CN114994877A - Large-aperture small-pixel large-target-surface ultra-wide-temperature composite heat dissipation differential thermal imaging lens - Google Patents
Large-aperture small-pixel large-target-surface ultra-wide-temperature composite heat dissipation differential thermal imaging lens Download PDFInfo
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Abstract
Description
技术领域technical field
本发明涉及一种红外热成像镜头消热差设计,尤其是需要大相对孔径,靶面越来越大,像元尺寸越来越小,而且工作温度范围超宽的工作场景的镜头消热差应用。The invention relates to an infrared thermal imaging lens athermalization design, in particular to the lens athermalization of a working scene that requires a large relative aperture, the target surface is getting larger, the pixel size is getting smaller and smaller, and the working temperature range is ultra-wide application.
背景技术Background technique
红外光学系统所处的使用环境都在常温常压下,未考虑温度变化等因素对光学系统成像质量的影响。然而对于特殊用途的红外光学系统而言,所处的环境温度会有很大的变化。当温度改变时,由于光学材料与结构材料的热不稳定性,当环境温度变化时,光学元件的曲率、厚度和间隔将发生变化,同时元件材料的折射率也发生改变,从而引起系统焦距变化,像面发生位移,导致系统性能急剧下降,图像质量恶化。因而在军用红外光学,空间红外光学,以及极端环境及工业应用场景情况下,需要满足环境工作温度的消热差红外热成像镜头设计需求。The operating environment of the infrared optical system is under normal temperature and pressure, and the influence of factors such as temperature change on the imaging quality of the optical system is not considered. However, for special-purpose infrared optical systems, the ambient temperature will vary greatly. When the temperature changes, due to the thermal instability of the optical material and the structural material, when the ambient temperature changes, the curvature, thickness and spacing of the optical element will change, and the refractive index of the element material will also change, causing the system focal length to change. , the image plane is displaced, resulting in a sharp drop in system performance and deterioration in image quality. Therefore, in the case of military infrared optics, space infrared optics, and extreme environments and industrial application scenarios, it is necessary to meet the design requirements of athermalized infrared thermal imaging lenses that meet the ambient operating temperature.
尤其是对于大相对孔径镜头来讲,景深相对较小。而且随着红外热成像探测器的发展,像元大小从35μm,25μm,17μm发展到现在10-12μm的像元尺寸,成像靶面从传统的160×120,320×240,384×288发展到现在640×512,1240×768甚至1280×1024阶段。所以对红外热成像消热差镜头设计需求有着更大的考验。Especially with large relative aperture lenses, the depth of field is relatively small. And with the development of infrared thermal imaging detectors, the pixel size has developed from 35μm, 25μm, 17μm to the current pixel size of 10-12μm, and the imaging target surface has developed from the traditional 160×120, 320×240, 384×288 to 640×512 , 1240×768 or even 1280×1024 stage. Therefore, there is a greater test for the design requirements of infrared thermal imaging athermal lenses.
目前消热差热成像镜头应用大都是早期大像元尺寸设计,满足工作温度段有限,基本集中在满足大于17微米以上像元,640×512靶面尺寸探测器,系统工作温度在-20℃~﹢40℃较多。At present, most of the athermal imaging lens applications are designed with large pixel size in the early stage, which can meet the limited operating temperature range, and basically focus on satisfying the pixel larger than 17 microns, 640 × 512 target size detectors, and the system operating temperature is -20 ℃ ~﹢40℃ is more.
目前采用的消热差设计主要有以下两种方式。There are two main methods of heat dissipation difference design currently used.
采用光机主动式:Adopt opto-mechanical active:
这种方法通过电机控制调焦机构,在不同温度环境下进行镜头的调焦适应,以达到满足成像质量。这种方法主要问题在于尺寸庞大,需增加复杂的调焦机构,以及电机等组件。增加了系统总体尺寸以及重量。同时增加了在调焦过程中光轴一致性的因素,容易造成在调焦过程中光轴晃动等不良影响。In this method, the focus adjustment mechanism is controlled by the motor, and the focus adjustment of the lens is carried out under different temperature environments to meet the imaging quality. The main problem with this method is the large size and the need to add a complex focusing mechanism, as well as components such as motors. Increases the overall size and weight of the system. At the same time, the factor of the consistency of the optical axis during the focusing process is increased, which is likely to cause adverse effects such as the optical axis shaking during the focusing process.
采用机械被动式和光学被动式:With mechanical passive and optical passive:
机械被动式方法采用特殊的合金材料作为镜筒框体结构,在光学设计时考虑镜筒的膨胀系数加以整体设计,通常所选材料为反常材料,高温材料缩短,低温材料膨胀。这样才能满足通常高温时焦平面前移,缩短与镜头间隔;低温时焦平面后移,增加与镜头间隔,采用这种材料成本极高。The mechanical passive method uses a special alloy material as the frame structure of the lens barrel. In the optical design, the expansion coefficient of the lens barrel is considered for the overall design. Usually, the selected material is an abnormal material, the high temperature material shortens, and the low temperature material expands. Only in this way can the focal plane move forward at high temperature, shortening the distance with the lens; when the temperature is low, the focal plane moves backward, increasing the distance with the lens, and the cost of using this material is extremely high.
光学被动式通常采用锗、硒化锌、硫系玻璃等两种以上的光学材质进行设计,成本高。而且对于硫系玻璃来讲,通常由S、Se、Te三种元素与其它如有Ge、Ga、As、Sb等金属元素形成的一种无氧红外玻璃,通常采用热压等方法成型,尺寸不会很大,很难加工大口径光学元件,并且通常掺杂元素里具有砷(As)等剧毒物质,加工不友好、不环保。Optical passive type is usually designed with two or more optical materials such as germanium, zinc selenide, chalcogenide glass, etc., and the cost is high. And for chalcogenide glass, an oxygen-free infrared glass usually formed by three elements of S, Se, Te and other metal elements such as Ge, Ga, As, Sb, etc., is usually formed by hot pressing and other methods. It is not very large, and it is difficult to process large-diameter optical components, and usually doping elements contain highly toxic substances such as arsenic (As), which are unfriendly and environmentally friendly.
对于以上两种被动设计方式的镜头设计应用在小相对孔径,例如F/1.2 F/1.4等小孔径小焦距镜头得以应用,但往往设计只能满足-20℃~+40℃的温差范围。并且设计基本只能满足在640×512靶面尺寸以下的,大于17μm像元尺寸以上的红外探测器应用。For the above two passive design methods, the lens design is applied to small relative aperture, such as F/1.2 F/1.4 and other small aperture and small focal length lenses, but the design can only meet the temperature difference range of -20℃~+40℃. And the design can basically only meet the application of infrared detectors below the target size of 640×512 and larger than the pixel size of 17μm.
发明内容SUMMARY OF THE INVENTION
为了克服现有技术中不能做到大相对孔径,难以满足小像元,大靶面设计,以及不能实现-50℃~+80℃的宽温度段无电机,小尺寸的无热化红外热成像的技术问题,本发明提供一种采用特殊材料配合多套环式结构设计与采用单一锗材料进行二元光学设计向结合的方式,实现了对于相对孔径F/#=1.0,环境温度-50℃~+80℃,对于像元尺寸10微米,1280×1024阵列的大靶面红外热成像自适应被动无热化光学镜头设计,使得全温度段成像质量接近衍射极限。In order to overcome the inability to achieve a large relative aperture in the prior art, it is difficult to meet the needs of small pixels, large target surface design, and the inability to achieve a wide temperature range of -50 ° C ~ + 80 ° C without motor, small size athermalized infrared thermal imaging To solve the technical problem, the present invention provides a way of combining special materials with multi-ring structure design and binary optical design using a single germanium material, which realizes the relative aperture F/#=1.0 and the ambient temperature -50°C. ~+80℃, for the pixel size of 10 microns, the large target infrared thermal imaging adaptive passive athermal optical lens design of 1280×1024 array makes the imaging quality in the whole temperature range close to the diffraction limit.
本发明解决其技术问题所采用的技术方案是:The technical scheme adopted by the present invention to solve its technical problems is:
红外光学系统消热差设计要求光学元件的轴向色差为零,温度变化时光学元件产生的离焦与机械结构产生的离焦相互抵消,从而使整个系统不产生温度离焦。全折射元件组成的光学被动式消热差系统,至少需要三种以上的材料,且系统比较复杂。而本发明采用单一锗单晶材料,同时采用衍射光学元件独特的温度特性和色散特性,实现外光学系统能够用更简单的结构实现一定温度范围内的消热差设计。The athermal design of the infrared optical system requires that the axial chromatic aberration of the optical element is zero, and the defocus generated by the optical element and the defocus generated by the mechanical structure cancel each other when the temperature changes, so that the entire system does not generate temperature defocus. The optical passive athermalization system composed of all-refractive elements requires at least three or more materials, and the system is relatively complex. However, the present invention adopts a single germanium single crystal material, and at the same time adopts the unique temperature characteristics and dispersion characteristics of diffractive optical elements, and realizes that the external optical system can realize the athermalization design within a certain temperature range with a simpler structure.
光学元件的温度特性由光热膨胀系数表示,定义为透镜温度变化引起的焦距的归一化变化:The temperature characteristic of an optical element is represented by the coefficient of photothermal expansion, defined as the normalized change in focal length due to changes in lens temperature:
对于折射元件,采用薄透镜模型可以得到它的光热膨胀系数:For a refractive element, its coefficient of thermal expansion of light can be obtained by using the thin lens model:
式中,α为光学元件的线膨胀系数,n为光学元件的折射率,”n0为环境介质的折射率,dn/dT为材料的折射率温度系数。In the formula, α is the linear expansion coefficient of the optical element, n is the refractive index of the optical element, "n 0 is the refractive index of the ambient medium, and dn/dT is the temperature coefficient of refractive index of the material.
衍射元件的光热膨胀系数为:The optical thermal expansion coefficient of the diffractive element is:
折射元件的温度特性由材料的膨胀系数和材料的折射率温度系数决定,而衍射元件的温度特性只是由材料的膨胀系数决定而与材料的折射率温度系数无关。The temperature characteristic of the refractive element is determined by the expansion coefficient of the material and the temperature coefficient of the refractive index of the material, while the temperature characteristic of the diffractive element is only determined by the expansion coefficient of the material and has nothing to do with the temperature coefficient of the refractive index of the material.
衍射元件的光热膨胀系数相对于折射元件很小,但其色散因子远远大于折射元件的,可以承担系统的消色差功能。因此折衍混合红外光学系统可以利用衍射元件消色差再合理分配折射元件的光焦度进行消热差,降低了消热差红外光学系统的设计难度,简化了系统结构.使系统有很大的设计自由度。The optical thermal expansion coefficient of the diffractive element is relatively small compared to the refractive element, but its dispersion factor is much larger than that of the refractive element, which can undertake the achromatic function of the system. Therefore, the diffractive-diffractive hybrid infrared optical system can use the diffractive element to achromatically distribute the refractive power of the refraction element for athermal aberration, which reduces the design difficulty of the athermalized infrared optical system and simplifies the system structure. The system has great design freedom.
单一采用衍射二元光学设计可以很好的优化成像质量,一定环境温度范围内能够满足小像元,大靶面的需求设计。但在大相对孔径,-50℃~+80℃的宽温度段范围内,不能够满足全温度范围的消热差设计。The single use of the diffractive binary optical design can optimize the imaging quality very well, and can meet the needs of small pixels and large target surfaces within a certain ambient temperature range. However, in the wide temperature range of -50℃~+80℃ with large relative pore size, it cannot meet the design of heat dissipation difference in the whole temperature range.
依照光学设计分析,温度升高时,焦平面相对前移,需缩小镜头与焦平面之间的距离。反之,当温度降低时,焦平面相对后移,需增加焦平面与镜头之间的距离。According to the optical design analysis, when the temperature rises, the focal plane moves forward relatively, and the distance between the lens and the focal plane needs to be reduced. Conversely, when the temperature decreases, the focal plane moves relatively backward, and the distance between the focal plane and the lens needs to be increased.
温度变化时像面与镜头相对位置线性变化,通过温度变化时,像面与镜头相对位置的变化长度L=ɑT,T为常温与高温或低温时的温度差值,ɑ为膨胀材料线膨胀系数。When the temperature changes, the relative position of the image surface and the lens changes linearly. When the temperature changes, the change length of the relative position of the image surface and the lens L=ɑT, T is the temperature difference between normal temperature and high temperature or low temperature, and ɑ is the linear expansion coefficient of the expansion material .
所以需选择满足高热膨胀系数的材料,同时具备一定的润滑功能,且改材料能够满足高低温极端温度工作环境。材料选用PE-UHMW超高分子量聚乙烯,是分子量高250万的热塑性工程塑料。抗冲击性、耐腐蚀性好、优异的耐化学性能、密度比其他热塑性塑料低,摩擦系数低、适中的机械强度、刚性的耐蠕变性能,优异的机械加工性能、良好的抗高能量辐射性能。同时PE-UHMW可以在-150℃~90℃环境温度下正常工作。更为重要的是,PE-UHMW高热膨胀系数的缺点,刚好在增加镜筒整体移动量的巨大优势,可以较小长度实现较大的膨胀、压缩距离。设计采用转接环衔接方式,这样在较短的空间可以实现温度变化时膨胀或压缩的变化累加量,最大程度减小镜头尺寸。转接环采用低膨胀系数的殷钢,减少转接环节带来的自身膨胀因素。为了使镜头整体移动,需内套活动镜筒受力均匀分布,弹簧采用多圈平端波纹簧。当温度升高时,膨胀材料的累积增加,压迫与滑动镜筒连接为一体的膨胀挡圈向后移动,滑动镜筒整体后移,达到了温度升高时缩短焦平面与镜头之间距离作用。当温度降低时,膨胀材料的累积缩短,压迫与滑动镜筒连接为一体的膨胀挡圈向前移动,滑动镜筒整体前移,达到了温度降低时增加焦平面与镜头之间距离作用。膨胀材料温度变化长度与光学设计温度变化离焦量结合设计膨胀材料总体长度。Therefore, it is necessary to select materials that meet the high thermal expansion coefficient, and at the same time have a certain lubricating function, and the modified materials can meet the high and low temperature extreme temperature working environment. The material is PE-UHMW ultra-high molecular weight polyethylene, which is a thermoplastic engineering plastic with a molecular weight of 2.5 million. Impact resistance, good corrosion resistance, excellent chemical resistance, lower density than other thermoplastics, low friction coefficient, moderate mechanical strength, rigid creep resistance, excellent machinability, good resistance to high energy radiation performance. At the same time, PE-UHMW can work normally under the ambient temperature of -150℃~90℃. More importantly, the disadvantage of PE-UHMW's high thermal expansion coefficient is just the huge advantage of increasing the overall movement of the lens barrel, which can achieve a larger expansion and compression distance with a smaller length. The design adopts an adapter ring connection method, so that the cumulative amount of expansion or compression changes can be realized in a short space, and the size of the lens can be minimized. The adapter ring is made of invar with low expansion coefficient, which reduces the self-expansion factor brought by the adapter link. In order to make the lens move as a whole, the inner sleeve of the movable lens barrel needs to be evenly distributed, and the spring adopts a multi-turn flat-end corrugated spring. When the temperature rises, the accumulation of the expanding material increases, and the expansion retaining ring connected with the sliding lens barrel is pressed to move backward, and the sliding lens barrel moves backward as a whole, which shortens the distance between the focal plane and the lens when the temperature rises. . When the temperature decreases, the accumulation of the expanding material shortens, and the expansion retaining ring connected with the sliding lens barrel is pressed to move forward, and the sliding lens barrel moves forward as a whole, so as to increase the distance between the focal plane and the lens when the temperature decreases. The temperature change length of the intumescent material and the defocus amount of the optical design temperature change are combined to design the overall length of the intumescent material.
本发明的有益效果是,本发明通过采用衍射二元光学设计与多套环式被动结构自调整的消热差相结合的设计技术方式。实现体积小、重量轻、可靠性高而工作温度范超大,同时满足大相对孔径,小像元,大靶面的现代高精度红外光学系统。有效解决了现有技术通过单一锗单晶不能满足大相对孔径,小像元,大靶面红外光学系统通过被动方式达到-50℃~+80℃的宽温度段范围清晰成像的目标。The beneficial effect of the present invention is that the present invention adopts a design technique that combines the diffractive binary optical design and the self-adjusted athermalization difference of the multi-ring passive structure. It realizes a modern high-precision infrared optical system with small size, light weight, high reliability and large operating temperature range, while meeting the requirements of large relative aperture, small pixel and large target surface. It effectively solves the problem that the existing technology cannot meet the large relative aperture, small pixel, and large target surface infrared optical system through a single germanium single crystal to achieve clear imaging in a wide temperature range of -50°C to +80°C by passive means.
附图说明:图1是本发明示意图;Description of drawings: Fig. 1 is the schematic diagram of the present invention;
图中:1.锗透镜1;2.锗透镜2;3.锗透镜3(含二元衍射面);4.高膨胀超高分子量聚乙烯;5.殷钢转接环;6.高膨胀超高分子量聚乙烯;7.膨胀挡圈;8.多圈平端波纹簧;9.滑动内镜筒;10.外镜筒;11.探测器成像面。In the picture: 1.
具体实施方式 :Detailed ways :
大孔径小像元大靶面超宽温复合消热差热成像镜头包括锗透镜1,锗透镜2,含有二元衍射面的锗透镜3。通过二元衍射光学设计与多套环式被动结构自调整的消热差相结合的设计技术方式实现针对大相对孔径,小像元大靶面的红外热成像光学系统在50℃~+80℃的宽温度段范围清晰成像的目的。在使用二元衍射面锗透镜3,保证常温环境附近较小的环境温度范围能够良好成像质量前提下,通过仿真出不同环境温度下镜头整体与探测器成像面11之间的相对位移。依照所选取的高膨胀超高分子量聚乙烯线胀系数,计算出所需高线胀系数且自润滑的高分子量聚乙烯的材料长度,使用套环的方式是的轴向空间尺寸变小,做到体积最小化的目的。当温度升高时,膨胀材料4和6的长度累积增加,压迫与滑动镜筒连接为一体的膨胀挡圈7向后移动,滑动镜筒整体后移,达到了温度升高时缩短焦平面与镜头之间距离作用。当温度降低时,膨胀材料4和6的累积缩短,压迫与滑动镜筒连接为一体的膨胀挡圈7向前移动,滑动镜筒整体前移,达到了温度降低时增加焦平面与镜头之间距离作用。膨胀挡圈7与内镜筒9刚性连接,转接环5采用热胀系数趋于零的殷钢材质,对内镜筒施力的弹簧使用多圈平端波纹簧8,保证内镜筒9移动轴向压力均匀,内镜筒9与外镜筒10能够平滑移动。最终达到整体被动无热化的光学系统。The large-aperture, small-pixel, large-target-surface, ultra-wide-temperature composite athermalization thermal imaging lens includes a
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