Observation window for missile launching vehicle

A missile launch and observation window technology, which is applied in the field of car windows, can solve the problems of unsatisfactory radar stealth ability, insufficient visible light transmission performance, and unfavorable external observation, etc., and achieve simple structure, strong anti-electromagnetic pulse ability, and improved protection performance. Effect

Active Publication Date: 2017-10-24
BEIJING INST OF SPACE LAUNCH TECH +1
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Benefits of technology

The technical effect described in this patented technology relates to making a new type of temperature control device called Temperature Glass® used inside flight vehicles without adding any extra parts like windows or lamps. It achieves these benefits through a unique design made from two layers of different materials - one includes both opaque and clear films – while another contains only reflector material. These components work together to create a stable system where there is no air gap around them. By combining multiple layers of special properties, such devices provide improved protection against heat shock waves, radio wave interference, and enhanced visual reception capabilities compared to existing designs.

Problems solved by technology

The problem addressed in this patented text relates to improving the flight time (FoV) of guided weapons systems such as drones during nighttime operations due to poor visibility from traditional opaque reflective surfaces used on these targets. This can lead to reduced mission success rates when observers cannot see through the target's surface clearly enough.

Method used

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  • Observation window for missile launching vehicle
  • Observation window for missile launching vehicle
  • Observation window for missile launching vehicle

Examples

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Embodiment Construction

[0018] Such as Figure 1 to Figure 6 Shown is a specific embodiment of an observation window for a missile launching vehicle of the present invention, including tempered glass 1 and window frame 2 . Let the tempered glass 1 adopt a layered structure including an outer glass and an inner glass, and coat the outer surface of the outer glass with a transparent metamaterial film, coat the outer surface of the inner glass with a transparent metal film, and coat the outer surface of the inner glass with a transparent metal film. The edge is plated with silver paste, and the inner side of the inner glass is pasted with an explosion-proof film, so that the inner side of the outer glass and the outer side of the inner glass are connected by lamination. Simultaneously, let window frame 2 specifically comprise outer pressure frame 21 and inner pressure frame 22, limit ring 23 is set on the inner surface of outer pressure frame 21, allow outer pressure frame 21 and inner pressure frame 22 to

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PUM

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Abstract

The invention relates to an observation window for a missile launching vehicle. The observation window comprises tempered glass and a window frame, the tempered glass comprises outer-layer glass and inner-layer glass, a transparent super material film is plated on the outer side face of the outer-layer glass, a transparent metal film is plated on the outer side face of the inner-layer glass, silver paste is plated at the edge of the outer side face of the inner-layer glass, an anti-explosion film is pasted on the inner side face of the inner-layer glass, and the inner side face of the outer-layer glass and the outer side face of the inner-layer glass are connected through a lined adhesive. The window frame comprises an outer pressing frame and an inner pressing frame, a limiting ring is arranged on the inner side face of the outer pressing frame, the outer pressing frame and the inner pressing frame are detachably connected, a ring groove is formed among the outer pressing frame, the inner pressing frame and the limiting ring, and the tempered glass is put in the ring groove and pressed by the outer pressing frame and the inner pressing frame. The observation window has the advantages of wide wave-absorbing frequency band, high resistance to electromagnetic pulse and good light transmitting performance, has certain anti-explosion ability and can effectively improve survivability of the missile launching vehicle.

Description

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Claims

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Application Information

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Owner BEIJING INST OF SPACE LAUNCH TECH
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