Rear navigation lamp with lower hemisphere plated with infrared filtering film

A navigation light and infrared film technology, applied in the field of aviation accessories

Pending Publication Date: 2022-03-08
BEIJING ZHONG CHUANG HU LIAN TECH CO LTD
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

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Problems solved by technology

[0004] The invention provides a rear navigation light with a lower hemisphere plated with an infrared filter film, which solves t

Method used

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  • Rear navigation lamp with lower hemisphere plated with infrared filtering film
  • Rear navigation lamp with lower hemisphere plated with infrared filtering film

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Embodiment Construction

[0023] The rear navigation light coated with the infrared filter film on the lower hemisphere provided by the present invention will be further described in detail below.

[0024] refer to Figure 1-2 , the present invention aims at the deficiencies and shortcomings of the prior art, and provides an external lighting device for the invisible lower hemisphere in the new infrared concealment mode in the aviation field. It is a double-mode function and invisible in the infrared concealment mode. rear navigation lights.

[0025] The rear navigation light of lower hemisphere plated infrared filter film provided by the present invention comprises: first light source, second light source and lampshade 3; Wherein,

[0026] The light emitted by the first light source is visible to the human eye, and the light emitted by the second light source is invisible to the human eye; wherein,

[0027] The rear navigation light is fixed on the aircraft fuselage and is vertically arranged, and t...

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Abstract

The invention provides a rear navigation lamp with a lower hemisphere plated with an infrared filtering film. The rear navigation lamp comprises a first light source, a second light source and a lampshade (3). Light emitted by the first light source is visible to human eyes, and light emitted by the second light source is invisible to human eyes; the rear navigation lamp is fixed on an aircraft body and is vertically arranged, and the first light source and the second light source are fixedly arranged in the rear navigation lamp and face the tail of the aircraft; the lampshade (3) covers the first light source and the second light source, the lower half portion of the lampshade (3) is plated with a filter membrane, the light transmittance of the filter membrane to the first light source is larger than the first light transmittance, and the light transmittance of the filter membrane to the second light source is not larger than the second light transmittance. And the filter membrane is used for preventing light rays emitted by the second light source from radiating towards the lower part of the airplane.

Description

technical field [0001] The invention belongs to the technical field of aviation accessories, in particular to a rear navigation light coated with an infrared filter film on the lower hemisphere. Background technique [0002] The rear navigation light is an important external lighting device of the aircraft. It is installed at the tail of the fuselage to display the maximum shape of the tail of the aircraft, provide its own position and direction of movement to other aircraft, and also help pilots visually identify other aircraft when flying at night. The heading of the aircraft, so as to grasp the situation of the surrounding airspace, and make timely predictions and corresponding measures. [0003] Most current aircraft use white LED lights as the light source for the rear navigation lights. However, there are some situations where only one's own side is required to be visible, and the existing rear navigation lights cannot be realized. Contents of the invention [0004...

Claims

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Application Information

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IPC IPC(8): F21S43/14F21S43/13F21S43/20F21V3/02F21V3/10F21W103/00F21W107/30F21Y115/10
CPCF21S43/14F21S43/13F21S43/255F21V3/02F21V3/10F21W2103/00F21W2107/30F21Y2115/10
Inventor 戚树腾李辉郝芯王建桢
Owner BEIJING ZHONG CHUANG HU LIAN TECH CO LTD
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