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I know how the analog Airspeed Indicator shows the Airspeed from the ram air pressure from the pitot tube. But I'd like to know how an ADIRU converts the raw pressure data to Airspeed that is displayed on a PFD.

  • What sensor is used for this purpose?
  • What exactly happens inside the ADIRU?
  • Does the sensor and / or procedure differ from unit to unit?
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  • $\begingroup$ Are you asking how the conversion from analogue to digital happens? $\endgroup$ – Rory Alsop Nov 1 '17 at 11:50
  • $\begingroup$ @RoryAlsop: Yes - what is the sensor being used, and is it standard in all ADIRUs? Also, how does the actual conversion actually happen? $\endgroup$ – ClobberXD Nov 1 '17 at 11:53
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    $\begingroup$ The sensor is the transducer into the pitot-static probe. A calibrated voltage is sent to the air data computer which uses some algorithm to compute the indicated airspeed (using temperature). Sensor are not standard, nor transducers. If the probe is only a pitot (total pressure), then an individual static pressure sensor is used and its signal goes to the AD unit too. See Wikipedia and Nasa $\endgroup$ – mins Nov 1 '17 at 13:33
  • $\begingroup$ Nice! What happens inside the transducer? i.e. Is there a membrane that is pushed / pulled (like a microphone) depending on the pressure difference? $\endgroup$ – ClobberXD Nov 1 '17 at 13:38
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    $\begingroup$ That was the case with aneroid capsule ASI, but in modern avionics the transducers are piezoresistive semiconductors on a Pyrex glass which generate a voltage. Try to not use the comments as a chat (better to refine your question) $\endgroup$ – mins Nov 1 '17 at 13:47
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Usually there is an intermediate module ADM (air data module) that makes the conversion from analog pressure into digital numerical value. One ADM will do this for the ram air pressure, another ADM will do the same for the static pressure. Their data are sent on Arinc numerical buses to the Air Data part of the ADIRU. Airspeed is basically the difference of the received data. Please refer to the following diagram:

https://upload.wikimedia.org/wikipedia/commons/f/ff/Airspeed_indication_system_-_fly_by_wire.png

Inside the ADM you have: first of all a PIEZO that will convert the mechanical pressure into electrical voltage, a piezo is somehow what you have in a balance you may use to get your weight. In the balance you have too an analog digital converter since the weight is displayed as a number.

Similarly in the ADM, the next item is an analog/digital converter that will convert the electrical voltage into a binary number that will be sent on the ARINC bus to the ADIRU

You might wonder why the ADM is apart and not inside the ADIRU, it is done like that to have the shortest possible pneumatic tube. I do understand I haven’t been enough clear in my previous answer that has been deleted, therefore it is important to understand the following:

The ADIRU managing Air Data and Inertial data, is located in an electronic bay, the pneumatic piping is not sent to the electronic bay, that will make a long distance, therefore no pressure conversion is done by the ADIRU, but by intermediate modules, the ADMs

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  • $\begingroup$ Now this is a much better answer! +1 $\endgroup$ – DeltaLima Jun 2 at 7:37

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