How can electrostatic discharge affect helicopters and their onboard equipment?

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Discussion Overview

The discussion revolves around the effects of electrostatic discharge (ESD) on helicopters and their onboard equipment. Participants explore the potential problems caused by ESD, methods of prevention, and the implications for both helicopters and fixed-wing aircraft. The conversation includes technical aspects of charge buildup, grounding methods, and safety considerations during operations.

Discussion Character

  • Technical explanation
  • Debate/contested
  • Conceptual clarification

Main Points Raised

  • One participant questions the problems ESD can cause to helicopters, particularly regarding the carbon fiber blades and potential charge buildup.
  • Another participant explains that aircraft are designed to ensure all surface panels are electrically connected to form a conducting cage, which helps prevent arcing and reduces effects on electrical systems.
  • Concerns are raised about the atmospheric static buildup on helicopters and the methods used to ground them, such as metal strips or conduction through landing gear.
  • A participant notes that they have not observed a helicopter discharging to the ground during landing or takeoff, citing the insulation provided by tires on aircraft like the Chinook.
  • Discussion includes the use of trailing wires or wicks to alleviate static buildup on helicopter surfaces.
  • One participant mentions the effectiveness of discharging wires or plates, which can control discharge rates to prevent rapid sparks.
  • Another participant asserts that Chinooks do charge their rotors and describes the dangers of improper grounding procedures when hooking up external loads.
  • The concept of the fuselage acting as a large Faraday cage is introduced, suggesting it may mitigate some ESD risks.

Areas of Agreement / Disagreement

Participants express differing views on the visibility and impact of ESD during helicopter operations. While some acknowledge the presence of charge buildup and the need for grounding, others question the extent and visibility of discharges during landing.

Contextual Notes

There are unresolved questions regarding the effectiveness of various grounding methods and the specific conditions under which ESD may pose risks to onboard equipment. The discussion reflects a range of experiences and observations, highlighting the complexity of the issue.

Who May Find This Useful

Individuals interested in aviation safety, electrostatics in aircraft design, and operational procedures for helicopters may find this discussion relevant.

TechSpec
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Hi

What kind of problems ESD can cause to a helicopter? Blades are usually made from a carbonfibre and they can cause electrostatic charge into a helicopter structure. Is there any method to prevent that to happen?
If that charging occurs, what happens when heli is landing, will it discharge itself into a ground with a spark, or is it prevented somehow?

What about charging differencies between different parts in a structure, let's say potential differencies. Helicopter blades are charghing themselves by static charge or some other parts in a helicopter, and its bodyshell is not, or charged less than other parts causing a potential differency between two parts. Is there a discharge happening time after time, or is this prevented by connecting different parts with a galvanic connection, wire or something like that?

How this charge/discharge can affect into a onboard equipments? radio interferency, radar etc.
Same sort of things might happen in a fixed wing plane too?TechSpec
 
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In aircraft you generally take great care to ensure that all the surface panels are electrically connected together forming a conducting cage.
This prevents arcing between panels but also reduces the effects on any electical systems inside the aircraft.
The atmospheric static built up on helicopters is a big problem, the ussually ground with either a metal strip on the undercarrigae or just rely on condution through the landing gear.

It is a major danger in rescue helicopters where you have to be very careful to let a grounding strap touch the deck first before grabbing hold of the basket/stretcher.
 
I have never seen a helicopter discharge to the ground when landing or taking off. For aircraft like a Chinook, we had the benefits of a landing gear with tires so you were well insulated. There are small trailing wires (wicks) to alleviate build up in surfaces:
http://www.precisionliftinc.com/images/pave-wicks.jpg
 
discharge

i have seen some pictures where a helicopter has a discharging "wire" hanging from a bottom of its shell. Those pictures were taken in a helicopter landing area on a floating oil pumping station somewhere. Those discharging wires or plates are best solution as you can control the discharge with a series of resistors and it would prevent charges to discharge rapidly with a spark.

I wonder why chinook helis don't discharge, or charge itself ?? If the heli charges itself it would probably be tens of thousands of volts, and it will discharge it even that there are rubber tires. If there is a potential differency, electricity will try to balance it no matter what ways, pilots steppin out from a heli, air discharge, langing gears, antennas, rubber tires and so on..
 
An oil platform is very different than solid ground.

Chinooks DEFINITELY charge their rotors. However, like I mentioned, they do have some trailing wicks on the landing gear tucked in between the tires. If they do discharge on landing, it definitely is not large enough to see with the naked eye. I have seen, plenty of times, what happens when someone trying to hook up an external load on the ground and does not follow proper grounding procedures (http://www.globalsecurity.org/military/library/policy/army/fm/3-21-38/image470.jpg and http://www.globalsecurity.org/military/library/policy/army/fm/3-21-38/image471.jpg). The static discharge is enough to knock you on your butt. It hurts...a lot.

We also had a hand held device called a shepherd's hook inside the aircraft. If we had to hook up an external load ourselves, we would use the shepherd's hook to grab the clevis to the sling through the hell hole. The hook was grounded to the structure of the aircraft. I assume that the entire fuselage acts like a large Faraday cage.
 
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