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Splicing type conformal optical window

An optical window and splicing technology, applied in optics, optical components, installation, etc., can solve problems such as limited field of view expansion, and achieve the effect of meeting the requirements of large field of view, stealth and aerodynamics of aircraft

Active Publication Date: 2015-07-01
CHANGCHUN INST OF OPTICS FINE MECHANICS & PHYSICS CHINESE ACAD OF SCI
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  • Summary
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  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0004] In order to solve the problem that the existing optical window can only expand the field of view angle of the optical load in one direction, and the field of view expansion is limited, the present invention provides a spliced ​​conformal optical window

Method used

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specific Embodiment approach 1

[0015] Specific implementation mode 1. Combination image 3 and Figure 4 Describe this implementation mode, a spliced ​​conformal optical window, the structural diagram of the optical window is as follows image 3 As shown, it mainly includes the main window glass 10, the first group of side glasses, the second group of side glasses and the third group of side glasses, each group of side glasses is composed of two side glasses with the same size and shape, and the adjacent two side glasses The sides are fixed by gluing, and one side of each group of side glass is fixed by gluing with the side of the main window glass. The first group of side glasses includes a first side front glass 11 and a second side front glass 12, and the second group of side glass The glass includes a first side front glass 13 and a second side front glass 14 , and the third set of side glass includes a first side rear glass 15 and a second side rear glass 16 .

[0016] In this embodiment, it consists...

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Abstract

The invention provides a splicing type conformal optical window, and relates to the field of aeronautical facilities. The problems that by the existing optical window, only an optical load visual field angle in one direction can be expanded, and expansion of a large range of the visual field is limited are solved. The splicing type conformal optical window comprises seven pieces of flat-plate optical glass, wherein the seven pieces of flat-plate optical glass are glued together and mainly comprise a piece of main window glass, a first group of side glass, a second group of side glass and a third group of side glass; each group of side glass consists of two pieces of side glass with the same size and the same shape; sides of each two adjacent pieces of side glass are fixedly glued; and one sides of each group of side glass are fixedly glued with a corresponding side of the main window glass. On the premise that requirements of a main visual field of an inner effective load are met, the splicing type conformal optical window has enough strength and enough rigidity to resist influences of an external environment, and requirements of dynamics performance and invisibility of an aircraft can be met.

Description

technical field [0001] The invention relates to the field of aviation equipment, in particular to a spliced ​​conformal optical window. Background technique [0002] As an important part of the aerial remote sensor observation system, the optical window is an important unit of the optical payload imaging system. When the payload is working, the imaging light enters the optical system through the optical window and is imaged on the target surface. Since the optical window is directly exposed to the complex external environment, it is affected by factors such as external acceleration, pressure, and heat, resulting in deformation and temperature gradients, which are prone to wavefront distortion, which directly affects the imaging quality of the payload. In addition, most of the optical windows are directly connected with the aircraft as a whole, which will have a relatively large impact on the aerodynamic characteristics and stealth characteristics of the entire aircraft syst...

Claims

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Application Information

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IPC IPC(8): G02B7/00
CPCG02B7/007
Inventor 程志峰刘家燕孔德杰王平张保
Owner CHANGCHUN INST OF OPTICS FINE MECHANICS & PHYSICS CHINESE ACAD OF SCI
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