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AES":yk49i2xe said:@mailee:
Not all aeroplanes (airliners) have two ailerons on each wing - please wait until tomorrow's pix (I do hope they haven't moved the A310 overnight)!
And to add to the "mysteries" of roll control, modern aircraft have both Spoilers and Speed Brakes on the upper surfaces of the wings. And in high speed cruise flight the Spoilers often "float" to assist the ailerons with the roll control. "My" Boeing 737 is a typical example (as are all B737s) and you should see the "Heath Robinson" mechanical mixers on the B737 - hiding in the RH Main Landing Gear Bay, which, with a series of "strings, pulleys and bellcranks", "mix" the amount of Spoiler movement of the "real" ailerons according to the speed of the aeroplane). But still, IMHO, it's better than the "plastic fantastic Scarebus" with it's multiude of invisible electrons wizzing silently along bits of wire - can you tell that I'm a mechanical bloke and not an avionics "fairy" at heart can't you?
Perhaps we'll get to gas turbines at a later date (not this trip from me though), although Bernoullui will stand you in good stead understanding those too.
Try that web link I posted yesterday.
Krgds
AES
A, I have just reread this post and realised that you would have LOVED the Britannia and its controll systems.
There were NO power controls on the aircraft. All of the control surface were 'free floating'. When it stood at the end of the runway, waiting for clearence for takeoff the ailerons and elevators were drooped, i.e. hanging fully down, and the rudder was blowing free in the wind! The control surfaces only had any authority when, rudder, 90 knots, elevators and ailerons about 110 knots and then they would come into line. They were totally free to move and the only thing that moved them in flight was a 5 or 6" servo tab along the trailing edge of those control surfaces. The tabs were moved with a series of 6 foot or so 'torque tubes' with universal connectors in line and the servo tubes went from the control coloumb to those control surfaces. The elevators were so sensitive that they had to had a 'feel simulator' to give the driver a sense of how much up/down he was putting in (no females in those daze).
It was a very sucessful system and there were several occasions where our Brits were leaving USAF bases and the tower would send an emergency message to stop the aircraft because the ailerons had failed and were both down! The normal response was "No problem, we have learned to fly with them like that :twisted: :twisted: "
Mailee, if you are worried about jet engines then you will love the `Bristol Proteus" because the air goes in the front, going backwards, then turns through 180º and goes backwards through the 12 stage compressor. Then it turns through another 180º and goes through the cans (the bit where it catches fire!), through the double turbine twin stage turbine and produces about 5,000 lbs thrust.
The double twin stage turbine? The first 2 rows of turbine blades are connected to the compressor and turn the 'jet' bit of the engine. The second 2 rows of turbine blade are connected through the centre of the main engine shaft to the proplellor gear box and turn the 16 foot prop. You with me so far??
The genral outcome is that you have a jet engine that is about the same length as an 'infernal conbustion engine' that runs on rough parafin (carasine (avtur), normal jet fuel) and is much more efficient at medium/ low altitudes than a pure jet 'cause it's got the big windmills on the front.