3. Analog Signals
______________
A. Inputs
-------------------------------------------------------------------------------| Signal | From | Acqn | I/P No. | Wire No.| |---------------------------------|----------------|------|---------|---------| | YAW V1 COM H | ) | C | ) 1 | ) 2 | | YAW V1 COM C | ) YAW | C | ) | ) | | | ) ACTUATOR | | | | | YAW V2 COM H | ) LVDT | C | ) 1 | ) 2 | | YAW V2 COM C | ) | C | ) | ) | |---------------------------------|----------------|------|---------|---------| | YAW V1 MON H | ) | M | ) 1 | ) 2 | | YAW V1 MON C | ) YAW | M | ) | ) | | | ) ACTUATOR | | | | | YAW V2 MON H | ) RVDT | M | ) 1 | ) 2 | | YAW V2 MON C | ) | M | ) | ) | |---------------------------------|----------------|------|---------|---------| | RUD TR V1 COM H | ) | C | ) 1 | ) 2 | | RUD TR V1 COM C | ) RUDDER TRIM | C | ) | ) | | | ) ACTUATOR | | | | | RUD TR V2 COM H | ) RVDT | C | ) 1 | ) 2 | | RUD TR V2 COM C | ) | C | ) | ) | |---------------------------------|----------------|------|---------|---------| | RUD TR V1 MON H | ) | M | ) 1 | ) 2 | | RUD TR V1 MON C | ) RUDDER TRIM | M | ) | ) | | | ) ACTUATOR | | | | | RUD TR V2 MON H | ) RVDT | M | ) 1 | ) 2 | | RUD TR V2 MON C | ) | M | ) | ) | |---------------------------------|----------------|------|---------|---------| | RTL V1 H | ) | C | ) 1 | ) 2 | | RTL V1 C | ) RTL | C | ) | ) | | | ) ACTUATOR | | | | | RTL V2 H | ) RVDT | C | ) 1 | ) 2 | | RTL V2 C | ) | C | ) | ) | |---------------------------------|----------------|------|---------|---------| | 28V+ | ) AIRCRAFT | C | ) 1 | ) 2 | | 28V GND | ) GENERATION | C | ) | ) | -------------------------------------------------------------------------------
1EFF : ALL 1 22-68-00Page 5 1 1 Feb 01/98 1 1 1CES 1 B. Outputs
-------------------------------------------------------------------------------| Signal | To | O/P No. | Wire No. | |--------------------------------|----------------------|----------|----------| | YAW SV ORDER H | YAW | ) 1 | ) 2 | | YAW SV ORDER C | ACTUATOR | ) | ) | |--------------------------------|----------------------|----------|----------| | RUD TR ORDER H | RUD TRIM | ) 1 | ) 2 | | RUD TR ORDER C | ACTUATOR | ) | ) | |--------------------------------|----------------------|----------|----------| | RTL ORDER H | RTL | ) 1 | ) 2 | | RTL ORDER C | ACTUATOR | ) | ) | |--------------------------------|----------------------|----------|----------| | CHASSIS GND | AIRCRAFT | 1 | 1 | |--------------------------------|----------------------|----------|----------| | AC 28V | FAC | 1 | 1 | | AC 28V GND | P/B SW | 1 | 1 | -------------------------------------------------------------------------------
1EFF : ALL 1 22-68-00Page 6 1 1 Feb 01/98 1 1 1CES 1 ARINC BUS INTERFACES (FAC) - DESCRIPTION AND OPERATION
______________________________________________________
1.
General
_______ (Ref. Fig. 001) The Flight Augmentation Computer (FAC) dialogues with the other components mainly through ARINC 429 digital information system buses. The figure shows the FAC interconnection. It is to be noted that the FAC data, except maintenance data, are transmitted to the other systems through the FAC main bus.
2.
Digital Outputs
_______________ This table contains all the output parameters in the digital form. They are sorted as per the numerical order of their output label. The infomation busses can be different between command and monitor channels: FAC OWN COM bus and FAC OWN MON bus. The following table gives:
-SYS LABEL SDI: (SDAC, FWC, DMC...) output label for which the parameter is available.
-PARAMETER DEFINITION: parameter name.
-RANGE ACCURACY: measurement range. Maximum value transmitted. When the digital value changes, the change step is equal to the accuracy.
-UNIT: unit in which the digital value is transmitted.
-SIG BIT: indicates whether a sign bit is available.
-DATA BITS: number of bits used by the parameter in the label.
-UPD/MSEC: output transmission interval. The refresh rate is given in
milliseconds.
-CODE:
BNR: binary data word
BCD: binary coded decimal data word
ISO: data word coded in ISO5 code
DIS: discrete data word
HEX: hexadecimal coded
HYB: mixed code
-ALPHA CODE: indicates the parameter mnemonic code.
-SOURCE ORIGIN: parameter source computer or system.
1EFF : ALL 1 22-69-00Page 1 1 1 Feb 01/98 1 1 1CES 1
FAC - ARINC Interface
Figure 001
1EFF : ALL 1 22-69-00 Page 2
1 1 Feb 01/98
1 1
1CES 1
-------------------------------------------------------------------------------
| PARAMETER LIST PARAMETER CHARACTERISTICS (NUMERIC) | -------------------------------------------------------------------------------|EQ.SYS.LAB.SDI|PARAMETER | WORD RANGE |UNIT|SIG |BITS|XMSN|CODE|ALPHA|SOURCE | | |DEFINITION| OPER RANGE | |BIT | |INTV| |CODE |ORIGIN | | |(*=REMARK)| RESOLUTION | | | | | | |BUS No.| | |(X=NOTE) | ACCURACY | | | | | | |ATA REF| | | | | | | | | | |CONV | -------------------------------------------------------------------------------| 1.047.00 |DSCRT DATA| |Deg | | 19 |175 |DIS | |SFCC | | 2.047.00 |WORD 1 | | | | | | | |27-81 | |(COM & MON) | | | | | | | | | | | |SLATS POS |Bit status 1| | 11| | | | | | | |VALID | | | | | | | | | | | | | | | | | | | | | |SLATS POS |Bit status 1| | 12| | | | | | | |0 DEG | | | | | | | | | | | | | | | | | | | | | |SLATS POS |Bit status 1| | 13| | | | | | | |>=21 DEG | | | | | | | | | | | | | | | | | | | | | |SLATS POS |Bit status 1| | 14| | | | | | | |>=26 DEG | | | | | | | | | | | | | | | | | | | | | |SLATS POS |Bit status 1| | 15| | | | | | | |MAX EXTD | | | | | | | | | | | | | | | | | | | | | |SLATS WTB |Bit status 1| | 16| | | | | | | |ENGD | | | | | | | | | | | | | | | | | | | | | |SLAT FAULT|Bit status 1| | 17| | | | | | | | | | | | | | | | | | |FLAPS POS |Bit status 1| | 18| | | | | | | |VALID | | | | | | | | | | | | | | | | | | | | | |FLAPS POS |Bit status 1| | 19| | | | | | | |0 DEG | | | | | | | | | | | | | | | | | | | | | |FLAPS POS |Bit status 1| | 20| | | | | | | |>=9 DEG | | | | | | | | | | | | | | | | | | | | | |FLAPS POS |Bit status 1| | 21| | | | | | | |>=19 DEG | | | | | | | | | | | | | | | | | | | | | |FLAPS POS |Bit status 1| | 22| | | | | | | |>=35 DEG | | | | | | | | | | | | | | | | | | | |
中国航空网 www.aero.cn
航空翻译 www.aviation.cn
本文链接地址：A320飞机维护手册 AMM AUTO FLIGHT 自动飞行2(46)
