A wide-angle lens suitable for a drone

CN224888945UActive Publication Date: 2026-10-23FUJIAN FUGUANG TIANTONG OPTICS
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Patent Information

Application Number
CN202522250518.7
Authority / Receiving Office
CN · China
Patent Type
Utility models(China)
Current Assignee / Owner
Filing Date
2025-10-24
Publication Date
2026-10-23
Estimated Expiration
2035-10-24

AI Technical Summary

Benefits of technology

[0013]与现有技术相比,本实用新型具有以下效果:本实用新型设计合理,采用两片玻璃球面镜片搭配四片塑胶非球面透镜使用,相较于全玻系统具有更轻的系统质量,相对于全塑系统具有更强的光学性能稳定性,同时在适应环境的同时降低了成本;对物体的成像角度大于130度,同时具较高的成像清晰度、大的通光口径、较低的公差敏感度和较好的高低温稳定性等优点同时,能够更加全面地对目标进行监控。

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Abstract

The present application relates to a kind of wide-angle lens suitable for unmanned aerial vehicle, the optical system of the lens is made of first lens, second lens, third lens, diaphragm, fourth lens, fifth lens and sixth lens, first lens is meniscus concave negative lens, second lens is meniscus concave negative lens, third lens is double convex positive lens, fourth lens is double convex positive lens, fifth lens is meniscus concave negative lens, sixth lens is double convex positive lens, fourth lens and fifth lens constitute cemented lens, first lens and third lens are glass spherical lens, second lens, fourth lens, fifth lens and sixth lens are plastic aspherical lens. Two glass spherical lenses are used with four plastic aspherical lenses, compared with all-glass system, the system has lighter mass, compared with all-plastic system, the optical performance has stronger stability, while adapting to the environment, the cost is reduced;The imaging angle of object is greater than 130 degrees.
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Description

Technical Field

[0001] This utility model belongs to the field of lens technology, and in particular relates to a wide-angle lens suitable for drones. Background Technology

[0002] Due to its advantages such as mobility, speed, and economy, unmanned aerial vehicle (UAV) remote sensing has been widely applied in many fields of scientific research and civilian use. In recent years, with the continuous deepening of UAV aerial photography technology in various fields, people have become increasingly demanding in terms of the payload of UAVs. While meeting the requirements of wide field of view and high-resolution real-time imaging, the optical system also needs to be compact, lightweight, and small in size. Utility Model Content

[0003] This utility model addresses the problems existing in the prior art by providing a wide-angle lens suitable for drones. The lens is reasonably designed and achieves clear imaging at a wide angle of 130° while maintaining a small size and high environmental stability.

[0004] To achieve the above objectives, the technical solution adopted by this utility model is as follows: a wide-angle lens suitable for drones, wherein the optical system of the lens consists of a first lens, a second lens, a third lens, an aperture stop, a fourth lens, a fifth lens, and a sixth lens arranged sequentially from left to right along the incident light path. The first lens is a meniscus negative lens, the second lens is a meniscus negative lens, the third lens is a biconvex positive lens, the fourth lens is a biconvex positive lens, the fifth lens is a meniscus negative lens, and the sixth lens is a biconvex positive lens. The fourth and fifth lenses form a cemented lens. The first and third lenses are glass spherical lenses, and the second, fourth, fifth, and sixth lenses are all plastic aspherical lenses.

[0005] Furthermore, the object-side surface of the first lens is convex, and the image-side surface is concave; the object-side surface of the second lens is concave, and the image-side surface is convex; the object-side surface of the third lens is convex, and the image-side surface is convex; the object-side surface of the fourth lens is convex, and the image-side surface is convex; the object-side surface of the fifth lens is concave, and the image-side surface is convex; and the object-side surface of the sixth lens is convex, and the image-side surface is convex.

[0006] Furthermore, the on-axis distances between the lenses satisfy the following relationships: the air gap between the first and second lenses is 3.0–3.5 mm; the air gap between the second and third lenses is 0.1–0.5 mm; the air gap between the third lens and the aperture stop is 0.1–0.5 mm; the air gap between the aperture stop and the fourth lens is 0.1–0.5 mm; the fourth and fifth lenses are a cemented lens group with an air gap of 0 mm; and the air gap between the fifth and sixth lenses is 0.5–1.0 mm.

[0007] Furthermore, the focal length of the optical system is f The focal lengths of the first lens, second lens, third lens, fourth lens, fifth lens, and sixth lens are respectively f 1 , f 2 , f 3 , f 4 , f 5 , f 6 ,in f 1 , f 2 , f 3 , f 4 , f 5 , f 6 and f Meets the following ratio: -2.0 < f 1 / f <-1.0, -5.0< f 2 / f <-4.0, 1.0< f 3 / f <2.0, 1.0< f 4 / f <2.0, -2.0< f 5 / f <-1.0, 4.0< f 6 / f <5.0.

[0008] Furthermore, the first lens satisfies the relation: 1.6 ≤ N d ≤1.9, V d ≤50.0; The second lens satisfies the relationship: 1.5≤ N d ≤1.8, V d ≥50.0; The third lens satisfies the relationship: 1.6≤ N d ≤1.9, V d ≤50.0; The fourth lens satisfies the relationship: 1.5≤N d ≤1.8, V d ≥50.0; The fifth lens satisfies the relationship: 1.5≤ N d ≤1.8, V d ≤50.0; The sixth lens satisfies the relationship: 1.5≤ N d ≤1.8, V d ≥50.0; of which N d For refractive index, V d Let be Abbe's constant.

[0009] Furthermore, the equations for the aspherical curves of the second, fourth, fifth, and sixth lenses are as follows: Where Z is the distance from the vertex of the aspherical surface to the optical axis at a height of r; c is the paraxial curvature of the aspherical surface; k is the conic constant; and α1, α2, α3, α4, α5, α6, α7, and α8 are all higher-order coefficients. Furthermore, the total optical length TTL of the optical system satisfies the following relationship with the focal length f: TTL / f ≤ 6.1.

[0010] Furthermore, the F-number of the optical system is ≤1.6.

[0011] Furthermore, the image height H of the optical system and the focal length f of the optical system satisfy the following condition: H / f≤1.1.

[0012] Furthermore, the right side of the sixth lens is provided with a first equivalent glass plate and a second equivalent glass plate arranged sequentially from left to right.

[0013] Compared with the prior art, the present invention has the following advantages: The present invention is reasonably designed, using two glass spherical lenses in combination with four plastic aspherical lenses, which has a lighter system weight compared with the all-glass system and stronger optical performance stability compared with the all-plastic system. At the same time, it reduces costs while adapting to the environment. The imaging angle of the object is greater than 130 degrees, and it has the advantages of high imaging clarity, large light transmission diameter, low tolerance sensitivity and good high and low temperature stability. At the same time, it can monitor the target more comprehensively. Attached Figure Description

[0014] Figure 1 This is a schematic diagram of the optical structure of an embodiment of the present invention; Figure 2 This is the axial chromatic aberration diagram of the entire working band of this utility model embodiment; Figure 3 This is a cross-axis chromatic aberration diagram of the entire working band of this utility model embodiment; Figure 4 This is a field curvature distortion diagram of the entire working band of this utility model embodiment.

[0015] In the picture: STO - Aperture stop; L1 - First lens; L2 - Second lens; L3 - Third lens; L4 - Fourth lens; L5 - Fifth lens; L6 - Sixth lens; L7 - First equivalent glass plate; L8 - Second equivalent glass plate; IMA - Imaging surface. Detailed Implementation

[0016] The present invention will now be described in further detail with reference to the accompanying drawings and specific embodiments.

[0017] In the description of this utility model, it should be understood that the terms "longitudinal", "lateral", "up", "down", "front", "back", "left", "right", "vertical", "horizontal", "top", "bottom", "inner", "outer", etc., indicate the orientation or positional relationship based on the orientation or positional relationship shown in the accompanying drawings. They are only for the convenience of describing this utility model and do not indicate or imply that the device or element referred to must have a specific orientation, or be constructed and operated in a specific orientation. Therefore, they should not be construed as limitations on this utility model.

[0018] like Figure 1 As shown, this utility model discloses a wide-angle lens suitable for drones. The optical system of the lens consists of a first lens, a second lens, a third lens, an aperture stop, a fourth lens, a fifth lens, and a sixth lens arranged sequentially from left to right along the incident light path. Without considering the curvature caused by aspherical coefficients, the first lens is a meniscus negative lens with a convex object-side surface and a concave image-side surface; the second lens is a meniscus negative lens with a concave object-side surface and a convex image-side surface; the third lens is a biconvex positive lens with a convex object-side surface and a convex image-side surface; the fourth lens is a biconvex positive lens with a convex object-side surface and a convex image-side surface; the fifth lens is a meniscus negative lens with a concave object-side surface and a convex image-side surface; and the sixth lens is a biconvex positive lens with a convex object-side surface and a convex image-side surface. The fourth and fifth lenses form a cemented lens, the first and third lenses are glass spherical lenses, and the second, fourth, fifth, and sixth lenses are all plastic aspherical lenses. The optical structure employs two glass lenses paired with four plastic aspherical lenses, fully leveraging the aberration correction advantages of aspherical lenses to achieve high-definition imaging while maintaining a smaller lens outer diameter and shorter overall optical length, ensuring lens miniaturization. Compared to all-glass systems, the hybrid glass-plastic system is lighter, while compared to all-plastic systems, it offers stronger optical performance stability, and reduces costs while being more adaptable to different environments.

[0019] In this embodiment, the first and third lenses are spherical lenses with negative optical power, which adjust large-angle light while reducing optical system distortion. The appropriate lens combination enables the optical system to achieve a small size, 130° ultra-wide angle, large aperture, day and night confocal focus, and low temperature drift design. Simultaneously, it provides good correction for on-axis and off-axis aberrations, resulting in good image quality. Figures 2 to 4 As shown.

[0020] In this embodiment, the on-axis distances between the lenses satisfy the following relationships: the air gap between the first lens and the second lens is 3.0 to 3.5 mm; the air gap between the second lens and the third lens is 0.1 to 0.5 mm; the air gap between the third lens and the aperture stop is 0.1 to 0.5 mm; the air gap between the aperture stop and the fourth lens is 0.1 to 0.5 mm; the fourth lens and the fifth lens are a cemented lens group with an air gap of 0; and the air gap between the fifth lens and the sixth lens is 0.5 to 1.0 mm.

[0021] In this embodiment, the focal length of the optical system is f The focal lengths of the first lens, second lens, third lens, fourth lens, fifth lens, and sixth lens are respectively f 1 , f 2 , f 3 , f 4 , f 5 , f 6 ,in f 1 , f 2 , f 3 , f 4 , f 5 , f 6 and f Meets the following ratio: -2.0 < f 1 / f <-1.0, -5.0< f 2 / f <-4.0, 1.0< f 3 / f <2.0, 1.0< f 4 / f<2.0, -2.0< f 5 / f <-1.0, 4.0< f 6 / f <5.0.

[0022] In this embodiment, the first lens satisfies the relationship: 1.6 ≤ N d ≤1.9, V d ≤50.0; The second lens satisfies the relationship: 1.5≤ N d ≤1.8, V d ≥50.0; The third lens satisfies the relationship: 1.6≤ N d ≤1.9, V d ≤50.0; The fourth lens satisfies the relationship: 1.5≤ N d ≤1.8, V d ≥50.0; The fifth lens satisfies the relationship: 1.5≤ N d ≤1.8, V d ≤50.0; The sixth lens satisfies the relationship: 1.5≤ N d ≤1.8, V d ≥50.0; of which N d For refractive index, V d Let be Abbe's constant.

[0023] In this embodiment, the equations for the aspherical curves of the second lens, the fourth lens, the fifth lens, and the sixth lens are as follows: Where Z is the distance from the vertex of the aspherical surface to the optical axis at a height of r; c is the paraxial curvature of the aspherical surface; k is the conic constant; and α1, α2, α3, α4, α5, α6, α7, and α8 are all higher-order coefficients. Furthermore, the total optical length TTL of the optical system satisfies the following relationship with the focal length f: TTL / f ≤ 6.1.

[0024] In this embodiment, the F-number of the optical system is ≤1.6.

[0025] In this embodiment, the image height H of the optical system and the focal length f of the optical system satisfy the following condition: H / f≤1.1.

[0026] In this embodiment, a first equivalent glass plate and a second equivalent glass plate are arranged sequentially from left to right on the right side of the sixth lens.

[0027] In this embodiment, the technical specifications achieved by the lens's optical system are as follows: (1) Effective focal length: 3.0≤EFFL≤4.0mm; (2) Aperture F≤1.6; (3) Field of view: 2w ≥ 130°; (4) Operating band: Visible light band.

[0028] To achieve the above technical specifications, the specific design of the optical system in this embodiment is shown in the table below: .

[0029] The aspherical coefficients of the aspherical lenses in the optical system of this embodiment are shown in the table below: The optical system in this embodiment achieves miniaturization of the lens group by rationally allocating the optical power, surface shape, center thickness of each lens, and on-axis distance between each lens, while meeting the requirements of 130° ultra-wide-angle imaging performance.

[0030] The advantages of this utility model are: 1. This lens has an imaging angle of more than 130 degrees and features high imaging clarity, large aperture, low tolerance sensitivity and good high and low temperature stability, while also enabling more comprehensive monitoring of the target. 2. By rationally matching the various optical lenses, the system structure is compact and reasonable, reducing the overall size, making it easy to assemble, with low tolerance sensitivity, and more suitable for large-scale high-yield production; 3. It uses two glass spherical lenses in combination with four plastic aspherical lenses, which has a lighter system weight compared to the all-glass system and stronger optical performance stability compared to the all-plastic system, while reducing costs while adapting to the environment. 4. The chromatic aberration along each axis, the transverse chromatic aberration, and higher-order chromatic aberrations have been corrected to ensure that the imaging system can maintain high imaging quality even at large angles.

[0031] If this utility model discloses or relates to mutually fixedly connected parts or structural components, then, unless otherwise stated, a fixed connection can be understood as: a detachable fixed connection (e.g., using bolts or screws), or a non-detachable fixed connection (e.g., riveting, welding). Of course, mutually fixed connections can also be replaced by an integral structure (e.g., manufactured using a casting process) (except where it is obviously impossible to use an integral forming process).

[0032] In addition, unless otherwise stated, the terms used to indicate positional relationships or shapes in any of the technical solutions disclosed in this utility model above include states or shapes that are similar to, close to, or approximate with them.

[0033] Any component provided by this utility model can be assembled from multiple individual components, or it can be a single component manufactured by a one-piece molding process.

[0034] Finally, it should be noted that the above embodiments are only used to illustrate the technical solution of this utility model and not to limit it; although the utility model has been described in detail with reference to preferred embodiments, those skilled in the art should understand that modifications can still be made to the specific implementation of this utility model or equivalent substitutions can be made to some technical features without departing from the spirit of the technical solution of this utility model, and all such modifications and substitutions should be covered within the scope of the technical solution claimed by this utility model.

Claims

1. A wide-angle lens suitable for drones, characterized in that: The optical system of the lens consists of a first lens, a second lens, a third lens, an aperture stop, a fourth lens, a fifth lens, and a sixth lens arranged sequentially from left to right along the incident light path. The first lens is a meniscus negative lens, the second lens is a meniscus negative lens, the third lens is a biconvex positive lens, the fourth lens is a biconvex positive lens, the fifth lens is a meniscus negative lens, and the sixth lens is a biconvex positive lens. The fourth and fifth lenses form a cemented lens. The first and third lenses are glass spherical lenses, while the second, fourth, fifth, and sixth lenses are all plastic aspherical lenses.

2. A wide-angle lens suitable for drones according to claim 1, characterized in that: The first lens has a convex object-side surface and a concave image-side surface; the second lens has a concave object-side surface and a convex image-side surface; the third lens has a convex object-side surface and a convex image-side surface; the fourth lens has a convex object-side surface and a convex image-side surface; the fifth lens has a concave object-side surface and a convex image-side surface; and the sixth lens has a convex object-side surface and a convex image-side surface.

3. A wide-angle lens suitable for drones according to claim 2, characterized in that: The on-axis distances between the lenses satisfy the following relationships: the air gap between the first and second lenses is 3.0–3.5 mm; the air gap between the second and third lenses is 0.1–0.5 mm; the air gap between the third lens and the aperture stop is 0.1–0.5 mm; the air gap between the aperture stop and the fourth lens is 0.1–0.5 mm; the fourth and fifth lenses are a cemented lens group with an air gap of 0 mm; and the air gap between the fifth and sixth lenses is 0.5–1.0 mm.

4. A wide-angle lens suitable for drones according to claim 1, characterized in that: The focal length of the optical system is f The focal lengths of the first lens, second lens, third lens, fourth lens, fifth lens, and sixth lens are respectively f 1 , f 2 , f 3 , f 4 , f 5 , f 6 ,in f 1 , f 2 , f 3 , f 4 , f 5 , f 6 and f Meets the following ratio: -2.0 < f 1 / f <-1.0, -5.0< f 2 / f <-4.0, 1.0< f 3 / f <2.0, 1.0< f 4 / f <2.0, -2.0< f 5 / f <-1.0, 4.0< f 6 / f <5.

0.

5. A wide-angle lens suitable for drones according to claim 1, characterized in that: The first lens satisfies the relation: 1.6 ≤ N d ≤1.9, V d ≤50.0; The second lens satisfies the relationship: 1.5≤ N d ≤1.8, V d ≥50.0; The third lens satisfies the relationship: 1.6≤ N d ≤1.9, V d ≤50.0; The fourth lens satisfies the relationship: 1.5≤ N d ≤1.8, V d ≥50.0; The fifth lens satisfies the relationship: 1.5≤ N d ≤1.8, V d ≤50.0; The sixth lens satisfies the relationship: 1.5≤ N d ≤1.8, V d ≥50.0; of which N d For refractive index, V d Let be Abbe's constant.

6. A wide-angle lens suitable for drones according to claim 1, characterized in that: The equations for the aspherical curves of the second, fourth, fifth, and sixth lenses are as follows: Where Z is the distance from the vertex of the aspherical surface to the optical axis at a height of r; c is the paraxial curvature of the aspherical surface; k is the conic constant; and α1, α2, α3, α4, α5, α6, α7, and α8 are all higher-order coefficients.

7. A wide-angle lens suitable for drones according to claim 1, characterized in that: The total optical length (TTL) of an optical system and the focal length (f) of the optical system satisfy the following condition: TTL / f ≤ 6.

1.

8. A wide-angle lens suitable for drones according to claim 1, characterized in that: The F-number of the optical system is ≤1.

6.

9. A wide-angle lens suitable for drones according to claim 1, characterized in that: The image height H of the optical system and the focal length f of the optical system satisfy the following relationship: H / f≤1.

1.

10. A wide-angle lens suitable for drones according to claim 1, characterized in that: The right side of the sixth lens is provided with a first equivalent glass plate and a second equivalent glass plate arranged from left to right.