• 热门标签

当前位置: 主页 > 航空资料 > 机务资料 >

时间:2011-03-25 18:01来源:蓝天飞行翻译 作者:admin
曝光台 注意防骗 网曝天猫店富美金盛家居专营店坑蒙拐骗欺诈消费者

 -
a 1 Mbyte flash EPROM

 -
a 512 Kbyte RAM
 The I/O2 board ensures:

 

 -DSI (discrete inputs) acquisitions,
 -ANI (analog inputs) acquisitions,
 -DGI (digital inputs) acquisitions,
 -DSO (discrete outputs) generations,
 -ANO (analog outputs) generations,
 -Power supply (5V plus or minus 15V) monitoring
 -Switching controls.

 (c)
 Connection between the two systems The dialogue is through 4 validity discretes (1 for each channel). During the functional test upon the landing gear extension an exchange of the codes sent over 8 discretes enables to test the two systems.

 (d)
 Operation At each energization the first system supplied takes control. The exclusion between the two systems is ensured by the software. If the two systems are supplied simultaneously the SYS1 has priority. If there is a disagreement between the control and monitoring channels of the system engaged:

 -
the system is disconnected, it cancels its validity bits and isolates its commands,

 -
the system in standby takes over. It validates its commands and ensures again all the functions of the unit with the same level of performance.

 


 1EFF : 401-499, 1 32-42-00Page 60 1 1 Config-2 Aug 01/05 1 1 1CES 1


 BSCU - Monitoring Channel - I/02 card
 Figure 031

 1EFF : 401-499, 1 32-42-00Page 61 1 1 Config-2 Aug 01/05 1 1 1CES 1


 (3) Software organization of the BSCU The BSCU is made of two systems physically distinct but functionally identical:
 -
System 1,


 -
System 2.
 The unit has two identical software programs (one for each system).
 Each system itself has two channels:

 

 -Control,

 -Monitoring.

 (a) Software architecture
 The software is divided into two parts:
 - operational software,

 -workshop maintenance software.
 Operational software
 The operational software includes:

 -
the functional software,


 -
the test software,


 -
the monitoring and test software.
 The functional software (braking control, anti-skid, ARINC 429
 management...) and the test software are integrated in the
 control channel.
 The monitoring software is integrated in the monitoring channel.
 The operational software is divided into modules as per the IDEFO
 method (ICAM Definition Method). The corresponding diagrams are
 given in the figures below:

 

 (Ref. Fig. 032, 033, 034, 035, 036, 037, 038, 039, 040)
 1EFF : 401-499, 1 32-42-00Page 62 1 1 Config-2 Aug 01/05 1 1 1CES 1


 BSCU Operational Software
 Figure 032

 1EFF : 401-499, 1 32-42-00Page 63 1 1 Config-2 Aug 01/05 1 1 1CES 1


 BSCU Operational Software
 Figure 033

 1EFF : 401-499, 1 32-42-00Page 64 1 1 Config-2 Aug 01/05 1 1 1CES 1


 BSCU Operational Software
 Figure 034

 1EFF : 401-499, 1 32-42-00Page 65 1 1 Config-2 Aug 01/05 1 1 1CES 1


 BSCU Operational Software
 Figure 035

 1EFF : 401-499, 1 32-42-00Page 66 1 1 Config-2 Aug 01/05 1 1 1CES 1


 BSCU Operational Software
 Figure 036

 1EFF : 401-499, 1 32-42-00Page 67 1 1 Config-2 Aug 01/05 1 1 1CES 1


 BSCU Operational Software
 Figure 037

 1EFF : 401-499, 1 32-42-00Page 68 1 1 Config-2 Aug 01/05 1 1 1CES 1


 BSCU Operational Software
 Figure 038

 1EFF : 401-499, 1 32-42-00Page 69 1 1 Config-2 Aug 01/05 1 1 1CES 1


 BSCU Operational Software
 Figure 039

 1EFF : 401-499, 1 32-42-00Page 70 1 1 Config-2 Aug 01/05 1 1 1CES 1


 BSCU Operational Software
 Figure 040

 1EFF : 401-499, 1 32-42-00Page 71 1 1 Config-2 Aug 01/05 1 1 1CES 1


 7. Operation/Control and Indicating________________________________
 A. Manual Braking
 (Ref. Fig. 041, 042)
 Manual braking is available when the Green hydraulic pressure is more
 than 150 bar (2176 psi) and one of these conditions occur:

 -
the left MLG or the right MLG is on the ground

 -
the average computed wheel speed is more than a specified value

 -
the ground speed (from the ADIRS) is less than a specified value.


 The operation of the brake pedal(s) causes the control lever(s) of the brake pedal transmitter unit (at the first officers position) to turn. The control lever(s) turns its related potentiometer which gives an electrical output to the BSCU. This output is in proportion to the angle through which the pedal(s) turn.
 
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 LANDING GEAR 起落架6(109)