaged before light order enters.
The object, technical solutions and advantages of the present invention are further described by above-listed preferred embodiment, are answered Understand, the foregoing is merely illustrative of the preferred embodiments of the present invention, is not intended to limit the invention, all essences in the present invention God any modification, equivalent substitution and improvements made etc., should be included in the scope of the protection with principle.

Claims (5)

  1. A kind of 1. big scene depth space radioresistance camera lens, it is characterised in that:In the optical system of the camera lens along light from left to right Incident direction is sequentially provided with preceding group of microscope group A, light bar B, rear group microscope group C, and microscope group A is organized before described from left to right successively by negative lens A- 1st, positive lens A-2, negative lens A-3 are formed, it is described after group microscope group C from left to right successively by positive lens C-1, biconcave lens C-2, just Lens C-3, positive lens C-4 are formed.
  2. 2. big scene depth space radioresistance camera lens according to claim 1, it is characterised in that:Group microscope group A and light bar B before described Between airspace be 1.36mm, the airspace between the light bar B and rear group microscope group C is 0.47mm.
  3. 3. big scene depth space radioresistance camera lens according to claim 1, it is characterised in that:The negative lens A-1 and just saturating Airspace between mirror A-2 is 4.15mm;Airspace between positive lens A-2 and negative lens A-3 is 1.78mm.
  4. 4. big scene depth space radioresistance camera lens according to claim 1, it is characterised in that:The positive lens C-1 and concave-concave Airspace between lens C-2 is 2.53mm;Airspace between biconcave lens C-2 and positive lens C-3 is 0.27mm;Just Airspace between lens C-3 and positive lens C-4 is 0.09mm.
  5. 5. big scene depth space radioresistance camera lens according to claim 1, it is characterised in that:The negative lens A-1, positive lens A-2, negative lens A-3, positive lens C-1 are made of radiation resistant glass LAK9G15, BK7G18.
CN201711013863.2A 2017-10-26 2017-10-26 Large depth-of-field space radiation-resistant lens Active CN107783257B (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201711013863.2A CN107783257B (en) 2017-10-26 2017-10-26 Large depth-of-field space radiation-resistant lens

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201711013863.2A CN107783257B (en) 2017-10-26 2017-10-26 Large depth-of-field space radiation-resistant lens

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CN107783257A true CN107783257A (en) 2018-03-09
CN107783257B CN107783257B (en) 2019-12-24

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Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN112666684A (en) * 2020-12-23 2021-04-16 福建福光股份有限公司 Radiation-resistant wide-angle lens
CN114153049A (en) * 2021-12-06 2022-03-08 杭州径上科技有限公司 Fixed-focus radiation-proof lens

Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5303088A (en) * 1991-10-23 1994-04-12 Canon Kabushiki Kaisha Retrofocus type lens
US5668669A (en) * 1991-11-13 1997-09-16 Nikon Corporation Compact wide-angle objective lens
JP2012252253A (en) * 2011-06-06 2012-12-20 Canon Inc Zoom lens and imaging device with the same
CN106291882A (en) * 2016-09-06 2017-01-04 浙江舜宇光学有限公司 Pick-up lens
CN206515544U (en) * 2016-12-27 2017-09-22 东莞市宇瞳光学科技股份有限公司 Small-sized super large aperture tight shot

Patent Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5303088A (en) * 1991-10-23 1994-04-12 Canon Kabushiki Kaisha Retrofocus type lens
US5668669A (en) * 1991-11-13 1997-09-16 Nikon Corporation Compact wide-angle objective lens
JP2012252253A (en) * 2011-06-06 2012-12-20 Canon Inc Zoom lens and imaging device with the same
CN106291882A (en) * 2016-09-06 2017-01-04 浙江舜宇光学有限公司 Pick-up lens
CN206515544U (en) * 2016-12-27 2017-09-22 东莞市宇瞳光学科技股份有限公司 Small-sized super large aperture tight shot

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN112666684A (en) * 2020-12-23 2021-04-16 福建福光股份有限公司 Radiation-resistant wide-angle lens
CN112666684B (en) * 2020-12-23 2023-01-31 福建福光股份有限公司 Radiation-resistant wide-angle lens
CN114153049A (en) * 2021-12-06 2022-03-08 杭州径上科技有限公司 Fixed-focus radiation-proof lens

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