Ventilation cooling equipment and method for avionics equipment

A kind of avionics equipment, ventilation and cooling technology, applied in the construction of electrical equipment components, separation methods, cleaning with electrostatic method, etc., can solve the problems of reducing electrical distance, taking a long time, destroying the insulation strength of electrical equipment, etc., to avoid failure , clean up fast effect

Inactive Publication Date: 2021-04-30
ZHENGZHOU UNIVERSITY OF AERONAUTICS
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0002] With the rapid development of modern science and technology, the electronic equipment of advanced aircraft is increasing, and the power is also increasing. Moreover, when the electronic equipment on the aircraft is working, the power loss of components is usually expressed in the form of heat dissipation, thus A large amount of heat energy is emitted, which makes the internal temperature of the equipment continuously increase, and the change of temperature also has a significant impact on the failure of components. Therefore, it is more important to cool these electronic equipment. Electronic equipment that often needs to be cooled includes control-type internal The control panel and the control cabinet in the bilge, the cooling method usually used at present is ventilation cooling, through the air compressor to transmit the compressed air to the electronic equipment that needs to be cooled, or to introduce cooling air from the cockpit to cool the electronic equipment Ventilation and cooling, but when cooling air is introduced into electronic equipment, it is inevitable that dust and other substances attached to the air will be brought into electronic equipment. Due to the chargeability of dust particles (dust particles floating in the air have 90 %-95% posi

Method used

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  • Ventilation cooling equipment and method for avionics equipment
  • Ventilation cooling equipment and method for avionics equipment
  • Ventilation cooling equipment and method for avionics equipment

Examples

Experimental program
Comparison scheme
Effect test

Example Embodiment

[0047]Embodiment 1, this embodiment provides an air electronic device ventilation cooling device, referring to attachmentfigure 1 ,,,,,,,,,,,,,,,,,,,,,,,,,,,,,,,,,,,,,,,,,,,,,,,,,,,,,,,,,,,,,,,,. The device is in a closed state when cleaning the process), referring to the attachmentimage 3 AttachFigure 4 As shown, we are provided with a ventilation cooling tube 2 on the bottom wall of the control cabinet 1 and a ventilation cooling tube 2, which transmits the outside air to the ventilation cooling tube 2 through the air compressor, or directly hold the cabin The internal cooling air is transmitted in the ventilation cooling tube 2, and the electronic device is ventilated as a cooling control, and several groups of electrostatic dust removal equipment are disposed above the ventilation cooling tube 2, and each set of electrostatic dust removal equipment core equipment includes a dust collecting plate 3. And the transmitting board 4, we connect the dust plate 3 and the transmitter 4 a...

Example Embodiment

[0049]Example 2, when the first blade plate 9 on the surface of the dust collecting plate 3 is cleaned up in the surface of the dust collecting plate 3, the dust has a certain adsorption, and the first scraper is still having a certain amount of adsorption. If the inclined surface of the plate 9 will remain on the dust from the dust collecting plate 3, if it is not cleaned up in time, the cleaning effect of the device will be reduced, referring to the attachmentFigure 7 AttachmentFigure 8 AttachFigure 9 As shown, we are located in the blade and the rotating shaft 10 and the link 8 are vertically rotated with the second screw 12, and the second screw 12 thread is fitted with the inclined surface of the first scraper 9 vertically slide together. The second scraper 13, and the upper end of the first blade 9 is provided with a support plate 14 sliding longitudinally in the control cabinet 1, and we rotate on the support plate 14 and mounting a sector torch gear 15 and the sector slope g...

Example Embodiment

[0051]Example 3, on the basis of Example 1, reference attachmentFigure 5 AttachFigure 6 As shown, the first driving device includes a longitudinal rotation mounted to a drive screw 22 below the first wire 5 below the lateral end of the control cabinet 1 and the drive lead screw 22 is fixed to the first chain transmission side by a fixed mounted in the control cabinet 1. The first motor 23 is driven, the first motor 23 is connected to an external power source and is electrically connected to a controller. We screw the drive ramp twisted with the inner wall of the control cabinet in the drive lead screw 22 and drive it. The rack 24 is rotatably mounted to the drive torch gear 25 adjacent the first motor 23 lateral side, and the drive tie gear 25 is driven to drive the drive active cone 26 on the control cabinet 1. Moreover, the driving active cone gear 26 is engaged with a driven driven cone 27 that is fixed at one end of the first wire 5 longitudinal to the first motor 23, and drives...

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Abstract

According to ventilation cooling equipment and method for avionics equipment, the problem that the time consumed when electrostatic dust removal equipment only adopts vibration to remove dust is relatively long is well solved, a first scraping plate continuously reciprocates on the surface of a dust collection plate through continuous swinging of an eccentric plate, so that the dust is scraped off. The first telescopic rod on the rotating shaft is matched, so that dust on the surface of the dust collecting plate is cleaned more quickly and thoroughly; a second scraping plate is arranged on the first scraping plate, and after the first scraping plate stops moving on the dust collecting plate, the second lead screw rotates in a reciprocating mode through cooperation of the long rod and the wedge-shaped rod, so that the second scraping plate slides on the working face of the first scraping plate in a reciprocating mode, and dust remaining on the first scraping plate is scraped off again; and dehumidification equipment is further arranged, so that the situation that the electronic device is short-circuited due to the fact that condensate water is generated when cooling air meets hot air in the electronic device is avoided.

Description

technical field [0001] The invention relates to the technical field of avionics equipment, in particular to a ventilation and cooling equipment for avionics equipment. Background technique [0002] With the rapid development of modern science and technology, the electronic equipment of advanced aircraft is increasing, and the power is also increasing. Moreover, when the electronic equipment on the aircraft is working, the power loss of components is usually expressed in the form of heat dissipation, thus A large amount of heat energy is emitted, which makes the internal temperature of the equipment continuously increase, and the change of temperature also has a significant impact on the failure of components. Therefore, it is more important to cool these electronic equipment. Electronic equipment that often needs to be cooled includes control-type internal The control panel and the control cabinet in the bilge, the cooling method usually used at present is ventilation coolin...

Claims

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Application Information

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IPC IPC(8): H05K7/20B08B6/00B08B1/04B08B1/00B01D53/26
CPCB01D53/26B08B1/005B08B1/007B08B1/04B08B6/00H05K7/20145H05K7/2029H05K7/20381
Inventor 张贺磊张翼耿直郭霄张翔于浩森
Owner ZHENGZHOU UNIVERSITY OF AERONAUTICS
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