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Air Data System

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1- 0.2 * Computer Mach Number Squared. STATIC AIR TEMPERATURE. TS= Total Air Temp. 1 0.2 * Computer Mach Number Squared. TAT TEMPERATURE CURVE. TAT/ADIRU FUNCTION ... – PowerPoint PPT presentation

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Title: Air Data System


1
  • Air Data System
  • Total Air Temperature Probe
  • Use of NCEP Warm Bias Data
  • Presented by David Cole

2
BUG
3
Air Data System
4
Air Data System
5
AIR DATA MODULE
6
TAT PROBE
7
TAT FUNCTION
8
(No Transcript)
9
TOTAL AIR TEMPERATURE
  • ?tw Total air temperature error correction due
    to resistance of the nominal length of wiring
    between the probe and the air data computer
    (degrees).
  • TTi Indicated total air temperature - the total
    air temperature as measured at the input
    terminals of the air data computer (degrees
    absolute).

10
TOTAL AIR TEMPERATURE/STATIC AIR TEMPERATURE
  • TT Total air temperature - indicated total air
    temperature corrected for wiring resistance and
    recovery error (degrees absolute) the air data
    computer output in degrees C.
  • Ts Static air temperature - total air
    temperature corrected for the adiabatic
    temperature rise due to compressibility (degrees
    absolute) the air data computer output in
    degrees C.

11
FORMULAS
  • TOTAL AIR TEMPERATURE
  • TT Indicated Total Air Temp Total Air Temp
    Error Corr. Due to Wire Resistance
  • 1- 0.2 Computer Mach Number Squared
  • STATIC AIR TEMPERATURE
  • TS Total Air Temp
  • 1 0.2 Computer Mach Number Squared

12
TAT TEMPERATURE CURVE
13
TAT/ADIRU FUNCTION
14
TAT PROBE ANALYSIS
15
TAT PROBE REVIEW
  • NCEP DATA ALLOWS CAL TO ISOLATE TAT PROBES THAT
    HAVE A HIGHER THAN NORMAL TEMPERATURE READING
  • ISOLATION OF THESE PROBES ALLOWS CAL TO REPLACE
    THEM PRIOR TO A POSSIBLE FAILURE
  • CAL AND BOEING ARE IN THE PROCESS OF IDENTIFYING
    HOW A HIGHER THAN NORMAL TAT PROBE TEMPERATURE
    CAN ALTER FUEL MILEAGE
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