How can electrostatic discharge affect helicopters and their onboard equipment?

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    Emi
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SUMMARY

Electrostatic discharge (ESD) poses significant risks to helicopters, particularly due to the carbon fiber blades that can accumulate static charge. Grounding methods, such as metal strips and trailing wicks, are employed to mitigate these risks during landing. The Chinook helicopter utilizes trailing wicks to manage static buildup, preventing visible discharges. Proper grounding procedures are critical, especially in rescue operations, to avoid dangerous static shocks when handling external loads.

PREREQUISITES
  • Understanding of electrostatic discharge (ESD) principles
  • Familiarity with helicopter design, particularly materials like carbon fiber
  • Knowledge of grounding techniques in aviation
  • Awareness of safety protocols for handling external loads in helicopters
NEXT STEPS
  • Research grounding methods for helicopters, focusing on metal strips and trailing wicks
  • Study the effects of electrostatic discharge on onboard equipment like radios and radar
  • Examine safety protocols for rescue operations involving helicopters
  • Learn about the design and function of Faraday cages in aviation
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Aerospace engineers, helicopter maintenance technicians, safety officers, and anyone involved in helicopter operations and design will benefit from this discussion.

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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