mtv wrote:NoCOpilot wrote:mtv wrote:So by that definition, ANY airspeed system is in fact an "Angle of Attack Indicator", since EVERY airspeed system in fact measures ram air pressure and compares it to static pressure.
There's not a static port on these differential pressure AOA systems, rather two ram ports at some angle to each other. If your AOA system acts like an ASI, or vise versa, then you're not doing it right. I've flown a bit in a Rans with a Dynon Skyview equipped with their optional AOA pitot tube (AOA integrated into the pitot tube, one of the two AOA ram ports is also the pitot port, but same principle as the standalone AOA systems), and they work quite well.
You can question the usefulness of having AOA information in the cockpit, but the operational principle of these devices is sound and totally different than an ASI.
My point was, that's a very poor definition of what a REAL AOA sensor looks like. Here's an image of a more typical AOA sensor:
The Piper Warrior pitot mast is remarkably similar to what one of these general aviation systems uses as a sensor. I'll post a photo when I can get through the snowdrifts to a hangar....
MTV
Well, there's more than one way to skin a cat, but it still tastes like chicken in the end!
Here's a photo of the Differential Pressure AOA vane/sensor on the Military Airplane I fly. Did I mention it was a Differential Pressure AOA system and not a mechanical flying wing sensor? The interesting thing about diff pressure sensors are they can sense angular changes faster than a mechanical flying wing (rheostat type) sensor...but I'm only talking about milliseconds. The bottom line is that it doesn't have to look like the image you posted to be an true AOA sensor/system.


Hey Vick!
How's the sand? Have you been "Chiefed" lately?
Semper Paratus (Always Something?)
or
Solum Volamus, Fieri Alam





