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时间:2011-03-26 09:12来源:蓝天飞行翻译 作者:admin
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 High Pressure Bleed Valve - Schematic
 Figure 010A

R 1EFF : 004-049, 055-099, 101-149, 151-199, 1 36-11-00Page 55 1201-299, 301-399, 401-499, 1Aug 01/05 1 1 1CES 1R **ON A/C 001-049, 052-099, 101-149, 151-199, 201-299, 301-399, 401-499,

 

 (3) Controls and Indicating HP bleed valve operation is fully pneumatic. The lower ECAM display unit indicates its position (open or closed) on the BLEED page (Ref. Fig. 011) The two BMCs monitor the operation of the HP bleed valve (close microswitch signal, and transfer pressure level). They receive and process the signals and transmit the information per data bus by the System Data Acquisition Concentrator (SDAC) to the ECAM system which generates the system display (Ref. 36-20-00). (Ref. Fig. 012) Additionally, they transmit the information to the Centralized Fault Display Interface Unit (CFDIU). The CFDIU generates maintenance information which is displayed on the Multi Function Control Display Unit (MCDU) if the MCDU MENU is selected. (Ref. Fig. 013, 014, 015)
 **ON A/C 001-049, 052-099, 101-105, 151-199, 201-228, 301-302,
 (Ref. Fig. 016)

R **ON A/C 106-149, 229-299, 303-399, 401-499,
 (Ref. Fig. 016A)

R **ON A/C 001-049, 052-099, 101-149, 151-199, 201-299, 301-399, 401-499,
 (Ref. Fig. 017, 018, 019)
 **ON A/C 051-051,
 (3) Controls and Indicating HP bleed valve operation is fully pneumatic. The lower ECAM display unit indicates its position (open or closed) on the BLEED page (Ref. Fig. 011) The two BMCs monitor the operation of the HP bleed valve (close/open microswitch signals, and transfer pressure level). They receive and process the signals and transmit the information per data bus by the System Data Acquisition Concentrator (SDAC) to the ECAM system which generates the system display (Ref. 36-20-00). (Ref. Fig. 012)
R 1EFF : ALL 1 36-11-00Page 56 1 1 Aug 01/05 1 1 1CES 1


 ECAM Upper and Lower Display Units Figure 011 
R 1EFF : 1 1 1CES  ALL  1 111 36-11-00 Page 57 Aug 01/05

 

 ECAM - Generation Figure 012
 1EFF : 1 1R 1CES  ALL  1 11 1 36-11-00 Page 58 Aug 01/05

 

 CFDS Menu
 Figure 013

R 1EFF : ALL 1 36-11-00Page 59/60 1 1 Aug 01/05 1 1 1CES
1


 LAST LEG REPORT Page Figure 014
 1EFF : 1 1R 1CES  ALL  1 11 1 36-11-00 Page 61 Aug 01/05

 

 PREVIOUS LEGS REPORT Page Figure 015 
R 1EFF : 1 1 1CES  ALL  1 111 36-11-00 Page 62 Aug 01/05

 

 LRU IDENT Page
 Figure 016

R 1EFF : 001-049, 051-099, 101-105, 151-199, 1 36-11-00Page 63 1201-228, 301-302, 1Aug 01/05 1 1 1CES 1


 LRU IDENT Page Figure 016A 
R 1EFF : 1 1 1CES  106-149, 229-299, 303-399, 401-499,  1 111 36-11-00 Page 64 Aug 01/05

 

 CURRENT STATUS Page Figure 017 
R 1EFF : 1 1 1CES  ALL  1 111 36-11-00 Page 65 Aug 01/05

 

 CLASS 3 FAULTS Page Figure 018 
R 1EFF : 1 1 1CES  ALL  1 111 36-11-00 Page 66 Aug 01/05

 

 INTENTIONALLY BLANK


R 1 1


36-11-00Page 67
1 1 Aug 01/05 1 1 1CES 1


 TEST Page Figure 019 (SHEET 1)
 1EFF : 1 1R 1CES  ALL  1 11 1 36-11-00 Page 68 Aug 01/05

 

 TEST Page Figure 019 (SHEET 2) 
R 1EFF : 1 1 1CES  ALL  1 111 36-11-00 Page 69 Aug 01/05

 

 Additionally, they transmit the information to the Centralized Fault Display Interface Unit (CFDIU). The CFDIU generates maintenance information which is displayed on the Multi Function Control Display Unit (MCDU) if the MCDU MENU is selected. (Ref. Fig. 013, 014, 015, 016, 017, 018, 019)
 **ON A/C 001-049, 051-099, 101-149, 201-299, 301-399,
 B. Bleed Pressure Regulator Valve (PRV)
 **ON A/C 001-003, 052-054, 056-056,
 (Ref. Fig. 020)
 **ON A/C 004-049, 055-055, 057-099, 101-149, 201-299, 301-399,
 (Ref. Fig. 020A)
 **ON A/C 051-051,
 (Ref. Fig. 020B)
 **ON A/C 001-049, 051-099, 101-149, 201-299, 301-399,
 (1) The PRV is a 4 in. dia. butterfly-type valve, normally spring-loaded closed in absence of upstream pressure. A minimum upstream pressure of 8 psig is necessary to open the valve. The PRV pneumatically regulates the downstream pressure to 44 plus or minus 1.75 psig. It closes automatically in the following cases : - overtemperature downstream of the precooler exchanger (257 plus or
 minus 3) deg.C (60 s delay), - overpressure downstream of the PRV (57 plus or minus 3) psig (15 s delay),
 -ambient overheat in pylon/wing/fuselage ducts surrounding areas,
 -APU bleed valve not closed,
 
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