Stator Vanes

popaviator

Well-Known Member
I wanted to know more about stator vanes. The definition out of the book I'm reading states that "By reducing rotational air movement from the spinning blades, stator vanes sustain linear airflow through the compressor and aid compression." How does the stator vane reduce rotational air movement from the spinning blades?
 
They're angled to direct the flow in the opposite direction that the compressor blades are.

Imagine a fan rotating and directing air. That air is going to be swirling.

Now imagine a set of airfoils oriented in the opposite direction, in the airflow. They're going to counter the rotation of the airflow.

Does that make any sense? My Scotch was helping with that explanation . . .
 
They're angled to direct the flow in the opposite direction that the compressor blades are.

Imagine a fan rotating and directing air. That air is going to be swirling.

Now imagine a set of airfoils oriented in the opposite direction, in the airflow. They're going to counter the rotation of the airflow.

Does that make any sense? My Scotch was helping with that explanation . . .

Thank you scotch! :beer:
 
Well hell, mtsu_av8er used fewer words than me. :)

On some engines (e.g. CFM-56), the AOA of the stator blades can be varied to manage the pressure differential across rotor blades as the rotational speed of the engine changes (improving efficiency and preventing surges).

P&W engines use 2.5 bleed valves (between the LP and HP compressors) to manage the mass flow during engine speed changes. RR uses three rotors to have a more gradual transition among sections.

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The posts above kind of cover the "how" so I'll talk a little about the "why." Sort of another viewpoint along the same lines (but the above is pretty good, too):


Ok, so the compressors add energy to the airflow by spinning, right? And as we know, the compressor blades are each like a little mini wing, or airfoil in the flow, and they are arranged in a big disk. But there is not just one disk of compressor blades (at least not on any engine I can think of), but instead there are many different stages of these disks, and all of the stages are connected at the center of the disks to the same rotating shaft. Hence, all of the stages rotate at the same rotational velocity (for the simplest jet engines anyway. Many engines use two different sets of stages: a low pressure compressor which is sometimes called a fan section, and a high pressure compressor. In that case, all the stages on each "set" rotate at the same speed, but the two different sets rotate at different speeds, usually called N1 speed and N2 speed).

Now, if there were no stators the air would come through the first compressor stage and that stage would impart some rotation to the air. When it got to the second set of spinning blades it would already be spinning at almost the same speed as the second set of blades. Hence, without stators, there would be very little relative or maybe NO motion between the air and the second (or third, fourth, fifth, etc.) sets of blades. So those follow on stages would not do anything.

So to remedy the problem, between each rotating disk of blades that is attached to the central spinning shaft, there is another disk of blades that remains stationary. Those blades are attached to the engine shroud.

The result? Well instead of the first stage of blades imparting a spin to the air, (and the follow on stages doing almost nothing), the air just gets squeezed... Hence the name "compressor".

By the way, the turbine has spinning blades (rotors) and stationary blades (stators) also. Works the exact same as the compressor, except in reverse. Instead of the blades spinning causing the air to get squeezed, the squeezed and heated air releases that energy by un-squeezing and turning the turbine blades.

From an energy standpoint you can think of the air like a spring. Compressing the air in the compressor (and then heating it in the combustor) is kind of like squeezing a big spring. Energy is stored in it. Once the energy is in the air (or in a compressed spring) it can be used to cause things to move. A squeezed spring could be placed behind a toy car, for example to launch it down a race track. The compressed and heated air pushes against the blades of the turbine to spin them (like when you blow on a pin-wheel).
 
OK very simple, the compressor blades energize the air, the stator blades slow the air while increasing its pressure (It diverges the air between the stator blades), and repeat for every compressor stage. There's a lot more detail going on, but this is the simple explanation, learned from designing 3 compressor stages of a 12 compressor stage.

It has little to nothing to do with rotating air because the blades are twisted and the naca airflow changed along the compressor blade to prevent/minimize this. You have to construct and H-S diagram to really visualize this, just know that the stator is like a bunch of divergence chambers if V goes down, P must go up, but you can only slow the air so much to increase its pressure before you run out of energy, so you send it through another compressor blade to re-energize the stream and so on until you reach the desire pressure.

One last point, there is such a thing as inlet guide vanes, which are stators, (i.e. not rotating) at the front of some engines to help align the airstream and properly distribute the airflow before it enters the engine.
 
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