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Stretchable static electricity discharge device for aircraft

An electrostatic discharge device, retractable technology, applied in the direction of aircraft electrostatic discharger, aircraft lighting protector, etc., can solve problems such as rubbing or damage

Inactive Publication Date: 2018-11-23
COMAC +1
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

The longer the length, the better the charge will be gathered at the tip and released. During the parking period on the ground, the static electricity is mainly discharged through the wheels. The electrostatic discharger does not work, but the discharger still sticks out of the body. The longer it is, the easier it is to cause friction or damage

Method used

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  • Stretchable static electricity discharge device for aircraft
  • Stretchable static electricity discharge device for aircraft
  • Stretchable static electricity discharge device for aircraft

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Embodiment Construction

[0039] Reference will now be made in detail to various embodiments of the invention, examples of which are illustrated in the accompanying drawings and described below. While the invention will be described in conjunction with exemplary embodiments, it will be appreciated that present description is not intended to limit the invention to those exemplary embodiments. On the contrary, the invention is intended to cover not only the exemplary embodiments but also various alternatives, modifications, equivalents and others, which may be included within the spirit and scope of the invention as defined by the appended claims. implementation plan. For ease of explanation and precise definition in the appended claims, the terms "upper", "lower", "inner", "outer", "left" and "right" as well as "front" and "rear" are used with reference to Features of the exemplary embodiments are described in terms of their positions shown in . Exemplary embodiments of the present invention will be d...

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PUM

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Abstract

The invention provides a stretchable static electricity discharge device for an aircraft. The device comprises a storage cylinder, a static electricity discharge device pole and an actuator, wherein the storage cylinder is installed on an aircraft body, at least part of the static electricity discharge device is contained inside the storage cylinder and can move between the retracting position andthe stretching position, at the retracting position, at least part of the static electricity discharge device is retracted into the storage cylinder, and at the stretching position, the static electricity discharge device pole stretches out relative to the retracting position; the actuator drives the static electricity discharge device pole to move between the stretching position and the retracting position. The static electricity discharge device can stretch and retract as needed, and the phenomenon that the device is impacted accidentally and damaged when the device is in the ground parkingstate is avoided.

Description

technical field [0001] The invention relates to a retractable electrostatic discharge device for aircraft. Background technique [0002] When the aircraft is flying, the surface of the aircraft is rubbed against dust, ice crystals, rain and other particles, the charged exhaust gas of the engine, and the induced charge generated by the charged cloud layer on the aircraft will all cause the aircraft to be electrified. If the generated charge is not discharged in time, there will be a large potential difference between the aircraft and the surrounding atmosphere, forming a corona discharge channel. The broadband electromagnetic field generated during this period is one of the main sources of noise that interferes with the receiver. The electromagnetic field passes through the skin surface and openings of the aircraft, and may couple with the avionics equipment, thereby causing failure of communication, navigation, and computer control, and even serious damage or accident of the...

Claims

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Application Information

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IPC IPC(8): B64D45/02
CPCB64D45/02
Inventor 宋金泽王闪闪
Owner COMAC
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