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时间:2011-03-26 14:43来源:蓝天飞行翻译 作者:admin
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 A. Program IGVs closed when speed is less than
 40 % and IGVs are 22 degrees when speed is
 equal or more than 40 %.
 B. Program Surge Control Valve open
 C. Program P2 = average of P2 for last 10 s
 Note: P2 calculated once per s
 (P2 = 0.875.Pt)
 3. If both P2 and Pt failed:
 -------------------------- Program P2 = 0.94 bar (13.66 psia)-----------------------------------------------------
2. DELTA P Sensor *  A. Program IGVs closed at 22 degrees (2.5 v)
 -------------------------- B. Program SCV open (O ma)-----------------------------------------------------
3. PT Sensor *  A. Program IGVs closed at 22 degrees (2.5 v)
 -------------------------- B. Program SCV open (O ma)-----------------------------------------------------
4. LCIT Sensor  A. Program T2 based on P2
 B. If P2 also failed: Program T2 based on
 -------------------------- programmed value P2.----------------------------------------------------
5. LVDT Sensor -------------------------- Program IGVs closed at 22 degrees (2.5 v)----------------------------------------------------
6. APU Sump Oil Sensor  Program oil temperature = 16 DEG. C
 -------------------------- (61 DEG. F)----------------------------------------------------
7. ECB  A. Program T2 based on P2
 B. If P2 also failed: Program T2 based on
 programmed value P2
 -------------------------- C. Program IGVs closed at 22 degrees (2.5 v)-----------------------------------------------------
8. LCDT  Set equal to last valid value

 -------------------------------------------------------------------------------
9. Generator Oil Temp Program oil temperature = 16 DEG. C
 (61 DEG. F) -------------------------------------------------------------------------------R **ON A/C 063-099, 401-499,

 

 B. Alternate Values for Failed Sensors
 (1) The ECB 59KD programs alternate values for certain failed LRUs. These are identified in the PUT or during the APU IOT. The LRU failures and the alternate actions are listed in Table 1. There is a time delay period between the failure of the LRU and program of the alternate value. The ECB uses the last value indicated before LRU failure.
 (2) Table 1 Alternate Values List for Failed Sensors -------------------------------------------------------------------------------Failed Action -------------------------------------------------------------------------------
1. P2 Sensor  A. On ground: use Pt,
 if Pt fails = 13,66 psia

 B. in flight: use Pt,
 if Pt fails = 7 psia -------------------------------------------------------------------------------
2.
 DELTA P Sensor calculated from Pt, P2 -------------------------------------------------------------------------------

3.
 PT Sensor  A. On ground: 13,66 psia


 B. In flight: 7 psia -------------------------------------------------------------------------------
4. LCIT Sensor  A. Program T2 based on P2
 B. If P2 also failed: Program T2 based on
 programmed value P2. ------------------------------------------------------------------------------
5. LVDT Sensor  A. When Bleed On: IGV max. 92 deg
 B. When no load: IGV max. 92 deg. at N > 80%
 IGV min. = 0 deg ------------------------------------------------------------------------------
6. APU Sump Oil Sensor A. Use Generator oil temperature
 B. If Gen. oil temp. fails = 110 deg. F
 (43 deg. C) ------------------------------------------------------------------------------
7. T2  A. Program T2 based on P2
 B. If P2 also failed: Program T2 based on
 programmed value P2 -------------------------------------------------------------------------------
8.
 LCDT Set equal to last valid value -------------------------------------------------------------------------------

9.
 Generator Oil Temp  A. Use APU sump oil temperature


 B. If Sump oil temp. fails = 110 deg. F
 (43 deg. C) -------------------------------------------------------------------------------


 CONTROL AND MONITORING - DESCRIPTION AND OPERATION
__________________________________________________
 1. General
_______ The Electronic Control Box (ECB) contains a Full Authority Digital Electronic Control (FADEC) to control the operation and monitoring of the Auxiliary Power Unit (APU). The ECB additionally provides communication to other aircraft systems. The ECB gives:
 -
Control of the automatic operation of the APU,

 -
Control of the APU at governed speeds,
 
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