CN212658836U - Double-channel optical device for image acquisition - Google Patents
Double-channel optical device for image acquisition Download PDFInfo
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- CN212658836U CN212658836U CN202022188551.9U CN202022188551U CN212658836U CN 212658836 U CN212658836 U CN 212658836U CN 202022188551 U CN202022188551 U CN 202022188551U CN 212658836 U CN212658836 U CN 212658836U
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Abstract
The utility model discloses a double-channel optical device for image acquisition, which comprises a reflection mechanism and a double-channel imaging mechanism positioned on the reflection light path of the reflection mechanism, wherein visible light or infrared light enters the double-channel imaging mechanism through the reflection of the reflection mechanism; the reflecting mechanism comprises a reflecting mirror fixed on the reflecting frame through a rotating shaft, and an inclination angle exists between the reflecting mirror and the horizontal direction; the rotating shaft is connected with a driving motor through a transmission belt, and the transmission belt can drive the rotating shaft to change the inclination angle of the reflector and the horizontal direction; the dual-channel imaging mechanism comprises an infrared detection channel and a visible light detection channel which are parallel; an infrared detection optical assembly is arranged in the infrared detection channel, and a visible light detection optical assembly is arranged in the visible light detection channel. The utility model ensures the effect of stabilizing the visual axis in the inertial space through the reflecting mechanism; the imaging quality can be higher through a larger field of view under certain meteorological conditions; is suitable for the detection of infrared light and visible light in flight respectively or simultaneously.
Description
Technical Field
The utility model belongs to the technical field of the detector, a binary channels optical device for image acquisition is related to.
Background
In recent years, the application of infrared technology and unmanned aerial vehicles is developed vigorously, and the importance of the infrared technology and the unmanned aerial vehicles is increasingly prominent in the national economy field and national defense military. The infrared image mainly reflects thermal radiation information of the target. Objects of different temperatures have distinct characteristics in the infrared band, with lower temperatures being darker in color. The infrared optical system detects the self radiation of the target, and compared with a visible light optical system, the infrared optical system has the advantages of all-weather observation, no environmental influence and strong penetrating power. For example, the environment monitoring is carried out by adopting the unmanned aerial vehicle infrared and visible light synchronous remote sensing technology, and the drainage blind hole hidden in the grass on both banks of the river can be effectively checked. With the increasing application requirements, flight detection technology is required to include the requirement of complex environment stability and higher imaging precision.
SUMMERY OF THE UTILITY MODEL
The utility model provides a technical problem lie in providing a binary channels optical device for image acquisition, through the image acquisition mode of reflection + binary channels formation of image, can realize under the environment of complicacy in the flight that two kinds of high accuracy images of infrared, visible light are shot.
The utility model discloses a realize through following technical scheme:
a dual-channel optical device for image acquisition comprises a reflection mechanism and a dual-channel imaging mechanism positioned on a reflection light path of the reflection mechanism, wherein visible light or infrared light is reflected by the reflection mechanism to enter the dual-channel imaging mechanism;
the reflecting mechanism comprises a reflecting mirror fixed on the reflecting frame through a rotating shaft, and the inclination angle of the reflecting mirror to the horizontal direction is 40-60 degrees; the rotating shaft is connected with a driving motor through a transmission belt, and the transmission belt can drive the rotating shaft to change the inclination angle of the reflector and the horizontal direction;
the double-channel imaging mechanism comprises a detection frame, wherein an infrared detection channel and a visible light detection channel which are parallel are arranged on the detection frame; an infrared detection optical assembly is arranged in the infrared detection channel, and the infrared detector is positioned at an infrared imaging focus at the tail end of the infrared detection channel or on a light path of the infrared imaging focus reflected by the reflector group;
the visible light detection channel is internally provided with a visible light detection optical assembly, the visible light detector is fixed above the tail end outlet of the visible light detection optical assembly, and the center line of the visible light detection channel is vertical to the center of the detector target surface of the visible light detector.
The infrared detector is positioned at the tail end of the infrared detection channel, and the center line of the hollow infrared detection channel is aligned with the center of the detector target surface of the infrared detector; a plurality of objective lens fixing tables are arranged in the infrared detection channel, and objective lenses are fixed on a ring frame and are nested on the objective lens fixing tables through the ring frame;
the objective lens comprises a first objective lens, a second objective lens, a third objective lens and a fourth objective lens, wherein the first objective lens, the second objective lens and the third objective lens are sequentially arranged at the head of the infrared detection channel, and the fourth objective lens is arranged at the tail of the infrared detection channel; a space required by the rear intercept is reserved between the third objective and the fourth objective; the target surface of the detector is positioned at the imaging focal point of the fourth objective lens.
The infrared detector is fixed on the detection frame below the infrared detection channel and positioned on a reflection light path of the second infrared reflector.
The ring frame is nested in the infrared detection channel through threads, and matched threads are arranged on the objective lens fixing table and on the outer side of the ring frame;
the diameters of the ring frames for fixing the first objective lens, the second objective lens and the third objective lens are sequentially reduced, and the objective lens fixing tables for nesting the corresponding ring frames are sequentially arranged.
The first objective lens is used as a diaphragm for receiving light, and the space between the first objective lens and the infrared detection channel is sealed by sealant; the convex surface of the second objective lens is an aspheric surface so as to correct spherical aberration introduced by the first objective lens; the convex surface of the third objective lens is attached to the concave surface of the second objective lens so as to correct chromatic aberration; the convex surface of the fourth objective lens is an aspheric surface, and the back intercept distance between the third objective lens and the fourth objective lens can be adjusted by rotating the ring frame.
A light-gathering cavity and a reflecting cavity are arranged in the visible light detection channel, a right-angle reflecting prism is arranged in the reflecting cavity, and the visible light detector is fixed at an outlet of the reflecting cavity; a plurality of lens fixing tables are arranged in the light gathering cavity, and the lenses are fixed on the ring frame and are embedded on the lens fixing tables through the lens fixing tables;
the lenses comprise a first lens and a second lens which are sequentially arranged at the head of the light-gathering cavity, and a third lens, a fourth lens and a fifth lens which are arranged at the tail of the light-gathering cavity and are attached to each other; an aperture diaphragm is arranged between the second lens and the third lens; the target surface of the detector is in mirror symmetry with the imaging focal point of the fourth lens.
The first lens is a meniscus thin lens, and the second lens is a thick lens; the third lens is a cemented lens for correcting chromatic aberration, the fourth lens is a thick lens for correcting field curvature, and the fifth lens is a thin lens for correcting spherical aberration; changing the distance between the second lens and the fourth lens corrects astigmatism.
The first lens is a double-single lens or a plurality of single lenses, and an optical filter is arranged on the emergent surface of the right-angle reflecting prism; the right-angle reflecting prism is fixed with the side wall of the reflecting cavity through fixing glue; the optical filter is fixed with the emergent surface of the right-angle reflecting prism through fixing glue.
The inclination angle of the reflector to the horizontal direction is 45 degrees, and light rays horizontally enter the dual-channel imaging mechanism after being reflected by the reflector; when the dual-channel imaging mechanism deflects relative to the vertical direction, the driving motor drives the reflecting mirror to rotate through the driving transmission belt, and light rays are kept to enter the dual-channel imaging mechanism horizontally through reflection.
It is characterized in that the reflection frame is connected with the detection frame through a fixing pin;
the driving motor and the reflecting mirror are arranged on two parallel shafts of the reflecting frame, the transmission ratio between the driving shaft of the driving motor and the rotating shaft is 1/2, and the transmission belt is a steel belt.
Compared with the prior art, the utility model discloses following profitable technological effect has:
in order to keep the stability of image acquisition or shooting, the shooting is carried out in a very complex motion environment during the shooting in flight; the utility model discloses a reflecting mechanism realizes the inertial stability of looking the axle, and binary channels image device is fixed, realizes the stability of shooting the axle by the speculum rotation for the series picture of shooting is the straight line and arranges and non-S nature arranges, and such mode stably occupies littleer space than imaging mechanism' S platform formula. And the transmission ratio between the driving shaft of the driving motor and the rotating shaft is set to be 1/2, when the reflecting mechanism rotates relatively, the 1/2 transmission mechanism drives the reflecting mirror to rotate by half an angle, according to the geometrical optics principle of the reflecting mirror, incident light is fixed, the normal line of the reflecting mirror rotates by half, and emergent light rotates by one degree, so that the effect that the visual axis is kept stable in the inertial space is ensured.
The utility model provides a binary channels imaging mechanism has guaranteed the image quality, and wherein infrared optics objective adopts four chip type structures, and objective optical surface introduces the aspheric surface design and can reduce the F number moreover, improves the image quality at visual field border, can also make the senior spherical aberration of off-axis visual field and the senior spherical aberration in epaxial aperture reduce simultaneously, can obtain higher image quality under the condition in great visual field.
Furthermore, a small aperture diaphragm is inserted into the optical path of the lens of the visible light, namely the luminous flux can be obviously reduced through the small aperture diaphragm under the strong light environment, and the small aperture diaphragm exits the optical path again when the external light intensity is weakened, so that the weak light imaging effect is improved; the lens of the utility model tends to be symmetrical, and the vertical axis aberration of the symmetrical system is easy to be corrected, only the correction of spherical aberration, chromatic aberration, field curvature and astigmatism needs to be considered; the field curvature is corrected through the structural change of the thick lens of the rear half system, the spherical aberration is corrected by utilizing the curvature of the thin lens, the astigmatism can be corrected by changing the distance between the two thick lenses, and the chromatic aberration is corrected by introducing a gluing surface into the thick lens; therefore, the imaging quality within the range of 50-100000 lux can be considered, and higher imaging quality can be obtained through a larger view field under certain meteorological conditions; is suitable for the detection of infrared light and visible light in flight respectively or simultaneously.
Drawings
Fig. 1 is a schematic structural view of the present invention;
FIG. 2 is a schematic structural view of the reflection mechanism of the present invention;
FIG. 3 is a schematic structural view of a dual-channel imaging mechanism of the present invention;
FIG. 4 is a schematic view of the structure of the probing frame of the present invention;
FIG. 5 is a schematic view of a detection channel and its detection optics;
fig. 6 is a schematic diagram of an infrared optical assembly according to the present invention;
fig. 7 is a schematic structural view of the infrared module of the present invention;
FIG. 8 is a schematic view of a visible optical assembly of the present invention;
FIG. 9 is a schematic view of the structure of the visible components of the present invention;
fig. 10 is a schematic view of an infrared light path according to the present invention;
fig. 11 is a schematic view of the visible light path of the present invention.
Wherein, 10 is a reflection frame, 11 is a detection frame, 12 is a first infrared reflection mirror, 13 is a second infrared reflection mirror, 14 is an infrared detection optical component, and 15 is a visible light detection optical component; 16 is a reflector, 17 is a fixed pin, and 18 is a transmission belt; 101 is an infrared detection channel, and 102 is a visible light detection channel; 1401 is a first objective lens, 1402 is a second objective lens, 1403 is a third objective lens, 1404 is a fourth objective lens, 1405 is an infrared detector, 1406 is an infrared detection channel, 1407 is a coil frame, and 1408 is a detector target surface; 1501 is a first lens, 1502 is a second lens, 1503 is a third lens, 1504 is a fourth lens, 1505 is a fifth lens, 1506 is a visible light detector, 1507 is a filter, 1508 is a rectangular prism, and 1509 is an aperture stop.
Detailed Description
The present invention will be described in further detail with reference to the following examples, which are intended to be illustrative, but not limiting, of the present invention.
Referring to fig. 1 to 11, a dual-channel optical device for image acquisition includes a reflection mechanism and a dual-channel imaging mechanism located on a reflection optical path of the reflection mechanism, and visible light or infrared light is reflected by the reflection mechanism and enters the dual-channel imaging mechanism;
the reflecting mechanism comprises a reflecting mirror 16 fixed on the reflecting frame 10 through a rotating shaft, and the inclination angle of the reflecting mirror 16 and the horizontal direction is 40-60 degrees; the rotating shaft is connected with a driving motor through a transmission belt 18, and the transmission belt 18 can drive the rotating shaft to change the inclination angle of the reflector 16 with the horizontal direction;
the dual-channel imaging mechanism comprises a detection frame 11, wherein an infrared detection channel 101 and a visible light detection channel 102 which are parallel to each other are arranged on the detection frame; an infrared detection optical assembly 14 is arranged in the infrared detection channel 101, and an infrared detector 1405 is positioned at an infrared imaging focus at the tail end of the infrared detection channel 101 or on a light path of the infrared imaging focus reflected by a reflector group;
the visible light detection channel 102 is internally provided with a visible light detection optical assembly 15, the visible light detector 1506 is fixed above an outlet at the tail end of the visible light detection optical assembly 15, and the center line of the visible light detection channel 102 is perpendicular to the center of the detector target surface of the visible light detector 1506.
Further, infrared detector 1405 is located at the end of infrared detection channel 1406, and the center line of hollow infrared detection channel 1406 is aligned with the center of detector target surface 1408 of infrared detector 1405; a plurality of objective lens fixing tables are arranged in the infrared detection channel 1406, and objective lenses are fixed on a ring frame 1407 and are embedded on the objective lens fixing tables through the ring frame 1407;
the objective lenses comprise a first objective lens 1401, a second objective lens 1402 and a third objective lens 1403 which are sequentially arranged at the head part of an infrared detection channel 1406, and a fourth objective lens 1404 arranged at the tail part of the infrared detection channel 1406; a space required by a rear intercept is left between the third objective 1403 and the fourth objective 1404; the detector target plane 1408 is located at the imaging focus of the fourth objective lens 1404.
Further, another setting mode of the infrared detector is provided:
the infrared imaging focus at the tail end of the infrared detection channel 1406 is provided with a first infrared reflecting mirror 12, a second infrared reflecting mirror 13 and the first infrared reflecting mirror 12 are arranged in an axisymmetric manner, and an infrared detector 1405 is fixed on a detection frame 11 below the infrared detection channel 1406 and is positioned on a reflection light path of the second infrared reflecting mirror 13.
Specifically, the ring 1407 is embedded in the infrared detection channel 1406 through a thread, and the objective fixing table and the outer side of the ring 1407 are both provided with matched threads;
the diameters of the coils 1407 for fixing the first objective 1401, the second objective 1402 and the third objective 1403 are sequentially reduced, and the objective fixing tables for nesting the corresponding coils 1407 are sequentially arranged.
Specifically, the first objective 1401 is used as a diaphragm for receiving light, and a space between the first objective and the infrared detection channel 1406 is sealed by a sealant; the convex surface of the second objective lens 1402 is an aspheric surface to correct the spherical aberration introduced by the first objective lens 1401; the convex surface of the third objective lens 1403 is attached to the concave surface of the second objective lens 1402, so that chromatic aberration is corrected; the convex surface of the fourth objective lens 1404 is aspheric, and the back intercept distance between the third objective lens 1403 and the fourth objective lens 1404 can be adjusted by rotating the ring frame 1407.
Furthermore, a light-gathering cavity and a reflection cavity are arranged in the visible light detection channel 102, a right-angle reflection prism 1508 is arranged in the reflection cavity, and the visible light detector 1506 is fixed at the outlet of the reflection cavity; a plurality of lens fixing tables are arranged in the light gathering cavity, and the lenses are fixed on the ring frame and are embedded on the lens fixing tables through the lens fixing tables;
the lenses comprise a first lens 1501 and a second lens 1502 which are sequentially arranged at the head of the light-gathering cavity, and a third lens 1503, a fourth lens 1504 and a fifth lens 1505 which are arranged at the tail of the light-gathering cavity and are attached to each other; an aperture stop 1509 is arranged between the second lens 1502 and the third lens 1503; the detector target surface is mirror symmetric to the imaging focal point of the fourth lens 1504.
Specifically, the first lens 1501 is a thin meniscus lens, and the second lens 1502 is a thick lens; the third lens 1503 is a cemented lens for correcting chromatic aberration, the fourth lens 1504 is a thick lens for correcting curvature of field, and the fifth lens 1505 is a thin lens for correcting spherical aberration; changing the distance between the second lens 1502 and the fourth lens 1504 can correct astigmatism.
Specifically, the first lens 1501 is a double-lens or multiple-lens, and an optical filter 1507 is further disposed on the exit surface of the right-angle reflecting prism 1508; the right-angle reflecting prism 1508 is fixed with the side wall of the reflecting cavity through fixing glue; the filter 1507 is fixed to the exit surface of the rectangular reflecting prism 1508 by fixing glue.
The inclination angle of the reflector 16 and the horizontal direction is 45 degrees, and light rays are reflected by the reflector 16 and horizontally enter the dual-channel imaging mechanism; when the dual-channel imaging mechanism deflects relative to the vertical direction, the drive motor drives the mirror 16 to rotate via the drive belt 18, keeping the light reflected horizontally into the dual-channel imaging mechanism.
The reflection frame 10 and the detection frame 11 are also connected through a fixing pin 17;
the driving motor and the reflecting mirror 16 are installed on two parallel shafts of the reflecting frame 10, the transmission ratio between the driving shaft of the driving motor and the rotating shaft is 1/2, and the transmission belt 18 is a steel belt.
Specific examples are given below.
In order to meet the requirements of visible light and infrared high-precision detection in flight, the two-channel assembly of the utility model needs to cover and shoot a 30m area below the assembly at the height of 100 m; and because the optical design is difficult to consider the imaging quality in a large spectral range, the following parameter requirements are provided for considering the imaging in the range of 50-100000 lux and the imaging quality: illumination range: 50-100000 lux, frame frequency: not less than 5fps, single frame exposure time: less than or equal to 40ms, image distortion: less than or equal to 5%, field angle: not less than 24 ° × 18 ° (transverse direction × longitudinal direction).
The following is a description of the infrared optical assembly.
1) Infrared optical system parameter requirements
Aiming at the imaging requirement, a thermal imager with 1028 multiplied by 768 resolution can meet the requirement of resolution; when the height exceeds 100m, the spatial resolution of the unit pixel is not more than 0.42 m; other optical system parameters require the following: frame frequency: not less than 5 fps; single frame exposure time: less than or equal to 40 ms; at the edge of the field of view, the image is distorted: less than or equal to 5 percent; a field angle of not less than 24 ° × 18 ° (lateral × longitudinal); the full-surface coverage can be realized by adopting a 24-degree and 18-degree view field, and when the confidence coefficient is 0.8, the reliability of the detection assembly is more than or equal to 0.99.
The optical system designed based on the above conditions requires: visual field: 24 ° × 18 °, caliber: Φ 34, integration time: 10ms, and the image distortion is less than or equal to 5% at the edge of a visual field.
The focal length is then calculated as:
the resolution of a receiving sensor (thermal imager) is 1024 × 768, the pixel size is 14 μm, the size of the target surface is 14.336mm × 10.752mm through calculation, the diagonal of the target surface is 17.92mm, the field size required by design is 24 ° × 18 °, and the focal length of the optical system is calculated by using the formula (1):
in the formula:
f' -optical system focal length in mm;
d is the height of the target surface in mm;
omega-half field angle, unit.
The focal length f' is 33.72mm calculated by the formula (1).
The entrance pupil diameter is calculated as:
the F number of the optical system is taken as 1, and the entrance pupil diameter of the system is calculated using equation (2):
in the formula:
d-entrance pupil diameter, in mm.
f' -the current field focal length in mm;
F#f number of System
Calculating the diameter of the entrance pupil by using the formula (2)
According to the above calculation, the external parameters required for the design of the optical system are as follows:
1) focal length: f ═ 33.72 mm;
2) wavelength range: 8-14 μm;
3) visual field: 2 ω 24 ° × 18 °;
4) f number: 1.
2) optical system design
In view of the large field of view of optical imaging, the optical objective adopts a four-piece structure to meet the imaging requirement. In order to reduce the F number and improve the imaging quality of the edge of a field of view, the optical surface of the objective adopts an aspheric surface, the structure can simultaneously reduce the high spherical aberration of an off-axis field of view and the high spherical aberration of an on-axis aperture, and can obtain higher imaging quality under the condition of a larger field of view.
The design result of the optical system is shown in FIG. 4, the optical effective aperture of the system is 32mm, and the optical total length is less than 50 mm. The first objective lens is made of germanium materials and serves as a diaphragm of the system and is used for receiving light rays in a large range; the second objective lens is used for correcting spherical aberration introduced by the first objective lens, and the germanium material is also adopted, and the convex surface of the second objective lens is an aspheric surface. And the third objective lens is made of zinc sulfide material and is used for correcting chromatic aberration of the system. The fourth objective lens is made of germanium materials, and the convex surface of the fourth objective lens is an aspheric surface, so that the rear intercept of the system is adjusted, and the final imaging quality is guaranteed. Image quality evaluation and detection show that MTF of the system is greater than 0.3(35lp/mm), the maximum field point array spot is 15 mu m and is approximately equal to one pixel size; the maximum distortion is less than 5%.
3) Transmittance calculation
The system transmittance was calculated according to equation (3)
τ＝τ1 N1×τ2 n (3)
In the formula:
tau-total transmittance
τ1-permeability of the interface with air, 99%;
n1 — number of transmission planes, 4;
τ2-optical material transmission, calculated from the absorption coefficient, 90%;
n-total thickness of material, 12 mm;
4) tolerance analysis
The imaging quality of the system can be influenced by the material error, the surface type error, the thickness error and the interval error of the optical lens, the errors are calculated by using a reversal sensitivity method, the surface type and the interval of the optical part are subjected to tolerance analysis, and an analysis result shows that the system is insensitive to the aperture and the material, and the processing and adjusting process is simple and feasible.
5) Optical-mechanical structure arrangement
Referring to fig. 5, an infrared detector 1405 is disposed at the end of infrared detection channel 1406, and the centerline of infrared detection channel 1406 is aligned with the center of detector target surface 1408 of infrared detector 1405; the objective lens is fixed on the ring frame 1407 and is nested in the infrared detection channel 1406 through the ring frame 1407; first objective 1401, second objective 1402 and third objective 1403 are arranged at the head of infrared detection channel 1406, and fourth objective 1404 is arranged at the tail of infrared detection channel 1406; a space is left between the third objective lens 1403 and the fourth objective lens 1404 to adjust a pitch required for the back intercept.
A description is given below of the visible light assembly.
1) Parameter requirements of visible light optical system
Because the optical design hardly considers the imaging quality in a large spectral range, the following parameter requirements are provided for considering the imaging in the range of 50-100000 lux and the imaging quality: illumination range: 50-100000 lux, frame frequency: not less than 5fps, single frame exposure time: less than or equal to 40ms, image distortion: less than or equal to 5%, field angle: not less than 24 ° × 18 ° (transverse direction × longitudinal direction).
In order to improve the weak light imaging effect, the F number is reduced as much as possible under the condition of space allowance, so that the anti-saturation capacity of imaging under strong light is reduced, and the adjustment of the dynamic range of the camera is difficult to deal with; it is therefore proposed to insert an aperture stop into the beam path, i.e. in a strong light environment the light flux can be significantly reduced by the aperture stop, which then exits the beam path when the external light intensity becomes weak.
And (3) focal length calculation:
the size of the target surface of the receiving sensor was 15.1312mm × 10.5984mm (17.664 diagonal), the field of view was 24 ° × 18 °, and the focal length of visible light was calculated using equation (1):
in the formula:
f' -the current field focal length in mm;
d is the height of the target surface in mm;
omega-half field angle, unit.
The focal length f' is 33.24mm calculated by the formula (1).
Entrance pupil diameter calculation:
the entrance pupil diameter of the system is calculated using equation (2):
in the formula:
d-entrance pupil diameter, in mm;
f' -the current field focal length in mm;
F#-an F number.
Using equation (2), the entrance pupil diameter D is calculated to be phi 18mm taking F as 1.8.
According to the above calculation, the visible light optical system design parameters are as follows:
focal length: f ═ 32.66 mm; wavelength range: 0.65-0.85 μm; visual field: 2 ω 24 ° × 18 °;
f number: 1.8.
2) visible light imaging scheme
The utility model discloses a visible light image device belongs to great aperture and great visual field optical system, so regard three piece type lens as the design basis. The F-number of the three-piece lens can be designed to 4 to 5, and the angle of view can be designed to 400 to 500.
In order to reduce the F number and improve the imaging quality of the edge of a view field, the three-piece type lens is optimized and one lens is added; the front half system consists of a thin meniscus lens and a thick lens, and the rear half system consists of a thick lens and a thin lens, so that the four lenses tend to be symmetrical.
Because the vertical axis aberration of the symmetrical system is easy to correct, only the correction of spherical aberration, chromatic aberration, field curvature and astigmatism needs to be considered. Therefore, the field curvature is corrected by the structural change of the thick lens of the rear half system, the spherical aberration is corrected by the curvature of the thin lens, the astigmatism can be corrected by changing the distance between the two thick lenses, and the chromatic aberration is corrected by introducing a cemented surface into the thick lens.
In order to further satisfy larger relative aperture and ensure imaging quality, the meniscus thin lens is further designed into a double single/multiple single lens, the structure can simultaneously reduce the high-level spherical aberration of the off-axis field of view and the high-level spherical aberration of the on-axis aperture, and higher imaging quality can be obtained under the condition of a larger field of view. Therefore, the utility model discloses based on four structures of symmetry type, introduce the cemented mirror in the thick lens of its latter half in order to rectify the colour aberration, this structure can make the senior spherical aberration of off-axis visual field and the senior spherical aberration in epaxial aperture reduce simultaneously, can obtain higher imaging quality under the condition of great visual field.
The optical lens is required to have a working waveband of 0.4-0.8 mu m, an effective aperture of an optical system of 16.7mm and an optical total length of 60 mm; the MTF of the visible band system is close to 0.4(150lp/mm), the spot alignment spot is <4 μm, and the distortion is less than 3.5%.
3) Transmittance calculation
The system transmittance was calculated according to equation (3)
τ＝τ1 N1×τ2 n×τ3 (3)
In the formula:
τ — total transmittance;
τ1-permeability of the interface with air, 99%;
n1-number of transmission faces, 10;
τ2-optical material transmittance, calculated from the absorption coefficient, 99%;
n-total thickness of material, 3.57 cm;
τ3-filter transmittance 92%;
4) unit pixel spatial resolution verification
When the target distance is 1km and the pixel size is 3.45 mu m, the target size of the target is 0.208m when the target surface of the detector occupies N1 lp, so that the spatial resolution of a single pixel is 0.104 m.
The utility model provides a two-channel optical device for image acquisition, after being carried by the aircraft; when shooting the target/scenery, the light rays pass through the reflector in the transmitting mechanism, are received by the visible light imaging mechanism and the infrared imaging mechanism in the dual-channel imaging mechanism, and form image signals.
When the reflecting mechanism rotates relatively, the 1/2 transmission mechanism drives the reflecting mirror to rotate by half an angle, according to the geometrical optics principle of the reflecting mirror, incident light is fixed, the normal line of the reflecting mirror rotates by half, emergent light rotates by one degree, and therefore the effect that the visual axis is kept stable in the inertial space is guaranteed.
The utility model can perform two kinds of detection of infrared and visible light in flight, and can obtain high-precision imaging shooting under the conditions of large range and large visual field; is suitable for the detection of infrared light and visible light in flight respectively or simultaneously.
The embodiments given above are preferred examples for implementing the present invention, and the present invention is not limited to the above-described embodiments. Any non-essential addition and replacement made by the technical features of the technical solution of the present invention by those skilled in the art all belong to the protection scope of the present invention.
Claims (10)
1. A double-channel optical device for image acquisition is characterized by comprising a reflection mechanism and a double-channel imaging mechanism positioned on a reflection light path of the reflection mechanism, wherein visible light or infrared light is reflected by the reflection mechanism to enter the double-channel imaging mechanism;
the reflecting mechanism comprises a reflecting mirror (16) fixed on the reflecting frame (10) through a rotating shaft, and the inclination angle of the reflecting mirror (16) to the horizontal direction is 40-60 degrees; the rotating shaft is connected with a driving motor through a transmission belt (18), and the transmission belt (18) can drive the rotating shaft to change the inclination angle of the reflector (16) with the horizontal direction;
the dual-channel imaging mechanism comprises a detection frame (11) which is provided with an infrared detection channel (101) and a visible light detection channel (102) which are parallel; an infrared detection optical assembly (14) is arranged in the infrared detection channel (101), and an infrared detector (1405) is positioned at an infrared imaging focus at the tail end of the infrared detection channel (101) or is positioned on a light path of the infrared imaging focus reflected by a reflector group;
the visible light detection channel (102) is internally provided with a visible light detection optical assembly (15), the visible light detector (1506) is fixed above an outlet at the tail end of the visible light detection optical assembly (15), and the center line of the visible light detection channel (102) is vertical to the center of the detector target surface of the visible light detector (1506).
2. The dual channel optics for image acquisition as claimed in claim 1, wherein the infrared detector (1405) is located at an end of the infrared detection channel (1406), a centerline of the hollow infrared detection channel (1406) being aligned with a center of a detector target surface (1408) of the infrared detector (1405); a plurality of objective lens fixing platforms are arranged in the infrared detection channel (1406), and the objective lens is fixed on a ring frame (1407) and is embedded on the objective lens fixing platforms through the ring frame (1407);
the objective lens comprises a first objective lens (1401), a second objective lens (1402) and a third objective lens (1403) which are sequentially arranged at the head of an infrared detection channel (1406), and a fourth objective lens (1404) arranged at the tail of the infrared detection channel (1406); a distance required by a rear intercept is reserved between the third objective lens (1403) and the fourth objective lens (1404); the detector target surface (1408) is located at the imaging focus of the fourth objective lens (1404).
3. The dual channel optics for image acquisition as claimed in claim 2, wherein a first infrared mirror (12) is provided at the infrared imaging focus at the end of the infrared detection channel (1406), a second infrared mirror (13) is provided in an axisymmetric manner with the first infrared mirror (12), and an infrared detector (1405) is fixed to the detection frame (11) below the infrared detection channel (1406) and in the path of the reflected light of the second infrared mirror (13).
4. The dual channel optics for image acquisition as claimed in claim 2 or 3, wherein the coil (1407) is embedded in the infrared detection channel (1406) by a screw thread, and the objective lens fixing stage and the outer side of the coil (1407) are provided with matching screw threads;
the diameters of the ring frames (1407) for fixing the first objective lens (1401), the second objective lens (1402) and the third objective lens (1403) are sequentially reduced, and the objective lens fixing tables for nesting the corresponding ring frames (1407) are sequentially arranged.
5. The dual channel optical device for image acquisition as claimed in claim 2 or 3, characterized in that the first objective (1401) acts as a diaphragm for receiving light and is sealed with a sealant with the infrared detection channel (1406); the convex surface of the second objective lens (1402) is an aspheric surface so as to correct spherical aberration introduced by the first objective lens (1401); the convex surface of the third objective lens (1403) is attached to the concave surface of the second objective lens (1402) so as to correct chromatic aberration; the convex surface of the fourth objective lens (1404) is an aspheric surface, and the back intercept distance between the third objective lens (1403) and the fourth objective lens (1404) can be adjusted by rotating the ring frame (1407).
6. The dual-channel optical device for image acquisition as claimed in claim 1, wherein the visible light detection channel (102) has a light-gathering cavity and a reflection cavity, the reflection cavity has a right-angle reflection prism (1508), and the visible light detector (1506) is fixed at the exit of the reflection cavity; a plurality of lens fixing tables are arranged in the light gathering cavity, and the lenses are fixed on the ring frame and are embedded on the lens fixing tables through the lens fixing tables;
the lens comprises a first lens (1501) and a second lens (1502) which are sequentially arranged at the head of the light-gathering cavity, and a third lens (1503), a fourth lens (1504) and a fifth lens (1505) which are arranged at the tail of the light-gathering cavity and are attached to each other; an aperture stop (1509) is arranged between the second lens (1502) and the third lens (1503); the target surface of the detector is in mirror symmetry with the imaging focal point of the fourth lens (1504).
7. The dual channel optics for image acquisition as claimed in claim 6, wherein the first lens (1501) is a thin meniscus lens and the second lens (1502) is a thick lens; the third lens (1503) is a cemented lens for correcting chromatic aberration, the fourth lens (1504) is a thick lens for correcting curvature of field, and the fifth lens (1505) is a thin lens for correcting spherical aberration; astigmatism can be corrected by changing the distance between the second lens (1502) and the fourth lens (1504).
8. The dual channel optical device for image acquisition as claimed in claim 6, wherein said first lens (1501) is a double singlet lens or a multiple singlet lens, and said right angle reflecting prism (1508) further has a filter (1507) on its exit surface; the right-angle reflecting prism (1508) is fixed with the side wall of the reflecting cavity through fixing glue; the optical filter (1507) is fixed with the emergent surface of the right-angle reflecting prism (1508) through fixing glue.
9. The dual channel optical device for image acquisition as claimed in claim 1, wherein the mirror (16) is inclined at an angle of 45 ° to the horizontal, and light rays are reflected by the mirror (16) horizontally into the dual channel imaging mechanism; when the dual-channel imaging mechanism deflects relative to the vertical direction, the driving motor drives the reflector (16) to rotate through the driving transmission belt (18), and light rays are kept to enter the dual-channel imaging mechanism horizontally through reflection.
10. The dual channel optical device for image acquisition as claimed in claim 1 or 9, characterized in that the reflection frame (10) and the detection frame (11) are further connected by means of fixing pins (17);
the driving motor and the reflecting mirror (16) are arranged on two parallel shafts of the reflecting frame (10), the transmission ratio between the driving shaft of the driving motor and the rotating shaft is 1/2, and the conveying belt (18) is a steel belt.
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| Application Number | Priority Date | Filing Date | Title |
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| CN202022188551.9U CN212658836U (en) | 2020-09-29 | 2020-09-29 | Double-channel optical device for image acquisition |
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| Application Number | Priority Date | Filing Date | Title |
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| CN202022188551.9U CN212658836U (en) | 2020-09-29 | 2020-09-29 | Double-channel optical device for image acquisition |
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| CN212658836U true CN212658836U (en) | 2021-03-05 |
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