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FX-H617-W19 Bi-spectrum Rotorcraft Camera RS232 two-channel SDI video output

FX-H617-W19 Bi-spectrum Rotorcraft Camera RS232 two-channel SDI video output

FX-H617-W19 Bi-spectrum Rotorcraft Camera RS232 two-channel SDI video output

  • Cname:Thermal Devices
  • Views:Times
  • Release date:2021-09-14 10:39:45

        

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Bi-spectrum Rotorcraft Camera.docx


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  • Applications
  • Features
  • Parameter

Uncooled thermal imaging cameras and visible light cameras (hereinafter referred to as "equipment") are mainly used for active rotorcraft equipment, which can detect and display the road conditions underneath the rotorcraft in day and night or in low visibility weather conditions such as smoke, fog, rain, and snow. The video image, assist the driver to drive the rotorcraft.

infrared imager

The equipment is mainly composed of infrared thermal imager, visible light camera and wiring harness (including communication line and power line). The equipment is installed at the front end of the rotorcraft to facilitate the collection of ground information. The device is connected to the integrated display with an aerial plug cable. The aerial plug cable includes DC:12V power supply for the device, serial communication RS232, and two-channel SDI video output.

The equipment can be used to identify ground routes, personnel, and equipment without any light source lighting (especially in wind, fog, rain, and snow); it can identify terrain undulations; it can smoothly guide the driver to lift the rotorcraft.


There are two options of the resolution: 640x512 and 384x288, both adapt optical 19mm fixed lens.

Dimension: (107.0±1.0mm)×(107.0±1.0mm)×(56.5±1.0mm)(L*W*H)


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a) High image quality, high recognition of scenes and obstacles;
b) Waterproof performance, high reliability, and solid structure;
c) Automatic window heating and defrosting to meet the use under various bad weather;
d)The weight of the equipment is small, less than 1kg.


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Structure and working principle
The working principle of the uncooled infrared thermal imaging camera is: the infrared radiation of the target object is focused to the photosensitive surface of the infrared focal plane detector through the infrared optical system. The infrared photoelectric conversion array of the detector converts the optical signal into electrical signal, and the core circuit The electrical signal is sampled by AD to obtain a digital video signal, and then processed by an image algorithm to output an infrared thermal image to the display.

The working principle of the visible light camera is: the light signal is collected by the sensor (CMOS), and the light signal is converted into an electrical signal. The movement circuit converts the electrical signal into a digital video signal, and then encodes to present an image, and then passes the image algorithm After processing, the visible light image is output to the monitor for display.

Bi-spectrum Rotorcraft Camera

Model

FX-H617-W19-V02

FX-A317-W19-V02

Infrared performance

Sensor type

VOx Uncooled FPA

Resolution

640*512

384*288

Wavelength

8μm~14μm

Pixel size

17μm

Optical focal length

19mm

Thermal FOV

≥28.4°×21.4°Horizontal × vertical

Frame Rate

≥25Hz

≥50Hz

NETD

≤50mK

Start-Up Time

≤20s25±2℃)

Operating distance (when the visibility is 8km, the temperature difference between the target and the background is not less than 5)

1) For human (1.7m×0.7m): identification distance≥ than 90m;

2) For vehicles (3.0m×3.0m): identification distance≥  300m

Thermal correction

Automatic NUC

Visible performance

Sensor type

CMOS

Resolution

1920×1080

FOV

≥28.4°×21.4°

Frame Rate

≥25Hz

Dynamic range

≥60db

Start-Up Time

≤5s (25±2)

Environmental illuminance range

Support 1Lx10000Lx

Operating distance

Identify 0.6m×0.6m objects in the range of 100m

Power Supply

Rated supply voltage

12VDC

Supply voltage range

9V36VDC

Normal temperature power consumption

≤10W

≤8W

Power consumption @low temperature heating

≤25W

≤22W

External interface (aviation plug)

Video format

Two-channel PAL

Communication

RS232

Environmental adaptability

Working temperature

-40℃~55

Storage temperature

-55℃~60

Vibration

GJB 150.16A-2009

Shock

GJB 150.16A-2009

Low pressure

GJB150.2A-2009

Rain test

GJB150.8A-2009

Damp heat test

GJB150.9A-2009

Mold test

GJB150.10A-2009

Salt spray test

GJB150.11A-2009

Sand and dust test

GJB150.12A-2009

Window usage

Deicing heating

Physical characteristics

Weight

≤1kg

≤1kg

Dimension (mm)

107×107×56.5

107×107×56.5

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