Anamorphic refractive objective lens assembly
10976528 · 2021-04-13
Assignee
Inventors
- Marco A. Avila (McKinney, TX, US)
- Douglas J. Hartnett (The Colony, TX, US)
- Mark Noethen (Tucson, AZ, US)
Cpc classification
G02B1/00
PHYSICS
International classification
G02B13/00
PHYSICS
Abstract
Aspects and embodiments are generally directed to compact anamorphic refractive objective lens assemblies. In one example, a refractive objective lens assembly includes a passively athermal anamorphic lens group including at least a first cylindrical lens having a surface optically powered in a first dimension, the first anamorphic lens group positioned to receive thermal infrared radiation, a focus cell positioned to receive the radiation from the anamorphic lens group, the focus cell including a first group of lenses each having a rotationally symmetric surface optically powered in the first dimension and a second dimension orthogonal to the first dimension, a relay lens group positioned receive the radiation from the focus cell, the relay lens group including a second group of lenses each having a rotationally symmetric surface optically powered in both the first and second dimensions, and a dewar assembly including a cold stop and an optical detector.
Claims
1. A refractive objective lens assembly comprising: a passively athermal anamorphic lens group positioned to receive thermal infrared radiation and including a first cylindrical lens, a second cylindrical lens, and a third cylindrical lens each having a surface optically powered in a first dimension, the anamorphic lens group being configured to athermalize a first focal length of the refractive objective lens assembly in the first dimension; a focus cell positioned to receive the thermal infrared radiation from the anamorphic lens group and including a first group of lenses each having a rotationally symmetric surface optically powered in at least a second dimension orthogonal to the first dimension, the first group of lenses being configured to adjust the first focal length and a temperature sensitive second focal length of the refractive objective lens assembly in the second dimension; and a relay lens group positioned to receive the thermal infrared radiation from the focus cell, the relay lens group including a second group of lenses each having a rotationally symmetric surface optically powered in at least the second dimension, wherein the second group of lenses includes a third lens, a fourth lens, and a fifth lens each formed from a first material, and a sixth lens and a seventh lens each formed from a second material, the second group of lenses arranged so as to alternate between the lenses of the first material and the lenses of the second material.
2. The refractive objective lens assembly of claim 1, further comprising a fold mirror interposed between the focus cell and the relay lens group and positioned to direct the thermal infrared radiation from the focus cell to the relay lens group.
3. The refractive objective lens assembly of claim 2, further comprising a fourth cylindrical lens having a surface optically powered in the first dimension, the fourth cylindrical lens interposed between the fold mirror and the relay lens group.
4. The refractive objective lens assembly of claim 3, wherein the first cylindrical lens is formed from silicon (Si), the second cylindrical lens is formed from Germanium (Ge), and the third cylindrical lens is formed from Silicon (Si), the second cylindrical lens being interposed between the first cylindrical lens and the third cylindrical lens.
5. The refractive objective lens assembly of claim 1, wherein at least the first cylindrical lens, the second cylindrical lens, and the third cylindrical lens are configured to expand the thermal infrared radiation in a plane of the first dimension.
6. The refractive objective lens assembly of claim 5, wherein an anamorphic ratio of the expansion of the thermal infrared radiation between the first dimension and the second dimension is two.
7. The refractive objective lens assembly of claim 1, wherein a ratio of a lens length and an effective focal length of the refractive objective lens assembly is 1.5.
Description
BRIEF DESCRIPTION OF THE DRAWINGS
(1) Various aspects of at least one embodiment are discussed below with reference to the accompanying figures, which are not intended to be drawn to scale. The figures are included to provide illustration and a further understanding of the various aspects and embodiments, and are incorporated in and constitute a part of this specification, but are not intended as a definition of the limits of the invention. In the figures, each identical or nearly identical component that is illustrated in various figures is represented by a like numeral. For purposes of clarity, not every component may be labeled in every figure. In the figures:
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DETAILED DESCRIPTION
(6) Aspects and examples are generally directed to a compact anamorphic refractive objective lens assembly for thermal infrared imaging operations, such as imaging operations within the mid-wavelength infrared spectral band of the electromagnetic spectrum. According to certain examples, the refractive objective lens assembly described herein includes a passively athermal anamorphic lens group that maintains a focus of the objective lens assembly over a wide range of temperatures (e.g., −40° C. to +55° C.) and operating conditions. Moreover, examples of the compact anamorphic objective lens assembly described herein have a reduced total length for a given anamorphic ratio and a given focal length when compared to typical anamorphic lens assemblies. For instance, the objective lens assembly may have a ratio of a lens length to an effective focal length of as low as 1.5. As a result of the reduced size and weight, and improved temperature insensitivity, of the described objective lens assembly, examples may be incorporated within aerial and other mobile imaging systems that are designed to perform wide area surveillance (WAS) imaging.
(7) In many aerial imaging applications, a field of view of an imaging system (e.g., a WAS imaging system) is projected at an angle slanted from altitude of the associated aerial platform. While this arrangement allows the imaging system to image “ahead” of the aerial platform, the projected slant often results in a distorted instantaneous field of view on the ground. That is, while an optical receiver of the imaging system may have a substantially square profile, the projected instantaneous field of view is distorted to a rectangular profile based on the angle of projection. While typical cinema projection lenses offer one potential solution to correcting the distorted field of view, current cinema projection lenses are too large and heavy to incorporate within most WAS imaging systems and are limited to operation within the visible portion of the electromagnetic spectrum. For instance, most cinema projection lenses include a simple afocal cylinder lens pair that more than doubles the length of the primary lens group and does not support high resolution imaging. To accommodate high resolution imaging, additional optics must be added, which further increases the size and weight of the lens assembly.
(8) Accordingly, various aspects and examples of the compact anamorphic refractive objective lens assembly discussed herein offer an improved lens design with a reduced size and weight. Particular embodiments may be incorporated within imaging systems that have limited available space, such as WAS imaging systems. While discussed with reference to an aerial imaging system for the purpose of explanation, in various other examples the WAS imaging system may be designed for a ground platform, a maritime platform, a space platform, or any other mobile platform or vehicle.
(9) It is to be appreciated that embodiments of the systems and apparatuses discussed herein are not limited in application to the details of construction and the arrangement of components set forth in the following description or illustrated in the accompanying drawings. The systems and apparatuses are capable of implementation in other embodiments and of being practiced or of being carried out in various ways. Examples of specific implementations are provided herein for illustrative purposes only and are not intended to be limiting. Also, the phraseology and terminology used herein is for the purpose of description and should not be regarded as limiting. The use herein of “including,” “comprising,” “having,” “containing,” “involving,” and variations thereof is meant to encompass the items listed thereafter and equivalents thereof as well as additional items. References to “or” may be construed as inclusive so that any terms described using “or” may indicate any of a single, more than one, and all of the described terms. Any references to front and back, left and right, top and bottom, upper and lower, and vertical and horizontal are intended for convenience of description, not to limit the present systems and methods or their components to any one positional or spatial orientation.
(10) Referring to
(11) The anamorphic lens group 102 is positioned to receive thermal infrared radiation from a scene along the optical path 114 and direct the thermal infrared radiation to the focus cell 104. The focus cell 104 is positioned to receive the thermal infrared radiation from the anamorphic lens group 102 and direct the thermal infrared radiation to the fold mirror 106. The fold mirror 106 reflects the received thermal infrared radiation along the optical path 114 to the relay lens group 110. The relay lens group 110 is positioned along the optical path 114 to receive the thermal infrared radiation from the fold mirror 106 and direct the thermal infrared radiation along the optical path 114 to the dewar assembly 112. The dewar assembly 112 is positioned to receive the thermal infrared radiation along the optical path 114 and focus the infrared radiation at an optical detector 116 located therein.
(12) In various examples, the anamorphic lens group 102, the focus cell 104, the fold mirror 106, the relay lens group 110, the additional cylindrical lens 108, and the dewar assembly 112 are supported within a housing (not shown). The housing surrounds and protects the components of the refractive objective lens assembly 100 from dirt, dust, moisture, and the like. The housing may include a window through which the anamorphic lens group 102 directly receives the thermal infrared radiation. However, in certain other examples one or more additional optics, such as a primary mirror and a secondary mirror may collect the thermal infrared radiation from a scene and direct the thermal infrared radiation to the anamorphic lens group 102. As discussed herein, thermal infrared radiation refers to electromagnetic radiation within the mid-wavelength infrared spectral band (e.g., 3 micrometers-8 micrometers) and long-wavelength infrared spectral band (e.g., 8 micrometers-15 micrometers). However, in particular examples the refractive objective lens assembly 100 may be optimized for just the mid-wavelength infrared spectral band or the long-wavelength infrared spectral band, or a portion thereof.
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(14) The anamorphic lens group 202 may include one or more cylindrical lenses that have a surface optically powered in a first dimension (e.g., an x-direction). In
(15) Each of the first, second, and third cylindrical lens 216, 218, 220 are positioned along the optical path to receive and transmit the thermal infrared radiation.
(16) In various examples, the anamorphic lens group 202 is passively athermalized due to the particular arrangement and material composition of the illustrated cylindrical lenses 216, 218, 220. That is, the anamorphic lens group 202 is insensitive to temperature fluctuations within the refractive objective lens assembly 200 and/or about the refractive objective lens assembly 200. In a particular example, the first cylindrical lens 216, the second cylindrical lens 218, and the third cylindrical lens 220 are positioned so as to fix a first focal length of the refractive objective lens assembly 200 in the dimension in which the first, second, and third cylindrical lenses 216, 218, 220 are optically powered (e.g., the first dimension). Each of the first cylindrical lens 216, the second cylindrical lens 218, and the third cylindrical lens 220 may be coupled to a corresponding bracket or support structure that immobilizes the corresponding cylindrical lens. As previously discussed, the first cylindrical lens 216, the second cylindrical lens 218, and the third cylindrical lens 220 influence (e.g., fix) the first focal length. In such an example, the first, second, and third cylindrical lenses 216, 218, 220 may be formed from materials that are inherently temperature insensitive, such as silicon (Si) or zinc sulfide (ZnS). For instance, the first cylindrical lens 216 may be formed from silicon (Si), the second lens 218 may be formed from zinc sulfide (ZnS), and the third cylindrical lens 220 may be formed from silicon (Si). However, in other examples, other materials that are transmissive to thermal infrared radiation and temperature insensitive may be used. Accordingly, in various examples the anamorphic lens group 202 athermalizes the first focal length of the refractive objective lens assembly 200.
(17) As illustrated in
(18) The second lens 224 of the focus cell 204 directs the thermal infrared radiation to the fold mirror 206. The fold mirror 206 is interposed between the focus cell 204 and the relay lens group 208 and positioned to direct the thermal infrared radiation from the focus cell 204 to the relay lens group 208. In particular, the fold mirror 206 may have a reflective surface that receives the thermal infrared radiation from the second lens 224 of the focus cell 204 and reflects the thermal infrared radiation to the relay lens group 208. As illustrated in
(19) As illustrated in
(20) In the illustrated example, the fourth cylindrical lens 212 directs the thermal infrared radiation to the relay lens group 208. The relay lens group 208 may include a second group of lenses that each have a rotationally symmetric surface optically powered in the first dimension and the second dimension (e.g., the x-direction and the y-direction, respectively). In the illustrated example, the relay lens group 208 includes a third lens 226, a fourth lens 228, a fifth lens 230, a sixth lens 232, and a seventh lens 234 centered about the optical path. Each lens 226, 228, 230, 232, 234 may focus or expand the thermal infrared radiation in the plane corresponding to the first dimension and the plane corresponding to the second dimension. That is, in various examples, the second group of lenses is configurable to adjust the focal length of the refractive objective lens assembly 200 in the second dimension (i.e., the temperature sensitive second focal length) and the focal length of the refractive objective lens assembly 200 in the first dimension (i.e., the first focal length). For instance, each of the lenses 226, 228, 230, 232, 234 may be positioned on a corresponding gimbal assembly, or adjustable support system, that is controllable to displace the corresponding lens 226, 228, 230, 232, 234 to affect an increase or decrease in both focal lengths of the refractive objective lens assembly 200. The lenses 226, 228, 230, 232, 234 may be independently adjustable, adjustable in sub-groups of the second group of lenses, or adjustable as a group.
(21) Accordingly, while the first focal length of the refractive objective lens assembly 200 may be adjusted by the anamorphic lens group 202, adjustments made to the lenses 226, 228, 230, 232, 234 of the relay lens group 208 may accommodate for impacts that temperature and/or operating conditions may have on the first and second focal lengths of the refractive objective lens assembly 200. In certain examples, the third lens 226, the fifth lens 230, and the seventh lens 234 may each be formed from a first material, and the fourth lens 228 and the sixth lens 232 may each be formed from a second material. For instance, the first material may be silicon (Si) and the second material may be zinc sulfide (ZnS). In one example, the second group of lenses is arranged so as to alternate between the lenses of the first material and the lenses of the second material. That is, the third lens 226 may direct the thermal infrared radiation to the fourth lens 228. The fourth lens 228 may receive the infrared radiation from the third lens 226 and direct the infrared radiation to the fifth lens 230. The fifth lens 230 may receive the infrared radiation from the fourth lens 228 and direct the infrared radiation to the sixth lens 232. The sixth lens 232 may receive the infrared radiation from the fifth lens 230 and direct the infrared radiation to the seventh lens 234. As illustrated in
(22) The dewar assembly 210 is positioned to receive the thermal infrared radiation from the seventh lens 234 and direct the thermal infrared radiation to an optical detector 236. The dewar assembly 210 may include a dewar, a dewar window, a cold stop 240, and the optical detector 236. The dewar encloses (e.g., in a vacuum environment) the cold stop 240 and the optical detector 236, and protects the contents of the dewar from temperature fluctuations of the operating environment. The dewar window is positioned to receive the thermal infrared radiation and direct the thermal infrared radiation to the cold stop 240. The cold stop 240 limits the amount of thermal infrared radiation that reaches an image plane of the refractive objective lens assembly 200. For example, the cold stop 240 may be an edge of a fixture that holds a lens in place or an edge of a lens. Thermal infrared radiation that passes through the cold stop 240 is directed to the optical detector 236.
(23) In various examples, the optical detector 236 is positioned at an image plane to receive and image the thermal infrared radiation. The optical detector 236 may include any photodetector sensitive to wavelengths within the thermal infrared spectrum or a subset of the thermal infrared spectrum, such as the mid-wavelength infrared spectral band or the long-wavelength infrared spectral band. For instance, the optical detector 236 may include an array of photo-sensitive detector elements (e.g., pixels) that receive and integrate impinging thermal infrared radiation. A circuit within each pixel of the optical detector 236 accumulates charge corresponding to the incident thermal infrared radiation. At the end of an integration period, each pixel may be deactivated, and a read-out signal may be provided based on the accumulated charge. The read-out signals may be used to generate and image based on the received thermal infrared radiation. In various embodiments, the array of detector elements may include infrared detector materials such as indium gallium arsenide (InGaAs) or mercury cadmium telluride (HgCaTe), to name a few examples.
(24) As further illustrated in
(25) Referring to
(26) In particular examples, the optical elements of the refractive objective lens assembly 200 are arranged to achieve an anamorphic ratio of two between the expansion of light within the first dimension and the expansion of light within the second dimension (e.g., expansion of light within the first dimension divided by the expansion of light within the second dimension). For example, when combined, each of the first, second, third, and fourth cylindrical lens 216, 218, 220, 212, as well as the other optical elements of the refractive objective lens assembly 200, may expand the received thermal infrared radiation substantially more in one dimension than in the other dimension. In one example, this may include adjusting the focal length twice as much in the first dimension (e.g., x-direction) as in the second dimension (e.g., y-direction), while in other examples it may include adjusting the focal length twice as much in the second dimension as in the first dimension. While an anamorphic ratio of two is described as one example, it is appreciated that in various other examples the optical elements of the refractive objective lens assembly 200 may be arranged to achieve other anamorphic ratios, such as from about 1 to 2.2 (±0.1 or 0.2). TABLE 1 provides examples of surface data for an optical prescription of an example of a refractive objective lens assembly that may be used to achieve an anamorphic ratio of two, for example.
(27) As discussed above, various examples of the refractive objective lens assembly 200 described herein have a reduced total length for a given anamorphic ratio and a given focal length when compared to typical anamorphic lens assemblies. For example, a ratio of length and effective focal length (L/EFL) of the refractive objective lens assembly 200 may be significantly less than most cinematic projection lenses, making the refractive objective lens assembly 200 easier to incorporate within WAS imaging systems. In one example, the ratio of lens length (shown in
(28) TABLE 1 below provides surface data for an optical prescription for an example of the refractive objective lens assembly 200 illustrated in
(29) TABLE-US-00001 TABLE 1 Ref. Asph. Asph. Surface Type Rad. Sep. Material Index Coef. Coef. 1 (front) Cylinder 14.325 0.1500 silicon 3.42 1 (back) Cylinder plane 0.0500 air 2 (front) Cylinder plane 0.1500 germanium 4.01 2 (back) Cylinder 66.794 4.1027 air 3 (front) Cylinder −9.430 0.1500 silicon 3.42 3 (back) Cylinder plane 0.1000 air 4 (front) 1.648 0.2000 silicon 3.42 4 (back) Asphere 3.039 0.0649 air 4th 0.0063 order 5 (front) 4.927 0.1500 zinc sulfide 2.25 5 (back) 1.899 1.4000 air Fold plane 0.4500 air Mirror plane 0.5106 air 6 (front) Cylinder 1.130 0.1249 zinc sulfide 2.25 6 (back) Cylinder 1.076 0.0250 air 7 (front) Asphere 0.903 0.1500 silicon 3.42 4th 0.0246 order 6th −0.1203 order 8th 0.2263 order 7 (back) 0.903 0.3273 air 8 (front) −0.850 0.1000 zinc sulfide 2.25 8 (back) 10.000 0.0519 air 9 (front) −6.630 0.2000 silicon 3.42 9 (back) Asphere −1.146 0.0400 air 4th 0.1609 order 6th −0.0566 order 10 (front) −1.078 0.1500 zinc sulfide 2.25 10 (back) Asphere −1.268 0.0400 air 4th −0.1732 order 6th 0.0750 order 11 (front) 0.700 0.2037 silicon 3.42 11 (back) Asphere 0.701 0.4500 air 4th 0.0117 order 6th 0.3488 order 12 (front) plane 0.0400 germanium 4.01 12 (back) plane 0.0390 air STOP plane 0.0000 air plane 0.9940 air Detector plane 0.0000 air
(30) As such, aspects and examples described herein provide a compact anamorphic refractive objective lens assembly for imaging within the thermal infrared spectrum. In particular, examples of the refractive objective lens assembly described herein have a reduced total length for a given anamorphic ratio and a given focal length when compared to typical anamorphic lens assemblies. Moreover, as further discussed herein, the refractive objective lens assembly may have a ratio of a lens length to an effective focal length of as low as 1.5. As a result of the reduced size and weight, and improved temperature insensitivity, of the described refractive objective lens assembly, examples may be incorporated within platforms in which available space is limited and weight is a significant design factor.
(31) Having described above several aspects of at least one example, it is to be appreciated that various alterations, modifications, and improvements will readily occur to those skilled in the art. Such alterations, modifications, and improvements are intended to be part of this disclosure and are intended to be within the scope of the invention. Accordingly, the foregoing description and drawings are by way of example only, and the scope of the invention should be determined from proper construction of the appended claims, and their equivalents.