쉐도잉 연습: ATPL Instrumentation - Class 1: Temperature and Time - 영상으로 영어 말하기 배우기

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If you're studying for your ATPLs and having a little bit of trouble with instrumentation, then this is the place to be.

Over the next few months, we're going to be breaking down all the topics within the instrumentation subject, analysing them and hopefully making them make sense for you in time for the exam.

Hi, I'm Grant and welcome to the first in a new series all about instrumentation.

There's lots of different things that we can measure on board an aircraft, and analyse to make certain decisions about where we need to go,

how high we need to fly and various other things.

The most fundamental and easy to understand though is temperature and time.

So we're going to start with them and slowly build up in complexity throughout the remainder of this course.

We need to sense the temperature of various components

so they don't overheat

and we also need to sense the temperature of the air around us to make sure we know

when to turn on any anti-ice systems and avoid any ice buildup.

We can measure temperature in Celsius, Fahrenheit or even Kelvin.

It doesn't really matter and the temperature probe will be calibrated to one of these

and then it can convert it if necessary or can do the conversions manually just like I've got at the top here.

So you've got Kelvin plus 273 equals Celsius.

Celsius times 9 over 5 plus 32 equals the Fahrenheit.

The simplest form of temperature sensor is to use a bi-metallic sensor.

This is where we use two different metals spiraled together and

when the temperature rises one metal will expand more than the other

which basically unwinds the spiral and rotates a needle on a display.

This is the sort of thing

that you might use to measure air temperature on a small aircraft

but you can't really measure the temperature of engine components

and display the information in a useful place because this biometallic strip can only be so long.

If you wanted to measure the temperature of the exhaust

and you wanted the display in the cockpit you need a biometallic strip

that went all the way to the back of the engine where the exhaust temperature was for example.

So simple, robust, very easy to understand but not

that useful for measuring some things but can be used in very simple applications.

A resistance temperature detector relies on a metal that will change in resistance when heated.

Four resistors are set up in this format essentially making a parallel circuit with a small battery outputting a consistent current.

The values of these three resistors are known and then this one down here is the variable resistance one.

As the resistance of this one changes it means

that the voltage passing through this side of a parallel circuit

measured at this point V2 will be different from the midpoint here at V1.

This resistor setup is fairly common in electronics

and it's called a wheat stone bridge if you're interested and want to look up more.

Because there is a difference in voltage between the two midpoints it means

that if we place a wire between point V1 and V2 we'll see that a current flows.

We can then use that current flow to turn a dial on a display

and the dial will turn based on how much resistance there is

because of how much voltage difference there is and that resistance changes depending on how much temperature there is.

So the temperature changes the resistance, changes the voltage, changes the voltage difference, turns the dial, gives us an effective display.

It's a good setup

and allows for the measurement of components from far away as all we need are longer wires to the display dial.

It does however need a constant DC power supply to make it work.

Thermocouples are used for very hot elements and work using a principle called Thermo-EMF, thermoelectromagnetic force.

This is when a metal creates a small voltage or electromagnetic force

when a temperature difference exists between two parts of the metal.

Basically say this is a metal rod

if it's hot over on the right hand side

and cold over on the left hand side a small voltage is produced in this metal.

Simple.

In a thermocouple we use two different metals.

We use metal one, let's just call it, and metal two in two sensing elements.

We also have a reference cold temperature.

This means we get a voltage difference produced when sensing a temperature which causes a current to flow.

Essentially we use that thermal EMF, we've got a hot and a cold, a hot and a cold we get a voltage generated in metal one

and a voltage generated in metal two because they're two different metals

that means that we're going to have a voltage difference

and then we do the same thing

that we did in the resistance temperature detector

and we hook up a dial and use the voltage difference and that current that's generated to turn the dial.

These are very effective because we can measure components from very far away just like we did with the

resistance temperature detector and it also doesn't need any power supply.

The problem is they aren't hugely accurate

so you wouldn't be using these for precision stuff

but depending on the metals used for the thermocouples they can

measure things at a very high temperature such as exhaust gas temperature in jet engines.

Air temperature is one of the most important things to measure

so that we can turn on any anti-icing systems when the temperature requires us to do so.

In light aircraft

that travel at low speed we tend to use a bi-metallic

type of temperature probe with the end of the gauge poking out into the airflow

and the dial giving us readings within the cockpit.

It's simple and effective but we run into a problem when we start to go faster.

Basically, as all the little particles in the air pass over the probe, they rub against it and create friction, causing the probe to heat up.

This distorts the results and doesn't give us a true reading

because we get this sort of kinetic heating effect whilst we're travelling through the air.

We therefore measure something that we call a total air temperature, or TAT.

and this is different from the actual air temperature which is the static air temperature

or sometimes referred to as the outside air temperature so you get sat, oat and tat.

That's a bit confusing and basically

when we add friction to the static air temperature we then are going to be measuring the total air temperature.

So how do we solve this problem?

Well we use clever design.

The most common type of probe and clever design that is used to get around this problem is called a Rosemount probe, which is I'm pretty sure a brand name,

but this style with a little variation is all over the place on different aircraft.

What happens in these probes is that air passes through this chamber past a small heater, which kind of seems a bit counter-intuitive,

but it's there to stop any ice formation on the front of this probe.

The venturi that follows the opening draws some of the air down into a sensing chamber

while the heavier particles that are in the air like water

or ice don't get drawn in and are free to pass by and they don't get sucked down into the sensing chamber.

In the chamber a resistance type temperature probe detects the heat of the air

before that air is dumped out the back of the probe.

The separate chamber eliminates most of the effects of the anti-icing heaters in the probe entry

and we can therefore get a reading for total air temperature

that is accurate and isn't affected by any need to de-ice

or anti-ice the probe

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and it also gets rid of all the particles in the air for a more accurate reading as well.

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It's important to note that this sort of probe will only work properly

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when it's moving through the air or has air moving through it.

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So when stationary, the air temperature readings will be way off and very, very high, especially if you've got the hot sun beating down on the probe, for example.

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So we've got our measure for true air temperature, but we want to know the outside air temperature or the static air temperature.

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What we do is we then use an equation

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or more specifically there'll be a little bit of electronics that does this calculation for you.

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The equation

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that we use is the static air temperature equals the total

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air temperature divided by 1 plus 3.2 times the recovery factor times the max squared.

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The equation has a few things to note.

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It must be used with Kelvin first of all,

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which confuses things because sometimes the recovery factor gets given the symbol k.

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And the recovery factor is essentially a measure of how efficient the probe is thermodynamically,

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as this equation is a thermodynamic expression, for how much heat is added to the air by the speed we are going through,

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hence the Mach number.

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So let's just put some numbers in this and talk through an example.

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So let's say we want to find out the outside air temperature, the static air temperature, and we have the following information.

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We've got a total air temperature is minus 40,

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that's what we measured, and we've got a recovery factor of 0.9

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and we've got a Mach number of 0.75 and we want to find out what is the

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static air temperature so the first thing we need to do is to convert it into Kelvin

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so we're going going to add 273 and

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that gives us an answer of 233 so 233 kelvin divided by 1 plus 0.2

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times 0.9 times 0.75 squared we'll just leave that in there for now

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and then I'll go away and do that on a calculator and see

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that we've got 233 divided by 1.10125 dot dot

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dot dot giving us a final answer in kelvin of 211.57 kelvin and if we wanted to convert that so let's

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just do it back over here so we've got 211.57 kelvin want to convert that back into

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um celsius so we take away 273

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and we get an answer so that's uh yes celsius is here that's going to give us minus 61.

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Yeah, 61.

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So we can see that the friction of us travelling through the air, we're going from minus 61 actual outside air temperature

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and we're adding about 20 degrees of friction to get us up to the total air temperature of minus 40.

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So it has a big effect whilst we're travelling at relatively high Mach numbers.

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In aviation, we measure things in UTC,

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universal time coordinate, which is a standardised time zone throughout the world.

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In the UK and parts of Europe, it is the same as the time in London, GMT, without daylight savings applied.

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And in other parts, it might be a few hours different from local, or even vastly different in places like New Zealand,

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where UTC is 12 hours different from local time.

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Basically, things can get confusing if you're referencing times to aviation related things like weather reports

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and arrival times which are all in UTC and then using your watch

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or phone which might be in local time especially

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when flying across different time zones with your phone maybe auto updating the time as you arrive in each place.

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So to save us and help us with

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that confusion we have a clock on the plane

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which is set to UTC time for referencing all these things like weather reports

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and arrival times etc and we call this the system clock.

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We use this as our time source when we are flying.

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These system clocks are the same as your wristwatch,

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usually a quartz based timekeeping device on smaller aircraft with larger aircraft having more complicated clocks with various features

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and they can use a GPS source to get an accurate time from the atomic clock

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on board the satellites up in space.

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They will also feature other things like a chrono which is a stopwatch used for timing short things.

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For example we need the engines to run at idle for

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at least three minutes before shutting them down after landing

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so we'd want to start the chrono shortly after landing to ensure we have achieved that three minute cool down time.

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We also have the elapsed time

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which we can use for longer timing typically for the time

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of pushback to the time of pulling back on stand again to get the block time of a flight, which is the flight time plus taxiing.

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Or we could use to record just the flight time by selecting it on just before take off

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and off just after landing.

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Another important use for an onboard system clock is to get

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an accurate measurement for how long the engine has been running and the the plane in general has been running.

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Engines have parts that need to be checked after a certain number of hours.

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So what we can do is we can manually record the startup

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and shutdown times in a tech log using the system clock

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and then we can get an accurate measurement of how long the engine has been running for

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and how often we need to service parts and

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when we need to service and check all of the components of the engine.

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Most aircraft will not rely on manually noting down the times though

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and they'll have a dedicated odometer that starts running when the engine starts and stops when the engine stops.

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This gives an accurate figure of how many hours the engine has been running for

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and it's kind of like the total mileage or total kilometreage odometer

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that you get on a car

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which gives an accurate figure of how long the engine has been on for

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and maintenance can be planned according to the figures on this odometer.

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In summary then you've got temperature sensing in a few different ways.

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Most simple is a bimetallic strip.

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You've got two different metals They untwine at different rates when heat is applied and the unspinning of one causes,

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faster than the other, causes a dial to move and we can measure temperature.

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Simple, but the biometallic strip limits how long it can be and how far away it can be from the source.

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You get resistive type elements that use a wheatstone bridge setup.

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the variable resistance reacts to heat and you'll get more or less heat and

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heat and more or less resistance according to that heat.

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You then get a voltage difference generated between each side of the Wheatstone bridge.

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That voltage difference creates a current that current can be used to turn a dial.

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They're good, they do rely on having a power source but it means that we can

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take this display and just attach some wires

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and send it to the cockpit away from the source of the temperature that we're measuring.

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You also get thermocouples which have the benefit of not needing power.

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They generate voltage when there's a temperature difference along their length.

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So it's going to be hot over here

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and it's going to be cold over here and that generates a voltage in this one metal, in this second metal,

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because it's a slightly different metal it means there's a slightly different voltage generated

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and we get two different voltages aka a voltage difference.

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Voltage difference means current can flow and we can use

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that flowing current to turn a dial which is proportional to the voltage difference and therefore proportional to the temperature

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and we get an accurate measurement of temperature in the cockpit.

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For air temperature sensing we generally on big aircraft use a rose mount probe.

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It's good because it means it's not going to

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ice up because there's heating elements here

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and then we draw air down into this sensing chamber

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and use a resistive type element to sense the temperature of the total air temperature

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and we get rid of all the particles of water

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and stuff in the air that might really affect and form this the result of the total air temperature.

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We then use electronics,

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we use an algorithm to calculate out what the static air temperature is compared to the total air temperature.

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The formula is static air temperature

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or outside air temperature equals the total air temperature divided by 1 plus 0.2 times the recovery factor times the Mach squared.

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These temperatures are in Kelvin.

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The recovery factor is a measurement of how efficient the resistive element

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and this system in general is and sometimes can be given the symbol k

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and then Mach is your Mach number

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which is going to be a measurement of how fast this air is flowing through the probe

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and how fast you're traveling through the air.

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So a few things to remember with this equation, but it's a good way of figuring out the outside air temperature versus the total air temperature.

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We also need to measure the time.

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Time is very easy to understand.

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It's UTC time, which is the universal worldwide time zone.

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Everything in aviation is referenced to UTC.

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So instead of using your watch where the local time might be vastly different to UTC,

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you can use the system clock which is always set to UTC for all aviation related things.

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And we can use accurate times from this to note down how long the engine's been running.

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And then we know how often we have to serve those parts and when we need to service those parts.

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항공기 계측기에 관한 이 비디오는 전문적인 내용을 쉽게 설명하는 대화체로 구성되어 있어, 영어 회화 연습에 최적입니다. 특히 기술적 용어와 일상적인 설명이 혼합된 구조는 실제 의사소통에서 필요한 유연성을 기르게 해줍니다. shadow speak(쉐도잉) 방식으로 따라하면, 자연스러운 발화 속도와 강세, 연결음을 익힐 수 있으며, 전문 분야의 영어도 동시에 학습할 수 있는 이점이 있습니다.

문맥 속 문법과 표현

"If you're studying for your ATPLs and having a little bit of trouble...": 조건문과 동시에 발생하는 상황을 표현하는 구조로, 일상 회화에서 자주 사용됩니다. "and"로 두 가지 상황을 연결하여 자연스러운 흐름을 만듭니다.
"the temperature probe will be calibrated to one of these and then it can convert...": 미래형과 "and then"을 사용하여 일련의 동작을 설명하는 패턴입니다. 기술적 내용을 설명할 때 유용하며, 순서를 명확히 전달합니다.
"This is where we use two different metals spiraled together...": "where"를 사용하여 장소뿐만 아니라 상황을 설명하는 구문입니다. 복잡한 개념을 쉽게 풀어낼 때 효과적입니다.

발음의 함정

이 비디오에는 몇 가지 발음이 어려운 단어가 있습니다. "bi-metallic"은 "바이-메탈릭"이 아니라 "바이메탈릭"으로 연결하여 발음하며, "thermocouples"는 "써모쿠플"이 아닌 "써모커플"로 발음합니다. 또한 "wheat stone bridge"는 "휘트스톤 브리지"가 아니라 "휘트스톤 브리지"로 강세를 "휘트"에 두어야 합니다. 영어 발음 교정을 위해 이 단어들을 반복해서 연습하고, 영어 쉐도잉 사이트에서 원어민 발음과 비교해보세요.

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문형	영상 속 표현
현재완료진행 have/has been + -ing — 전에 시작해 지금도 계속되는 동작	has been running · engine's been running
수동태 be + 과거분사 — 누가 하는지보다 무슨 일이 일어나는지에 초점	will be calibrated · are set · are known
관계절 who / which + 절 — 사람이나 사물에 대한 추가 정보	temperature which is · probe, which is · coordinate, which is
현재완료 have/has + 과거분사 — 과거의 일이 지금도 관련이 있을 때	have achieved · has been

쉐도잉이란? 영어 실력을 빠르게 키우는 과학적 방법

쉐도잉(Shadowing)은 원래 전문 통역사 훈련을 위해 개발된 언어 학습 기법으로, 다언어 학자인 Dr. Alexander Arguelles에 의해 대중화된 방법입니다. 핵심 원리는 간단하지만 매우 강력합니다: 원어민의 영어를 들으면서 1~2초의 짧은 지연으로 즉시 소리 내어 따라 말하는 것——마치 '그림자(shadow)'처럼 화자를 따라가는 것입니다. 문법 공부나 수동적인 청취와 달리, 쉐도잉은 뇌와 입 근육이 동시에 실시간으로 영어를 처리하고 재현하도록 훈련합니다. 연구에 따르면 이 방법은 발음 정확도, 억양, 리듬, 연음, 청취력, 말하기 유창성을 크게 향상시킵니다. IELTS 스피킹 준비와 자연스러운 영어 소통을 원하는 분들에게 특히 효과적입니다.

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ATPL Instrumentation - Class 2: Pressure Measurement.

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