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> OT: Airliner air conditioning, I know someone here will know this...
URY914
post Nov 5 2004, 02:17 PM
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On a car the a/c compressor runs off the engine.
In a house the a/c compressor is run by an electric motor.

(you can figure out my next question, can't you?)

How is the compressor on a airliner (737, 747,etc) powered?
I've never noticed a big v-belt on the engine before.

If it is powered by a electric motor, if so how is the generator powered? Is there some type of power take off from jet engines?

Thanks,

Paul
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Cano
post Nov 5 2004, 02:21 PM
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It is my understanding, from watching something on the History Channel on the history of HVAC (It was more interesting than it sounds, really) that jet engines compress the air coming into them, and that this compressed air is taken from the engines before fuel is mixed in and burned. Hopefully someone else can elaborate a bit more.
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GaroldShaffer
post Nov 5 2004, 02:26 PM
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I thought the pilot just opened a window (IMG:style_emoticons/default/blink.gif) (IMG:style_emoticons/default/cool_shades.gif)

Ok ok I know (IMG:style_emoticons/default/slap.gif)
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Allan
post Nov 5 2004, 02:27 PM
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Engine bypass air.
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URY914
post Nov 5 2004, 02:29 PM
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QUOTE(Headrage @ Nov 5 2004, 12:27 PM)
Engine bypass air.

WTF does that mean.

I was on a plane last week an it hit me that the real cool stuff doesn't start until we get in the air with the engines really humming.
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Allan
post Nov 5 2004, 02:35 PM
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On all the planes I worked on, they had ducting that would divert engine intake air to a turbine that was used for the hvac system.
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SLITS
post Nov 5 2004, 02:37 PM
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Also, consider the temp of the intake air at altitude - real a/c
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URY914
post Nov 5 2004, 02:38 PM
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So the turbine would only be spinning with enough speed to power the compressor when the plane is in the air.

Correct?
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2-OH!
post Nov 5 2004, 02:45 PM
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On the ground, air is bled off the APU (auxillary power unit - small jet engine) ducted into the heat exchangers and then fanned into the cabin...Once the engines are running, (APU off) air is bled off the 13th and 6th stages of the compressor (on each engine) then run through the heat exchangers and fanned into the cabin...The reason it's not so cool is because the bleed air is around 450 degrees and so it just cannot cool fast enough before it goes into the cabin...Ambient air also plays into the equation...The hotter the day, the hotter the bleed air, the longer it takes to cool it down...However, the air speed through the duct system is constant, so it does not get to linger or re-circulate through the exchangers again...

Once in the air, outside RAM air comes in to help and very quickly when you figure 35,000 feet is around 40 below 0...Also, the tube (airframe) becomes cooler instantly at that temp...

Except for the Concorde...That airplane growns 11.12 inches in flight due to heat expansion...Every flight...Remember, metal has memory...What happens to a paper clip after you bend it 100 times...

2-OH!
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Kerrys914
post Nov 5 2004, 02:45 PM
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Well in flight. How about no compressor at all (IMG:style_emoticons/default/ohmy.gif) (IMG:style_emoticons/default/ohmy.gif)

The air outside the plane is cold enough to cool the cabin. They more then likely need to add heat to it before it enters the cabin. This is kind of the same concept large buildings use for cooling requirments in the winter season so they don't need to run a chiller.

Cheers (IMG:style_emoticons/default/beer.gif)
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maf914
post Nov 5 2004, 03:39 PM
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QUOTE(Kerrys914 @ Nov 5 2004, 12:45 PM)
Well in flight. How about no compressor at all (IMG:style_emoticons/default/ohmy.gif) (IMG:style_emoticons/default/ohmy.gif)

The air outside the plane is cold enough to cool the cabin. They more then likely need to add heat to it before it enters the cabin. This is kind of the same concept large buildings use for cooling requirments in the winter season so they don't need to run a chiller.

Cheers (IMG:style_emoticons/default/beer.gif)

Sounds good, but remember at 35,000 feet the air is pretty thin. The stewardesses may like the idea of unconscious passengers, but I don't think that would fly with the flying public! (IMG:style_emoticons/default/laugh.gif)
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redshift
post Nov 5 2004, 03:48 PM
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lol


m
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spare time toys
post Nov 5 2004, 03:50 PM
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It takes air off the compressor section. Depending on what stage it is coming off of it could be upwards of 490 Deg. F( if over that you should get a pack trip) It then goes into a precooler at the pylon. From there it goes into two big heat exchangers and an air cycle mechiene ( think a big turbo) and past the 35 degree valve then into a water seperator. The 35 deg. valve injects hot air back in so the water seps dont freeze.After that it goes into the distribution bay at the back of the forward bag bin then off to cool little Timmy on his way to Grandmas. The out flow valve at the rear closes to start presureization. but as you climb the pres actually decreases from ground pres. The cabin altitude will climb to aprox 10000 feet while the airframe is at 30000+ when you come down it increases the cabin pres to field elevation. That is basicaly it. Hope this helps.
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SLITS
post Nov 5 2004, 04:00 PM
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And if you board a plane in Norfolk, VA in the summertime, it blows snow (IMG:style_emoticons/default/sad.gif)
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J P Stein
post Nov 5 2004, 04:00 PM
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The new CF 7E7 is gonna eliminate bleed air ducting.
They'll use a hellforstout APU to do the work conventionally done by bleed air.

This makes the airplane MUCH simpler to build and, with the CF fuselage, they can raise the humidity in the cabin to a much more comfortable level.
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spare time toys
post Nov 5 2004, 04:11 PM
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QUOTE(J P Stein @ Nov 5 2004, 05:00 PM)
The new CF 7E7 is gonna eliminate bleed air ducting.
They'll use a hellforstout APU to do the work conventionally done by bleed air.

I would be willing to bet this idea gets scrapped. The airlines will not want to run an APU in flight just to run the packs when they have good engines they can pull air off for virtually no cost
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Elliot_Cannon
post Nov 5 2004, 05:37 PM
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Bleed air ain't free.
Cheers, Elliot
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Dominic
post Nov 5 2004, 06:05 PM
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QUOTE(spare time toys @ Nov 5 2004, 01:50 PM)
It takes air off the compressor section. Depending on what stage it is coming off of it could be upwards of 490 Deg. F( if over that you should get a pack trip) It then goes into a precooler at the pylon. From there it goes into two big heat exchangers and an air cycle mechiene ( think a big turbo) and past the 35 degree valve then into a water seperator. The 35 deg. valve injects hot air back in so the water seps dont freeze.After that it goes into the distribution bay at the back of the forward bag bin then off to cool little Timmy on his way to Grandmas. The out flow valve at the rear closes to start presureization. but as you climb the pres actually decreases from ground pres. The cabin altitude will climb to aprox 10000 feet while the airframe is at 30000+ when you come down it increases the cabin pres to field elevation. That is basicaly it. Hope this helps.

(IMG:style_emoticons/default/agree.gif) Except for the cabin altitude part....35000 FT at 8.2 psi differential pressure is around 5500 FT cabin altitude.
I spent a lot of hours in the air controlling the pressurization (IMG:style_emoticons/default/biggrin.gif)
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J P Stein
post Nov 5 2004, 06:26 PM
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QUOTE(spare time toys @ Nov 5 2004, 02:11 PM)

I would be willing to bet this idea gets scrapped. The airlines will not want to run an APU in flight just to run the packs when they have good engines they can pull air off for virtually no cost

It's a done deal....but I will bet 50 bucks if you insist (IMG:style_emoticons/default/laugh.gif)
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Elliot_Cannon
post Nov 5 2004, 07:18 PM
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Martin,
That's why you get the big bucks.
cheers, Elliot
PS Congrats.
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