CN111024235B - Infrared focal plane supporting structure with thermal stress unloading function - Google Patents
Infrared focal plane supporting structure with thermal stress unloading function Download PDFInfo
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- G01J5/00—Radiation pyrometry, e.g. infrared or optical thermometry
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Abstract
本发明公开了一种具有热应力卸载功能的红外焦面支撑结构,包括:探测器读出电路、基板、支撑结构、冷头、冷指和柔性卸载导热丝;其中,所述探测器读出电路粘接在基板上;所述基板粘接在所述支撑结构上;所述支撑结构安装在冷头上;所述冷指与所述冷头相连接;所述柔性卸载导热丝设置于所述支撑结构内。本发明解决了红外焦平面组件的高效导热以及热应力和热变形问题。
The invention discloses an infrared focal plane support structure with thermal stress unloading function, comprising: a detector readout circuit, a substrate, a support structure, a cold head, a cold finger and a flexible unloading heat-conducting wire; wherein, the detector reads out The circuit is bonded on the substrate; the substrate is bonded on the support structure; the support structure is mounted on the cold head; the cold finger is connected with the cold head; the flexible unloading thermal wire is arranged on the inside the support structure. The invention solves the problems of efficient heat conduction and thermal stress and thermal deformation of the infrared focal plane assembly.
Description
技术领域technical field
本发明属于空间遥感器焦平面支撑结构技术领域,尤其涉及一种具有热应力卸载功能的红外焦面支撑结构。The invention belongs to the technical field of focal plane support structures of space remote sensors, and in particular relates to an infrared focal plane support structure with thermal stress unloading function.
背景技术Background technique
近年来,随着空间红外相机的不断发展,红外探测器由单元、少元、多元线列向多元面阵、长线列、大面阵方向发展,推动红外探测技术由点目标向扫描成像、推扫成像到凝视成像方向发展。目前广泛采用多片探测器拼接技术来满足使用要求,焦面的尺寸可以达到100~300毫米。In recent years, with the continuous development of space infrared cameras, infrared detectors have developed from single-unit, few-element, multi-element line arrays to multi-element area arrays, long line arrays, and large area arrays, promoting infrared detection technology from point targets to scanning imaging, pushing From scanning imaging to gaze imaging. At present, multi-piece detector splicing technology is widely used to meet the requirements of use, and the size of the focal plane can reach 100-300 mm.
倒装互连焊接焦方式是探测器集成的主要方式之一,将碲镉汞光敏元芯片与读出电路芯片互连耦合,形成焦平面探测器。然后将探测器粘接到拼接基板上(基本材料可选用蓝宝石、碳化硅、硅等),然后再粘接到焦面支撑结构上。支撑结构连接焦面基板和制冷机的冷头,冷头一般采用紫铜、钼铜等材料。多种材料在常温下集成或装配在一起,在低温下工作时,不可避免地产生热变形和热应力。支撑结构的主要功能是:1)将冷头的冷量高效率地传递到焦面;2)减小焦平面的热变形,减小探测器的热应力,保证焦面的平面度。Flip-chip interconnect welding focal method is one of the main methods of detector integration. The mercury cadmium telluride photosensitive element chip is interconnected and coupled with the readout circuit chip to form a focal plane detector. The detector is then bonded to the splice substrate (sapphire, silicon carbide, silicon, etc. can be selected as the base material), and then bonded to the focal plane support structure. The support structure connects the focal plane substrate and the cold head of the refrigerator, and the cold head is generally made of copper, molybdenum copper and other materials. A variety of materials are integrated or assembled together at normal temperature, and thermal deformation and thermal stress are inevitably generated when working at low temperature. The main functions of the support structure are: 1) efficiently transfer the cooling energy of the cold head to the focal plane; 2) reduce the thermal deformation of the focal plane, reduce the thermal stress of the detector, and ensure the flatness of the focal plane.
红外探测器需要通过制冷手段降低热噪声,通常情况需要在低温下(55K~120K)才具备良好的成像性能。探测器组件在常温下装配,在降温过程中由于材料热膨胀系数差异会产生热应力及变形,可能会造成探测器光敏面不共面甚至探测器出现断裂,严重影响了成像质量和组件可靠性。Infrared detectors need to reduce thermal noise by means of cooling, and usually need to have good imaging performance at low temperatures (55K ~ 120K). Detector components are assembled at room temperature. During the cooling process, thermal stress and deformation will occur due to the difference in thermal expansion coefficient of materials, which may cause the photosensitive surface of the detector to be non-coplanar or even break the detector, which seriously affects the imaging quality and component reliability.
发明内容SUMMARY OF THE INVENTION
本发明解决的技术问题是:克服现有技术的不足,提供了一种具有热应力卸载功能的红外焦面支撑结构,解决了红外焦平面组件的高效导热以及热应力和热变形问题。The technical problem solved by the present invention is to overcome the deficiencies of the prior art, provide an infrared focal plane support structure with thermal stress unloading function, and solve the problems of efficient heat conduction, thermal stress and thermal deformation of the infrared focal plane assembly.
本发明目的通过以下技术方案予以实现:一种具有热应力卸载功能的红外焦面支撑结构,包括:探测器读出电路、基板、支撑结构、冷头、冷指和柔性卸载导热丝;其中,所述探测器读出电路粘接在基板上;所述基板粘接在所述支撑结构上;所述支撑结构安装在冷头上;所述冷指与所述冷头相连接;所述柔性卸载导热丝设置于所述支撑结构内。The object of the present invention is achieved through the following technical solutions: an infrared focal plane support structure with thermal stress unloading function, comprising: a detector readout circuit, a substrate, a support structure, a cold head, a cold finger and a flexible unloading heat conducting wire; wherein, the detector readout circuit is bonded on the substrate; the substrate is bonded on the support structure; the support structure is mounted on the cold head; the cold finger is connected with the cold head; the flexible The unloading thermal wire is arranged in the support structure.
上述具有热应力卸载功能的红外焦面支撑结构中,所述支撑结构为平板,其中,平板的下表面设置有H型冷指粘接面;平板的上表面设置有第一探测器基板侧粘接面、第二探测器基板侧粘接面、第三探测器基板侧粘接面、第四探测器基板侧粘接面和柔性传热区域;其中,第一探测器基板侧粘接面和第二探测器基板侧粘接面相对,第一探测器基板侧粘接面和第二探测器基板侧粘接面均位于平板的上表面的外边缘;第三探测器基板侧粘接面和第四探测器基板侧粘接面相对,第三探测器基板侧粘接面和第四探测器基板侧粘接面均位于平板的上表面的外边缘;柔性传热区域位于平板的上表面的中间位置,柔性卸载导热丝设置于柔性传热区域。In the above infrared focal plane support structure with thermal stress unloading function, the support structure is a flat plate, wherein the lower surface of the flat plate is provided with an H-type cold finger adhesive surface; the upper surface of the flat plate is provided with a first detector substrate side adhesive surface. a junction surface, a second detector substrate side bonding surface, a third detector substrate side bonding surface, a fourth detector substrate side bonding surface and a flexible heat transfer area; wherein the first detector substrate side bonding surface and The bonding surfaces on the side of the second detector substrate are opposite, and the bonding surfaces on the side of the first detector substrate and the side of the second detector substrate are both located at the outer edge of the upper surface of the flat plate; The adhesive surfaces on the side of the fourth detector substrate are opposite to each other, and the adhesive surfaces on the side of the third detector substrate and the side of the fourth detector substrate are both located at the outer edge of the upper surface of the flat plate; the flexible heat transfer area is located on the upper surface of the flat plate. In the middle position, the flexible unloading thermal wire is arranged in the flexible heat transfer area.
上述具有热应力卸载功能的红外焦面支撑结构中,平板的上表面开设有贯穿槽X1、贯穿槽X2、贯穿槽X3、贯穿槽X4、非贯穿槽X5、非贯穿槽X6、非贯穿槽Y1和非贯穿槽Y2;其中,贯穿槽X1、贯穿槽X2、贯穿槽X3、贯穿槽X4、非贯穿槽X5、非贯穿槽X6、非贯穿槽Y1和非贯穿槽Y2位于H型冷指粘接面的边界位置处;非贯穿槽X5和非贯穿槽X6相对,非贯穿槽X5和非贯穿槽X6平行;贯穿槽X1和贯穿槽X2相对,贯穿槽X1和贯穿槽X2平行;贯穿槽X3和贯穿槽X4相对,贯穿槽X3和贯穿槽X4平行;非贯穿槽Y1和非贯穿槽Y2相对,非贯穿槽Y1和非贯穿槽Y2平行。In the above-mentioned infrared focal plane support structure with thermal stress unloading function, the upper surface of the flat plate is provided with a through slot X1, a through slot X2, a through slot X3, a through slot X4, a non-through slot X5, a non-through slot X6, and a non-through slot Y1. and non-penetrating groove Y2; wherein, the penetration groove X1, penetration groove X2, penetration groove X3, penetration groove X4, non penetration groove X5, non penetration groove X6, non penetration groove Y1 and non penetration groove Y2 are located in the H-type cold finger bonding At the boundary position of the surface; the non-penetrating groove X5 is opposite to the non-penetrating groove X6, and the non-penetrating groove X5 and the non-penetrating groove X6 are parallel; the penetration groove X1 is opposite to the penetration groove X2, and the penetration groove X1 and the penetration groove X2 are parallel; The through grooves X4 are opposite, the through grooves X3 and X4 are parallel; the non-through grooves Y1 and the non-through grooves Y2 are opposite, and the non-through grooves Y1 and the non-through grooves Y2 are parallel.
上述具有热应力卸载功能的红外焦面支撑结构中,平板的下表面开设有非贯穿槽X7、非贯穿槽X8、非贯穿槽Y3、非贯穿槽Y4、非贯穿槽Y5和非贯穿槽Y6;其中,非贯穿槽X7位于第一探测器基板侧粘接面1的内边界,非贯穿槽X8位于第二探测器基板侧粘接面2的内边界,非贯穿槽Y3位于第三探测器基板侧粘接面3的内边界,非贯穿槽Y4位于第四探测器基板侧粘接面4的内边界,非贯穿槽Y5位于第一探测器基板侧粘接面1的中心位置,非贯穿槽Y6位于第二探测器基板侧粘接面2的中心位置。In the above-mentioned infrared focal plane support structure with thermal stress unloading function, the lower surface of the flat plate is provided with a non-penetrating groove X7, a non-penetrating groove X8, a non-penetrating groove Y3, a non-penetrating groove Y4, a non-penetrating groove Y5 and a non-penetrating groove Y6; The non-penetrating groove X7 is located on the inner boundary of the bonding surface 1 on the first detector substrate side, the non-penetrating groove X8 is located on the inner boundary of the bonding surface 2 on the second detector substrate side, and the non-penetrating groove Y3 is located on the third detector substrate. The inner boundary of the side bonding surface 3, the non-penetrating groove Y4 is located at the inner boundary of the bonding surface 4 on the fourth detector substrate side, the non-penetrating groove Y5 is located at the center of the bonding surface 1 on the first detector substrate side, and the non-penetrating groove Y5 is located at the center of the bonding surface 1 on the first detector substrate side. Y6 is located at the center of the bonding surface 2 on the substrate side of the second detector.
上述具有热应力卸载功能的红外焦面支撑结构中,平板开设有非贯穿槽Z1、非贯穿槽Z2、非贯穿槽Z3、非贯穿槽Z4;非贯穿槽Z1位于第三探测器基板侧粘接面3的左边界沿厚度方向1/3~1/2位置;非贯穿槽Z3位于第四探测器基板侧粘接面4的左边界沿厚度方向1/3~1/2位置;非贯穿槽Z2位于第三探测器基板侧粘接面3的右边界沿厚度方向1/3~1/2位置;非贯穿槽Z4位于第四探测器基板侧粘接面4的右边界沿厚度方向1/3~1/2位置。In the above infrared focal plane support structure with thermal stress unloading function, the flat plate is provided with a non-penetrating groove Z1, a non-penetrating groove Z2, a non-penetrating groove Z3, and a non-penetrating groove Z4; the non-penetrating groove Z1 is located on the side of the third detector substrate for bonding. The left boundary of the surface 3 is located at 1/3-1/2 along the thickness direction; the non-penetrating groove Z3 is located at the 1/3-1/2 position along the thickness direction of the left boundary of the bonding surface 4 on the substrate side of the fourth detector; the non-penetrating groove Z2 is located at 1/3-1/2 of the right boundary of the bonding surface 3 on the third detector substrate side along the thickness direction; the non-penetrating groove Z4 is located at the right boundary of the bonding surface 4 on the fourth detector substrate side along the thickness direction 1/3 3 to 1/2 position.
上述具有热应力卸载功能的红外焦面支撑结构中,坐标系以平板下表面的长边和短边交点为原点,长边为X向,短边为Y向,厚度方向为Z向。In the above infrared focal plane support structure with thermal stress unloading function, the coordinate system takes the intersection of the long side and the short side of the lower surface of the flat plate as the origin, the long side is the X direction, the short side is the Y direction, and the thickness direction is the Z direction.
本发明与现有技术相比具有如下有益效果:Compared with the prior art, the present invention has the following beneficial effects:
1)本发明通过X向、Y向、Z向三种卸载槽,将红外焦面处所受的热应力充分卸载,保证了成像质量;1) The present invention fully unloads the thermal stress at the infrared focal plane through three unloading grooves in the X, Y, and Z directions to ensure the imaging quality;
2)本发明通过柔性传热丝组成的柔性传热区域,将制冷机的冷量充分传递到探测器,保证了探测器成像的环境温度及温度的均匀传输,同时柔性结构不会造成应力集中。2) The present invention fully transmits the cooling capacity of the refrigerator to the detector through the flexible heat transfer area composed of the flexible heat transfer wire, which ensures the uniform transmission of the ambient temperature and temperature imaged by the detector, and at the same time, the flexible structure does not cause stress concentration. .
附图说明Description of drawings
通过阅读下文优选实施方式的详细描述,各种其他的优点和益处对于本领域普通技术人员将变得清楚明了。附图仅用于示出优选实施方式的目的,而并不认为是对本发明的限制。而且在整个附图中,用相同的参考符号表示相同的部件。在附图中:Various other advantages and benefits will become apparent to those of ordinary skill in the art upon reading the following detailed description of the preferred embodiments. The drawings are for the purpose of illustrating preferred embodiments only and are not to be considered limiting of the invention. Also, the same components are denoted by the same reference numerals throughout the drawings. In the attached image:
图1是本发明实施例提供的具有热应力卸载功能的红外焦面支撑结构的截面图;1 is a cross-sectional view of an infrared focal plane support structure with thermal stress unloading function provided by an embodiment of the present invention;
图2是本发明实施例提供的具有热应力卸载功能的红外焦面支撑结构的爆炸图;2 is an exploded view of an infrared focal plane support structure with thermal stress unloading function provided by an embodiment of the present invention;
图3是本发明实施例提供的支撑结构的示意图;3 is a schematic diagram of a support structure provided by an embodiment of the present invention;
图4是本发明实施例提供的支撑结构的另一示意图;4 is another schematic diagram of a support structure provided by an embodiment of the present invention;
图5是本发明实施例提供的支撑结构的又一示意图;5 is another schematic diagram of a support structure provided by an embodiment of the present invention;
图6是本发明实施例提供的支撑结构仿真结果示意图。FIG. 6 is a schematic diagram of a simulation result of a support structure provided by an embodiment of the present invention.
具体实施方式Detailed ways
下面将参照附图更详细地描述本公开的示例性实施例。虽然附图中显示了本公开的示例性实施例,然而应当理解,可以以各种形式实现本公开而不应被这里阐述的实施例所限制。相反,提供这些实施例是为了能够更透彻地理解本公开,并且能够将本公开的范围完整的传达给本领域的技术人员。需要说明的是,在不冲突的情况下,本发明中的实施例及实施例中的特征可以相互组合。下面将参考附图并结合实施例来详细说明本发明。Exemplary embodiments of the present disclosure will be described in more detail below with reference to the accompanying drawings. While exemplary embodiments of the present disclosure are shown in the drawings, it should be understood that the present disclosure may be embodied in various forms and should not be limited by the embodiments set forth herein. Rather, these embodiments are provided so that the present disclosure will be more thoroughly understood, and will fully convey the scope of the present disclosure to those skilled in the art. It should be noted that the embodiments of the present invention and the features of the embodiments may be combined with each other under the condition of no conflict. The present invention will be described in detail below with reference to the accompanying drawings and in conjunction with the embodiments.
图1是本发明实施例提供的具有热应力卸载功能的红外焦面支撑结构的截面图。图2是本发明实施例提供的具有热应力卸载功能的红外焦面支撑结构的爆炸图。如图1和图2所示,该红外焦平面支撑结构,包括探测器读出电路100、基板200、支撑结构300、冷头400、冷指500和柔性卸载导热丝600;其中,FIG. 1 is a cross-sectional view of an infrared focal plane support structure with thermal stress unloading function provided by an embodiment of the present invention. FIG. 2 is an exploded view of an infrared focal plane support structure with thermal stress unloading function provided by an embodiment of the present invention. As shown in FIG. 1 and FIG. 2 , the infrared focal plane support structure includes a
所述探测器读出电路100粘接在基板200上;所述基板200粘接在所述支撑结构300上;所述支撑结构300安装在冷头400上;所述冷指500与所述冷头400相连接;所述柔性卸载导热丝600设置于所述支撑结构300内。The
图3是本发明实施例提供的支撑结构的示意图。如图3所示,支撑结构300为平板,其中,平板的下表面设置有H型冷指粘接面;平板的上表面设置有第一探测器基板侧粘接面1、第二探测器基板侧粘接面2、第三探测器基板侧粘接面3、第四探测器基板侧粘接面4和柔性传热区域;其中,第一探测器基板侧粘接面1和第二探测器基板侧粘接面2相对,第一探测器基板侧粘接面1和第二探测器基板侧粘接面2均位于平板的上表面的外边缘;第三探测器基板侧粘接面3和第四探测器基板侧粘接面4相对,第三探测器基板侧粘接面3和第四探测器基板侧粘接面4均位于平板的上表面的外边缘;柔性传热区域位于平板的上表面的中间位置,柔性卸载导热丝600设置于柔性传热区域。FIG. 3 is a schematic diagram of a support structure provided by an embodiment of the present invention. As shown in FIG. 3 , the
如图3所示,平板的上表面开设有贯穿槽X1、贯穿槽X2、贯穿槽X3、贯穿槽X4、非贯穿槽X5、非贯穿槽X6、非贯穿槽Y1和非贯穿槽Y2;其中,贯穿槽X1、贯穿槽X2、贯穿槽X3、贯穿槽X4、非贯穿槽X5、非贯穿槽X6、非贯穿槽Y1和非贯穿槽Y2位于H型冷指粘接面的边界位置处;非贯穿槽X5和非贯穿槽X6相对,非贯穿槽X5和非贯穿槽X6平行;贯穿槽X1和贯穿槽X2相对,贯穿槽X1和贯穿槽X2平行;贯穿槽X3和贯穿槽X4相对,贯穿槽X3和贯穿槽X4平行;非贯穿槽Y1和非贯穿槽Y2相对,非贯穿槽Y1和非贯穿槽Y2平行。贯穿槽X1、贯穿槽X2、贯穿槽X3、贯穿槽X4、非贯穿槽X5、非贯穿槽X6、非贯穿槽Y1和非贯穿槽Y2用于卸载X、Y向热应力。As shown in FIG. 3 , the upper surface of the flat plate is provided with through grooves X1, through grooves X2, through grooves X3, through grooves X4, non-through grooves X5, non-through grooves X6, non-through grooves Y1 and non-through grooves Y2; wherein, Through groove X1, through groove X2, through groove X3, through groove X4, non-through groove X5, non-through groove X6, non-through groove Y1 and non-through groove Y2 are located at the boundary position of the H-type cold finger bonding surface; The groove X5 is opposite to the non-penetrating groove X6, the non-penetrating groove X5 is parallel to the non-penetrating groove X6; the penetration groove X1 is opposite to the penetration groove X2, the penetration groove X1 is parallel to the penetration groove X2; the penetration groove X3 is opposite to the penetration groove X4, and the penetration groove X3 It is parallel to the through groove X4; the non-penetrating groove Y1 and the non-penetrating groove Y2 are opposite, and the non-penetrating groove Y1 and the non-penetrating groove Y2 are parallel. The penetrating groove X1, the penetrating groove X2, the penetrating groove X3, the penetrating groove X4, the non-penetrating groove X5, the non-penetrating groove X6, the non-penetrating groove Y1 and the non-penetrating groove Y2 are used to relieve the thermal stress in the X and Y directions.
如图5所示,平板的下表面开设有非贯穿槽X7、非贯穿槽X8、非贯穿槽Y3、非贯穿槽Y4、非贯穿槽Y5和非贯穿槽Y6;其中,非贯穿槽X7位于第一探测器基板侧粘接面1的内边界,非贯穿槽X8位于第二探测器基板侧粘接面2的内边界,非贯穿槽Y3位于第三探测器基板侧粘接面3的内边界,非贯穿槽Y4位于第四探测器基板侧粘接面4的内边界,非贯穿槽Y5位于第一探测器基板侧粘接面1的中心位置,非贯穿槽Y6位于第二探测器基板侧粘接面2的中心位置。非贯穿槽X7、非贯穿槽X8、非贯穿槽Y3、非贯穿槽Y4、非贯穿槽Y5和非贯穿槽Y6用于卸载X、Y向热应力。As shown in FIG. 5 , a non-penetrating groove X7, a non-penetrating groove X8, a non-penetrating groove Y3, a non-penetrating groove Y4, a non-penetrating groove Y5 and a non-penetrating groove Y6 are formed on the lower surface of the flat plate; A non-penetrating groove X8 is located at the inner boundary of the bonding surface 1 on the substrate side of the detector, and the non-penetrating groove Y3 is located at the inner boundary of the bonding surface 3 on the substrate side of the third detector. , the non-penetrating groove Y4 is located at the inner boundary of the bonding surface 4 on the fourth detector substrate side, the non-penetrating groove Y5 is located at the center of the bonding surface 1 on the first detector substrate side, and the non-penetrating groove Y6 is located on the second detector substrate side The center position of the bonding surface 2. The non-penetrating groove X7, the non-penetrating groove X8, the non-penetrating groove Y3, the non-penetrating groove Y4, the non-penetrating groove Y5 and the non-penetrating groove Y6 are used to relieve the thermal stress in the X and Y directions.
图4是本发明实施例提供的支撑结构的另一示意图。如图4所示,平板开设有非贯穿槽Z1、非贯穿槽Z2、非贯穿槽Z3和非贯穿槽Z4;非贯穿槽Z1位于第三探测器基板侧粘接面3的左边界沿厚度方向1/3~1/2位置;非贯穿槽Z3位于第四探测器基板侧粘接面4的左边界沿厚度方向1/3~1/2位置;非贯穿槽Z2位于第三探测器基板侧粘接面3的右边界沿厚度方向1/3~1/2位置;非贯穿槽Z4位于第四探测器基板侧粘接面4的右边界沿厚度方向1/3~1/2位置。非贯穿槽Z1、非贯穿槽Z2、非贯穿槽Z3、非贯穿槽Z4用于卸载Z向热应力。FIG. 4 is another schematic diagram of a support structure provided by an embodiment of the present invention. As shown in FIG. 4 , the flat plate is provided with a non-penetrating groove Z1, a non-penetrating groove Z2, a non-penetrating groove Z3 and a non-penetrating groove Z4; the non-penetrating groove Z1 is located on the left boundary of the bonding surface 3 on the substrate side of the third detector along the thickness direction 1/3~1/2 position; non-penetrating groove Z3 is located at 1/3~1/2 position along the thickness direction of the left boundary of the bonding surface 4 on the fourth detector substrate side; non-penetrating groove Z2 is located on the third detector substrate side The right boundary of the bonding surface 3 is located at 1/3-1/2 position along the thickness direction; the non-penetrating groove Z4 is located at 1/3-1/2 position along the thickness direction of the right boundary of the bonding surface 4 on the fourth detector substrate side. The non-penetrating groove Z1, the non-penetrating groove Z2, the non-penetrating groove Z3, and the non-penetrating groove Z4 are used to relieve the thermal stress in the Z direction.
坐标系以平板下表面(冷头粘接面侧)长边和短边交点为原点,长边为X向,短边为Y向,厚度方向为Z向The coordinate system takes the intersection of the long side and the short side of the lower surface of the plate (the side of the cold head bonding surface) as the origin, the long side is the X direction, the short side is the Y direction, and the thickness direction is the Z direction
红外焦平面支撑结构的工作原理如下:在降温的过程中,冷头与支撑结构采用相同材料(钼铜、紫铜等材料),热膨胀系数比基板大,将产生上凸形变。将上凸应力分解成X、Y、Z三个方向的力,每个方向的力均设置应力卸载槽,同时在槽根部的应力集中区域设计应力卸载圆角。由通过支撑结构,中部热应力在中间凹槽处被卸载;四周下凹部分的热应力由环形卸载槽卸载。基板本身具有较高的硬度,也可改善硅片粘接面的变形。The working principle of the infrared focal plane support structure is as follows: in the process of cooling, the cold head and the support structure are made of the same material (molybdenum copper, copper and other materials), and the thermal expansion coefficient is larger than that of the substrate, which will cause convex deformation. The upward convex stress is decomposed into forces in three directions of X, Y, and Z. A stress relief groove is set for each direction of force, and a stress relief fillet is designed in the stress concentration area at the root of the groove. By passing through the support structure, the thermal stress in the middle is unloaded at the middle groove; the thermal stress on the concave part around it is unloaded by the annular unloading groove. The substrate itself has high hardness, which can also improve the deformation of the bonding surface of the silicon wafer.
另外,冷指在降温的过程中,一方面会产生机械振动或压力气体波动,振动将随着冷指传递到探测器焦面,严重时将影响焦面的成像质量。本发明中的支撑结构延长了振动的传递路径,从而降低了探测器处的振动;另一方面,支撑结构与基板接触面积较小将不利于冷量的传递。支撑结构中心凹槽中粘接了阻尼特性较好、导热系数较高的细丝结构(可选用铜箔、铜丝、铟丝等材料),有效减小了热阻,从而确保有足够的接触面积来传递冷量。In addition, in the process of cooling the cold finger, on the one hand, mechanical vibration or pressure gas fluctuation will be generated, and the vibration will be transmitted to the focal plane of the detector along with the cold finger, which will affect the imaging quality of the focal plane in severe cases. The support structure in the present invention prolongs the transmission path of the vibration, thereby reducing the vibration at the detector; on the other hand, the small contact area between the support structure and the substrate is not conducive to the transmission of cooling energy. A filament structure with good damping characteristics and high thermal conductivity (copper foil, copper wire, indium wire and other materials can be selected) is bonded to the central groove of the support structure, which effectively reduces the thermal resistance and ensures sufficient contact area to transfer cooling.
运用Patran软件对支撑结构进行仿真分析,结果如图6所示。应力集中区域在四角无约束区域(冷指侧),耦合基板的应力较小,且应力分布均匀,未出现较大的应力集中。其中,中心区域为探测器芯片的粘接位置,由仿真结果可以看出,往中心方向的应力逐渐减小,直接作用在器件上的力较小,达到了应力卸载的目的。The support structure is simulated and analyzed by Patran software, and the results are shown in Figure 6. The stress concentration area is in the unconstrained area at the four corners (cold finger side), the stress of the coupling substrate is small, and the stress distribution is uniform, and there is no large stress concentration. Among them, the central area is the bonding position of the detector chip. It can be seen from the simulation results that the stress in the direction of the center gradually decreases, and the force directly acting on the device is small, which achieves the purpose of stress unloading.
本发明通过X向、Y向、Z向三种卸载槽,将红外焦面处所受的热应力充分卸载,保证了成像质量;本发明通过柔性传热丝组成的柔性传热区域,将制冷机的冷量充分传递到探测器,保证了探测器成像的环境温度及温度的均匀传输,同时柔性结构不会造成应力集中。The present invention fully unloads the thermal stress on the infrared focal plane through three unloading grooves of X, Y and Z directions to ensure imaging quality; The cooling energy of the machine is fully transmitted to the detector, which ensures the uniform transmission of the ambient temperature and temperature imaged by the detector, and the flexible structure will not cause stress concentration.
本发明虽然已以较佳实施例公开如上,但其并不是用来限定本发明,任何本领域技术人员在不脱离本发明的精神和范围内,都可以利用上述揭示的方法和技术内容对本发明技术方案做出可能的变动和修改,因此,凡是未脱离本发明技术方案的内容,依据本发明的技术实质对以上实施例所作的任何简单修改、等同变化及修饰,均属于本发明技术方案的保护范围。Although the present invention has been disclosed above with preferred embodiments, it is not intended to limit the present invention. Any person skilled in the art can use the methods and technical contents disclosed above to improve the present invention without departing from the spirit and scope of the present invention. The technical solutions are subject to possible changes and modifications. Therefore, any simple modifications, equivalent changes and modifications made to the above embodiments according to the technical essence of the present invention without departing from the content of the technical solutions of the present invention belong to the technical solutions of the present invention. protected range.
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