5.14 Electromagnetic Environment Flashcards

1
Q

electric field strength can be measured in terms of

A

volts per metre

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2
Q

Electrostatic induction occurs when

A

a charged object redistributes charges to another object due to the attraction of opposite charges.

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3
Q

magnetic field strength is measured in

A

amperes per metre

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4
Q

As part of the EMC process, designers must look at two components:

A

Emission - what does the component emit?
Susceptibility - how susceptible is the component to outside emissions?

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5
Q

According to MIL-STD-461, Line Replaceable Units (LRU) must be designed with EMI-sensitive electronics located on one side of the enclosure, forming a

A

“Faraday cage” shielded from EMI effects . This ensures that sensitive microelectronic devices are operated in a protected environment

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6
Q

Cabling must be shielded and grounded to be protected against:

A

External radiated interference from passenger electronic devices, e.g., laptops and mobile phones
High-Intensity Radiated Fields (HIRF)
Lightning strikes

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7
Q

Electromagnetic Interference (EMI) can be defined as

A

the presence of unwanted voltages or currents that can adversely affect the performance of an electrical/electronic system

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8
Q

The effects of EMI include:

A

-Errors in indications
-Unwanted noise on audio signals
-Random patterns on electronic displays
-Repetitive ‘buzzing’ on intercom and cabin phone systems
-Desensitising of radio and radar receivers
-False indications in radar and navigation equipment
-Nuisance triggering of alarms

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9
Q

There are many sources of EMI throughout the aircraft these include

A

-Fluorescent lights
-Radio and radar transmitters
-Power lines
-AC powered window heat controllers
-Motors/generators, particularly if they are DC with commutators and brushes
-Switching and light dimming circuits
-Microprocessors
-Pulsed high-frequency circuits
-Data bus cables (but not fibre optic cables)
-Static discharge and lightning

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10
Q

In electromagnetic field radiation, energy is transmitted through what

A

electrically nonconductive paths, such as air, plastic materials, or fibreglass

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11
Q

The need for protection of modern electrical and electronic systems from HIRF is required because of the following factors

A

Dependence on these systems used for the continued safe flight and landing of the aircraft
Increased use of composite materials (reducing the natural Faraday cage protection of metallic structures)
Increased complexity of digital systems (faster operating speeds, higher-density integrated circuits)
Expanded frequency usage of microwave energy
Increased quantity and power of transmitters
The number of RF transmitters
Electrically initiated explosive cartridges e.g. fire bottle cartridges, helicopter winch cable cutter cartridges

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12
Q

High Intensity Radiated Fields (HIRF) are generated by certain Radio Frequency (RF) sources that are external to the aircraft. These fields disrupt electronic components and systems within the aircraft via currents that are induced from these fields into the aircraft’s wiring

A

.

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13
Q

Electromagnetic interference can jam equipment, burn out electrical circuits, cause false readings on instruments, cause a false command in a flight control system (especially fly-by-wire), detonate a squib, or even cause an explosion of fuel vapour

A

.

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14
Q

a common HIRF device found in aircraft galleys is a

A

microwave

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15
Q

HIRF interference can also be caused by high-power radio and microwave towers, including Air Traffic Control (ATC) primary surveillance radars.

A

.

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16
Q

aircraft protection from HIRF includes

A

HIRF protection features are incorporated inside the LRU.

Protection devices such as filter pin connectors, discrete filter capacitors and transient protection devices (transorbs) are installed within LRUs on one or more of the LRU interface circuits

17
Q

what is HERP

A

hazard of electromagnetic radiation to personnel is the danger to personnel from the absorption of electromagnetic energy by the human body

18
Q

in relation to HIRF and maintenance personnel

it is important to ensure all precautions are taken when

A

Working on or maintaining high energy sources such as radar systems, HF etc.
Fuelling and defueling of aircraft
Replacing fire extinguishers, fire extinguisher cartridges, helicopter winch cable cutter cartridges etc.

19
Q

aircraft have been required to comply with HIRF requirements since when

A

early 1992

20
Q

CS 23.1308 High Intensity Radiated Fields (HIRF) Protection

A

.

21
Q

Each electrical and electronic system that performs a function whose failure would prevent the continued safe flight and landing of the aeroplane must be designed and installed so that

A

the function is not adversely affected during and after the time the aeroplane is exposed to HIRF environment.

The system automatically recovers normal operation of that function, in a timely manner, after the aeroplane is exposed to HIRF environment.

The system is not adversely affected during and after the time the aeroplane is exposed to HIRF environment.

22
Q

most lightning strikes occur when

A

during the climb and descent phases of flight between
5,000 and 15,000ft

23
Q

likelihood of a lightning strike decreases significantly at what altitude

A

above 20,000ft

24
Q

Around 70% of lightning strikes occur during the presence of rain

A

.

25
Q

During a lightning strike, voltages can be superimposed on unprotected signals. These can increase the signal level up

A

to 500 times

26
Q

The currents produced by this phenomenon can be

A

300 000 times higher under normal conditions

27
Q

to protect against the indirect effects of a lightning strike, certain design features are implemented which are

A

Protected components are segregated, wire lanes are separated, and system components are protected by filters, which only allow spike free currents to access them

The filters have to be able to neutralise power with a magnitude of 500 kW.

28
Q

The direction of a lightning discharge can be calculated by an

A

Automatic Direction Finder (ADF) receiver using a loop antenna.

29
Q

Precipitation is termed ‘hard’ or ‘soft’ depending on the type of particles

A

Hard precipitation refers to relatively dry particles such as snow, ice, hail, and sand.

Soft precipitation refers to wet particles, such as rain and sleet.

30
Q

Optimum siting of dischargers can only be determined by

A

a thorough investigation of the characteristics of the aircraft type.

however in general the wing, tail and fin tips are the locations of the greatest potential gradient

31
Q

Measures to protect against lightning strikes and other forms of electromagnetic interference include

A

Proper grounding and shielding with inductances kept to as low a value as possible.
Grounded shields for external computer cables that run right up to the main grounding point.
Symmetrical or separated ground connections for all critical signals.
The separation of critical electronic circuits from interference-prone areas.
The eradication of voltage surges.

32
Q

to keep EMI contained by following the necessary maintenance procedures.

to ensure the continuing safety of the aircraft:

A

Bonding checks must be correctly carried out.
Bonding terminals must be correctly torque loaded.
Crimping compounds must be used where specified.
Cable screens must be correctly terminated and earthed.

33
Q

how can aircraft and their systems be protected against High-Intensity Radiated Fields (HIRF)

A

Through the use of Electromagnetic Interference (EMI) filters, electrical shielding of cables, good aircraft electrical bonding, and fitted electrostatic dischargers.

34
Q

which way do the magnetic lines of force travel if the current is flowing toward the receiver

A

anti-clockwise

35
Q
A