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CN101750143B - Integrated optical interference three-dimensional vibration monitor - Google Patents

Integrated optical interference three-dimensional vibration monitor Download PDF

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CN101750143B
CN101750143B CN2010100228594A CN201010022859A CN101750143B CN 101750143 B CN101750143 B CN 101750143B CN 2010100228594 A CN2010100228594 A CN 2010100228594A CN 201010022859 A CN201010022859 A CN 201010022859A CN 101750143 B CN101750143 B CN 101750143B
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light
lens
laser
vibration
prism
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CN101750143A (en
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张雪洁
黄伟
杨朋千
冯滔
孙明营
张燕
朱健强
刘德安
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Shanghai Institute of Optics and Fine Mechanics of CAS
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Abstract

一种集成式光学干涉三维振动监测仪,包括激光器,沿该激光器输出光束的前进方向依次是同光轴的第一透镜、分光棱镜、光阑和测量反射镜,所述的测量反射镜固定在待监测物体的表面上,在该分光棱镜的相干光输出面外依次是第二透镜、第三透镜和光电探测器并构成探测系统。本发明将光路主要部分集成于单块分光棱镜中,结构简单,稳定可靠。另外,进行干涉的两列波都源自于激光器发出的经过透镜之后的发散光,因此均为球面波,可以实现区分被测物体振动与测量光路振动的光学干涉的三维监测。

Figure 201010022859

An integrated optical interference three-dimensional vibration monitor includes a laser, and along the forward direction of the laser output light beam are a first lens, a beam splitter, an aperture and a measuring reflector on the same optical axis in sequence. The measuring reflector is fixed on the surface of the object to be monitored, and outside the coherent light output surface of the beam splitter prism are a second lens, a third lens and a photodetector in sequence to form a detection system. The present invention integrates the main part of the optical path into a single beam splitter prism, and has a simple structure, stable and reliable. In addition, the two waves that interfere are both derived from the divergent light emitted by the laser after passing through the lens, and are therefore both spherical waves, which can realize three-dimensional monitoring of optical interference that distinguishes the vibration of the object to be measured from the vibration of the measuring light path.

Figure 201010022859

Description

集成式光学干涉三维振动监测仪 Integrated optical interference three-dimensional vibration monitor

技术领域technical field

本发明涉及动监测仪,特别是一种集成式光学干涉三维振动监测仪。The invention relates to a motion monitor, in particular to an integrated optical interference three-dimensional vibration monitor.

背景技术Background technique

机械结构的低频振动普遍具有衰减慢、振幅大和难隔振等特点。在大型光学精密机械平台中,低频振动通过光学元件会对在其中传播的光束产生不可忽略的影响,因此有效监测光学平台的振动是非常重要的。The low-frequency vibration of mechanical structures generally has the characteristics of slow attenuation, large amplitude and difficult vibration isolation. In a large-scale optical precision mechanical platform, low-frequency vibration passing through optical components will have a non-negligible impact on the beam propagating in it, so it is very important to effectively monitor the vibration of the optical platform.

传统的光学干涉测量方法,都是采用双光束干涉,其中一束作为参考光,另外一束作为测量光,通过光电探测器检测干涉条纹的变化,来反映物体的振动状况。如“机械振动测量的激光干涉技术原理及其应用”一文中提到的测量方法,一方面进行干涉的两列波均为平面波,只能反映物体振动的二维信息,不能有效反映物体的三维振动;另一方面在测量过程中,没有采取对激光束锁定等措施,这样可能会由于光路本身的振动使干涉条纹发生变化,从而影响对被测物体的监测的干扰,也就是说不能有效地区分被测物体的振动和监测光路的振动。The traditional optical interferometry method uses two-beam interference, one of which is used as a reference beam, and the other is used as a measurement beam. The change of interference fringes is detected by a photodetector to reflect the vibration of the object. For example, the measurement method mentioned in the article "Laser Interferometry Technology Principle and Application of Mechanical Vibration Measurement", on the one hand, the two waves for interference are plane waves, which can only reflect the two-dimensional information of the vibration of the object, and cannot effectively reflect the three-dimensional information of the object Vibration; on the other hand, during the measurement process, no measures such as locking the laser beam are taken, which may cause interference fringes to change due to the vibration of the optical path itself, thereby affecting the interference to the monitoring of the measured object, that is to say, the effective area cannot be Divide the vibration of the measured object and monitor the vibration of the optical path.

因此,若要实现实用性的测量,有两方面需要注意:一方面要实现振动分离,目前还没有好的方案;另一方面要实现对物体振动的三维监测,现在通常都是采用多个平台进行测量,相对而言比较复杂,不实用,如在文献“带有三维激光干涉仪和压电位移执行器的新型主动隔离系统”中提到的方法。Therefore, in order to achieve practical measurement, there are two aspects that need to be paid attention to: on the one hand, there is no good solution to achieve vibration separation; on the other hand, to achieve three-dimensional monitoring of object vibration, multiple platforms are usually used now It is relatively complex and impractical to carry out measurements, such as the method mentioned in the paper "Novel Active Isolation System with 3D Laser Interferometer and Piezoelectric Displacement Actuator".

发明内容Contents of the invention

本发明的目的在于克服上述现有技术的不足,提供一种集成式光学干涉三维振动监测仪,该监测仪可以实现区分被测物体振动与测量光路振动的光学干涉的三维监测。The purpose of the present invention is to overcome the shortcomings of the above-mentioned prior art, and provide an integrated optical interference three-dimensional vibration monitor, which can realize three-dimensional monitoring of optical interference that distinguishes between the vibration of the measured object and the vibration of the measurement optical path.

本发明的技术解决方案如下:Technical solution of the present invention is as follows:

一种集成式光学干涉三维振动监测仪,包括激光器,沿该激光器输出光束的前进方向依次是同光轴的第一透镜、分光棱镜、光阑、测量反射镜,所述的测量反射镜固定在待监测物体的表面上,所述的分光棱镜的分光面与所述的光轴的夹角为45°,该分光棱镜的分光面将从入射面输入的激光束分为反射光和透射光,该分光棱镜中与所述的入射面相对的一面的外围镀有全反膜,中间留有通光孔,所述的透射光中通过通光孔和光阑并直射所述的测量反射镜的光束为探测光束,该分光棱镜的反射面镀有全反膜,所述的反射光经所述的反射面反射后称为参考光束,与所述的反射面相对的一面是相干光输出面,在该分光棱镜的相干光输出面外依次是第二透镜、第三透镜和光电探测器并构成探测系统。An integrated optical interference three-dimensional vibration monitor, including a laser, along the forward direction of the output beam of the laser is a first lens with the same optical axis, a beam splitting prism, a diaphragm, and a measuring reflector, and the measuring reflector is fixed on On the surface of the object to be monitored, the angle between the beam-splitting surface of the beam-splitting prism and the optical axis is 45°, and the beam-splitting surface of the beam-splitting prism divides the laser beam input from the incident surface into reflected light and transmitted light, In the dichroic prism, the periphery of the side opposite to the incident surface is coated with a total reflection film, and a light hole is left in the middle, and the beam of the transmitted light passes through the light hole and the diaphragm and directly hits the measuring reflector In order to detect the light beam, the reflective surface of the dichroic prism is coated with a total reflection film. The reflected light is called the reference beam after being reflected by the reflective surface, and the side opposite to the reflective surface is the coherent light output surface. The coherent light output surface of the dichroic prism is followed by a second lens, a third lens and a photodetector to form a detection system.

激光器发出的光经过第一透镜之后,以发散光的形式入射到分光棱镜上,经分光面将入射光线分成两束:反射光和透射光。其中反射光束作为参考光,被镀有全反膜的侧面反射后,直接回到分光面。而透射光则又分成了两部分:After passing through the first lens, the light emitted by the laser is incident on the beam splitting prism in the form of divergent light, and the incident light is divided into two beams by the beam splitting surface: reflected light and transmitted light. The reflected light beam is used as the reference light, and after being reflected by the side coated with the total reflection film, it returns directly to the splitting surface. The transmitted light is further divided into two parts:

位于外围的光束受这一侧面四周所镀反射膜的影响,直接反射回分光面,与参考光束会合之后,通过两个透镜进行缩束,最后照射到光电探测器上,形成外环干涉条纹;而位于内圈的光束则通过中间的通光孔以及光阑之后,被测量反射镜反射,然后同样返回到分光面,与参考光束的中间部分进行干涉,在光电探测器上形成内环条纹。The light beam located at the periphery is affected by the reflective film coated around this side, and is directly reflected back to the splitter surface. After meeting with the reference beam, the light beam is shrunk through two lenses, and finally irradiated on the photodetector to form outer ring interference fringes; The beam located in the inner ring passes through the middle aperture and the diaphragm, is reflected by the measuring mirror, and then returns to the beam splitting surface, and interferes with the middle part of the reference beam to form an inner ring fringe on the photodetector.

本发明与现有技术相比所具有的优点和效果是,光路本身的监测与被测物体的监测两者相互独立。外环的干涉条纹是由分光棱镜本身两个侧面的反射光干涉形成的,并不包含任何被测物体的信息,因此只反映了光路本身的信息。如果外环条纹发生了变化,则说明测量光路振动了。而内环的干涉条纹由于是由从测量反射镜返回的光和参考光干涉形成的,因此可以反映物体的振动状况。由于测量光路的变化也会引起内环的变化,因此在外环、内环同时变化的情况下,内环条纹的变化并不能正确反映被测物体的振动情况。只有在保证测量光路不动,即外环条纹没有变化的情况下,内环条纹的变化才能完全反映被测物体的振动。同时,本发明将主要光路集成于单块分光棱镜中,结构简单,稳定可靠。另外,进行干涉的两列波都源自于激光器发出的经过透镜之后的发散光,因此均为球面波,可以实现区分被测物体振动与测量光路振动的光学干涉的三维监测。Compared with the prior art, the present invention has the advantages and effects that the monitoring of the optical path itself and the monitoring of the measured object are independent of each other. The interference fringes in the outer ring are formed by the interference of reflected light from the two sides of the beam splitting prism itself, and do not contain any information of the measured object, so it only reflects the information of the optical path itself. If the outer ring fringes change, it means that the measurement optical path is vibrating. The interference fringes of the inner ring are formed by the interference of the light returned from the measuring mirror and the reference light, so it can reflect the vibration condition of the object. Since the change of the measurement optical path will also cause the change of the inner ring, the change of the inner ring stripes cannot correctly reflect the vibration of the measured object when the outer ring and the inner ring change at the same time. Only when the measurement optical path is kept still, that is, the outer ring fringe does not change, can the change of the inner ring fringe completely reflect the vibration of the measured object. Simultaneously, the present invention integrates the main optical path into a single beam splitting prism, which has a simple structure, is stable and reliable. In addition, the two interfering waves are both derived from the divergent light emitted by the laser after passing through the lens, so they are both spherical waves, which can realize three-dimensional monitoring of optical interference that distinguishes between the vibration of the measured object and the vibration of the measurement optical path.

附图说明Description of drawings

图1是本发明的装置示意图;Fig. 1 is a device schematic diagram of the present invention;

图2是本发明实施例的光路示意图;Fig. 2 is the optical path schematic diagram of the embodiment of the present invention;

图3是本发明三维监测原理图。Fig. 3 is a principle diagram of the three-dimensional monitoring of the present invention.

具体实施方式Detailed ways

下面结合附图和实施例对本发明作进一步说明。The present invention will be further described below in conjunction with drawings and embodiments.

由图1可见,本发明集成式光学干涉三维振动监测仪,包括激光器1,特征在于,沿该激光器1输出光束的前进方向依次是同光轴的第一透镜2、分光棱镜3、光阑8和测量反射镜9,所述的测量反射镜9固定在待监测物体10的表面上,所述的分光棱镜3的分光面与所述的光轴的夹角为45°,该分光棱镜3的分光面将从入射面输入的激光束分为反射光和透射光,该分光棱镜3中与所述的入射面相对的一面的外围镀有全反膜5、7,中间留有通光孔6,所述的透射光中通过通光孔6和光阑8并直射所述的测量反射镜9的光束为探测光束,该分光棱镜3的反射面4镀有全反膜,所述的反射光经所述的反射面4反射后称为参考光束,与所述的反射面4相对的一面是相干光输出面,在该分光棱镜3的相干光输出面外依次是第二透镜11、第三透镜12和光电探测器13并构成探测系统。It can be seen from Fig. 1 that the integrated optical interference three-dimensional vibration monitor of the present invention includes a laser 1, and is characterized in that along the advancing direction of the output beam of the laser 1, there are successively a first lens 2, a dichroic prism 3, and an aperture 8 on the same optical axis. And measuring reflector 9, described measuring reflector 9 is fixed on the surface of object 10 to be monitored, and the included angle between the beam-splitting surface of described beam-splitting prism 3 and described optical axis is 45 °, and the angle of this beam-splitting prism 3 The beam splitting surface divides the laser beam input from the incident surface into reflected light and transmitted light. The periphery of the side opposite to the incident surface in the beam splitting prism 3 is coated with a total reflection film 5, 7, and a light hole 6 is left in the middle. , the light beam that passes through the light hole 6 and the diaphragm 8 and directly hits the measuring mirror 9 in the transmitted light is the detection beam, and the reflective surface 4 of the dichroic prism 3 is coated with a total reflection film, and the reflected light is passed through The reflection of the reflective surface 4 is referred to as a reference beam, and the side opposite to the reflective surface 4 is a coherent light output surface. Outside the coherent light output surface of the dichroic prism 3 are the second lens 11 and the third lens in sequence. 12 and photodetector 13 and constitute a detection system.

下面结合图2对本发明的具体监测方法进行说明。在本实施例中,所述的激光器1为He-Ne激光器。The specific monitoring method of the present invention will be described below in conjunction with FIG. 2 . In this embodiment, the laser 1 is a He-Ne laser.

激光器1发出的光经过第一透镜2之后,以一束发散光束的形式照射在分光棱镜3的入射面上。该分光棱镜3通过分光面将入射光分成反射光和透射光两部分。The light emitted by the laser 1 passes through the first lens 2 and then irradiates the incident surface of the dichroic prism 3 in the form of a divergent light beam. The dichroic prism 3 splits the incident light into reflected light and transmitted light through the dichroic surface.

其中反射光部分,即光线16与17之间的光束,经过分光棱镜3的全反面4的反射后,直接到达干涉区域。这部分光作为参考光,存在于光线18与19之间。Wherein the reflected light part, that is, the light beam between the light rays 16 and 17 , after being reflected by the total negative surface 4 of the dichroic prism 3 , directly reaches the interference area. This portion of light exists between rays 18 and 19 as reference light.

透射光部分又可分为两部分:The transmitted light part can be divided into two parts:

其中位于外围的光束,即光线14与20之间的以及15与23之间的光束,经过全反膜5和7的反射后,又经光棱镜3的分光面的反射也直接到达干涉区域。这部分光,存在于光线24与25之间以及28与29之间,与参考光进行干涉,形成外环干涉条纹,用于监测光路本身的振动。Wherein the light beams located in the periphery, that is, the light beams between the light rays 14 and 20 and the light beams between 15 and 23, after being reflected by the total reflection films 5 and 7, are reflected by the light splitting surface of the optical prism 3 and directly reach the interference area. This part of the light, which exists between the light rays 24 and 25 and between 28 and 29, interferes with the reference light to form outer ring interference fringes, which are used to monitor the vibration of the light path itself.

另一部分透射光,即位于内圈的透射光,即光线21与22之间的光,则通过通光孔6和光阑8之后,到达测量反射镜9,然后反射回所述的分光棱镜3,经分光棱镜3的分光面的反射后与参考光束会合后到达干涉区域,形成测量光束。这部分光位于光线26与27之间,同样与参考光进行干涉,形成内圈干涉条纹,用于监测被测物体的振动。值得注意的是,位于光线20与21之间的光束以及光线22与23之间的光束,部分因为光阑8的表面为漫反射面,光束进行了漫反射,部分经过测量反射镜9反射之后被光阑8挡住,都并没有反射回光电探测器13,如光线30所示。这样在内圈干涉条纹和外环干涉条纹之间就会形成部分空白,即光线26与25以及27与28之间的部分,从而可以清楚的分辨开两部分干涉条纹。The other part of the transmitted light, that is, the transmitted light located in the inner ring, that is, the light between the light rays 21 and 22, passes through the aperture 6 and the aperture 8, then reaches the measuring reflector 9, and then reflects back to the dichroic prism 3, After being reflected by the beam-splitting surface of the beam-splitting prism 3, it meets the reference beam and reaches the interference area to form a measuring beam. This part of light is located between the light rays 26 and 27 and also interferes with the reference light to form inner interference fringes for monitoring the vibration of the measured object. It is worth noting that the light beams located between the light rays 20 and 21 and the light beams between the light rays 22 and 23 are partly because the surface of the aperture 8 is a diffuse reflection surface, and the light beams are diffusely reflected, and partly after being reflected by the measuring mirror 9 Blocked by the diaphragm 8, they are not reflected back to the photodetector 13, as shown by the ray 30. In this way, a part of blanks will be formed between the inner ring interference fringes and the outer ring interference fringes, that is, the part between the light rays 26 and 25 and 27 and 28, so that the two parts of the interference fringes can be clearly distinguished.

由图2可知,进行干涉的两列波均为球面波,因此可以实现三维监测。下面对此原理进行简单说明。It can be seen from Figure 2 that the two waves interfering are spherical waves, so three-dimensional monitoring can be realized. A brief description of this principle is given below.

对于球面波而言,z=0平面的位相函数为:For spherical waves, the phase function of the z=0 plane is:

Figure G2010100228594D00041
Figure G2010100228594D00041

其中(xo,yo,zo)为球面波的中心位置,令

Figure G2010100228594D00042
(1)式可化简为:where (x o , y o , z o ) is the center position of the spherical wave, let
Figure G2010100228594D00042
(1) can be simplified as:

Figure G2010100228594D00043
Figure G2010100228594D00043

当方括号中含1/lo 2的项小于1时,用二项式定理展开(2)式,并在菲涅耳近似的条件下,忽略1/lo 3以上的项,可得:When the items containing 1/l o 2 in the square brackets are less than 1, use the binomial theorem to expand the formula (2), and under the condition of Fresnel approximation, ignore the items above 1/l o 3 , we can get:

Figure G2010100228594D00044
Figure G2010100228594D00044

在本发明中,在光电探测器13上进行干涉的两列球面波都是由位于光线14与15之间的光经过一系列反射形成的。因此,可以认为存在等效的虚拟光源,干涉条纹是由它们发出的球面波形成的,虚拟光源的位置可以通过反射定理求出。In the present invention, the two columns of spherical waves interfering on the photodetector 13 are formed by a series of reflections of the light between the light rays 14 and 15 . Therefore, it can be considered that there are equivalent virtual light sources, the interference fringes are formed by the spherical waves emitted by them, and the position of the virtual light source can be obtained by the reflection theorem.

假设参考光波和测量光波虚拟光源的位置分别为(xR,yR,zR),(xo,yo,zo),类似地,它们在探测面上的位相函数可以写成:Assuming that the positions of the reference light wave and the virtual light source of the measurement light wave are (x R , y R , z R ), (x o , y o , z o ), similarly, their phase functions on the detection surface can be written as:

Figure G2010100228594D00045
Figure G2010100228594D00045

Figure G2010100228594D00046
Figure G2010100228594D00046

从而,可以得出光程差函数为:Thus, the optical path difference function can be obtained as:

ΔΔ == (( xx 22 ++ ythe y 22 )) (( 11 22 ll oo -- 11 22 ll RR )) -- xx (( xx oo ll oo -- xx RR ll RR )) -- ythe y (( ythe y oo ll oo -- ythe y RR ll RR )) -- -- -- (( 66 ))

因为峰值强度位置处的光程差Δ=nλ,(n=0,±1,±2,…),代入(6)式,可以在一级近似下求出条纹方程为:Because the optical path difference Δ=nλ at the peak intensity position, (n=0, ±1, ±2,...), substituting into (6) formula, the fringe equation can be obtained under the first-order approximation as:

xx 22 ++ ythe y 22 -- 22 xx ll RR xx oo -- ll oo xx RR ll RR -- ll oo -- 22 ythe y ll RR ythe y oo -- ll oo ythe y RR ll RR -- ll oo -- 22 nλnλ ll oo ll RR ll RR -- ll oo == 00 -- -- -- (( 77 ))

再次说明了干涉条纹为一族同心圆,圆心坐标为:Again, it shows that the interference fringes are a family of concentric circles, and the coordinates of the center of the circle are:

xx ′′ == ll RR xx oo -- ll oo xx RR ll RR -- ll oo ythe y ′′ == ll RR ythe y oo -- ll oo ythe y RR ll RR -- ll oo -- -- -- (( 88 ))

条纹的曲率半径为:The radius of curvature of the stripes is:

rr == [[ (( ll RR xx oo -- ll oo xx RR ll RR -- ll oo )) 22 ++ (( ll RR ythe y oo -- ll oo ythe y RR ll RR -- ll oo )) 22 ++ 22 nλnλ ll oo ll RR ll RR -- ll oo ]] 11 // 22 .. -- -- -- (( 99 ))

当被测物体振动时,测量反射镜相应振动,引起测量光波发生变化,这也就相当于改变了虚拟光源的位置。由(8)式和(9)式可以看出,最终引起干涉条纹的圆心位置和曲率半径改变。而且从图2可以看出,在被测物体10进行如图所示三个方向的振动时,无论哪个方向都会引起虚拟光源的位置改变,导致干涉条纹变化。正是利用这一点实现了平面波干涉所不能实现的三维监测。When the measured object vibrates, the measuring mirror vibrates accordingly, causing the measuring light wave to change, which is equivalent to changing the position of the virtual light source. It can be seen from formulas (8) and (9) that the center position and radius of curvature of the interference fringes will eventually change. Moreover, it can be seen from FIG. 2 that when the measured object 10 vibrates in three directions as shown in the figure, no matter which direction will cause the position of the virtual light source to change, resulting in changes in the interference fringes. It is by using this point that three-dimensional monitoring cannot be realized by plane wave interference.

如图3所示,假设R和O分别为参考光波和测量光波的虚拟光源,那么当被测物体10进行如图2所示三个方向的振动时,都会引起O点发生变化,而且其变化量最终都可以分解到图3所示的x,y,z三个方向上。As shown in Figure 3, assuming that R and O are the virtual light sources of the reference light wave and the measurement light wave respectively, then when the measured object 10 vibrates in three directions as shown in Figure 2, it will cause the point O to change, and its change Quantities can finally be decomposed into the three directions of x, y, and z shown in Figure 3.

根据(8)式和(9)式,当O沿z轴方向振动时,干涉条纹的中心不发生变化,只有曲率半径变化。也就是说当O沿z轴正向运动时,干涉条纹将进行收缩,而反向运动时,条纹则会发生扩张。同样分析可以得出:当O沿x(y)轴方向振动时,干涉条纹的中心也会沿x(y)轴方向振动,同时半径有微小变化。这样最终实现了对被测物体的三维监测。According to (8) and (9), when O vibrates along the z-axis direction, the center of the interference fringe does not change, only the radius of curvature changes. That is to say, when O moves in the positive direction along the z-axis, the interference fringes will shrink, and when O moves in the reverse direction, the fringes will expand. The same analysis shows that when O vibrates along the x(y) axis, the center of the interference fringes also vibrates along the x(y) axis, and the radius changes slightly. In this way, the three-dimensional monitoring of the measured object is finally realized.

由此可见,本发明实现了三维监测,以及光路监测与被测物体振动监测的分离,而且结构简单,采用单块集成式,稳定可靠。It can be seen that the present invention realizes three-dimensional monitoring and the separation of optical path monitoring and vibration monitoring of the measured object, and has a simple structure, adopts single-block integration, and is stable and reliable.

Claims (1)

1.一种集成式光学干涉三维振动监测仪,包括激光器(1),特征在于,沿该激光器(1)输出光束的前进方向依次是同光轴的第一透镜(2)、分光棱镜(3)、光阑(8)、测量反射镜(9),所述的测量反射镜(9)固定在待监测物体(10)的表面上,所述的分光棱镜(3)的分光面与所述的光轴的夹角为45°,该分光棱镜(3)的分光面将从入射面输入的激光束分为反射光和透射光,该分光棱镜(3)中与所述的入射面相对的一面的外围镀有全反膜(5、7),且所述的入射面相对的一面的中间留有通光孔(6),所述的透射光中通过通光孔(6)和光阑(8)并直射所述的测量反射镜(9)的光束为探测光束,该分光棱镜(3)的反射面(4)镀有全反膜,所述的反射光经所述的反射面(4)反射后称为参考光束,与所述的反射面(4)相对的一面是相干光输出面,在该分光棱镜(3)的相干光输出面外依次是第二透镜(11)、第三透镜(12)和光电探测器(13)并构成探测系统。1. An integrated optical interference three-dimensional vibration monitor, comprising a laser (1), is characterized in that, along the advancing direction of the laser (1) output light beam, the first lens (2) and the beam splitting prism (3) of the same optical axis are successively ), diaphragm (8), measuring reflector (9), described measuring reflector (9) is fixed on the surface of the object to be monitored (10), the splitting surface of the described beam splitting prism (3) and the described The included angle of the optical axis of the beam splitting prism (3) is 45 °, and the laser beam input from the incident surface is divided into reflected light and transmitted light by the beam splitting surface of the beam splitting prism (3). A total reflection film (5, 7) is coated on the periphery of one side, and a light hole (6) is left in the middle of the side opposite to the incident surface, and the transmitted light passes through the light hole (6) and the diaphragm ( 8) and the light beam that directly shines on the measuring reflector (9) is a detection beam, and the reflective surface (4) of the dichroic prism (3) is coated with a total reflection film, and the reflected light passes through the described reflective surface (4). ) is called the reference beam after reflection, and the side opposite to the reflective surface (4) is the coherent light output surface, and outside the coherent light output surface of the dichroic prism (3) are the second lens (11), the third The lens (12) and the photodetector (13) together constitute a detection system.
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