BCU is also responsible for:
1) Anti-Skid Protection
2) Wheel locked protection
3) Touchdown protection
Anti-Skid Protection
What’s monitoring brake pressure?
Pressure transducers
Brake system consist of:
1) Normal braking
2) Emergency braking
3) gear retraction in-flight braking
How to check brake wear?
Top/bottom brake wear indicators
Locked wheel protection
* if one wheel speed is lower than others but 30% BCU will relieve all braking for that one wheel
What supplies normal brake system?
• Hydraulic system #1,2
• Electrically commanded and monitored
( Brake by wire )
Normal braking without valid ground WOW signals
Active down to 10kts ( use emergency brake to stop )
Touchdown protection
Whichever happens first:
1) WOW + 3 sec
2) Wheel speed of 50 kts
Done through BCU and Shut off valves
Electrical system of normal brakes
BCU
|
Shut off valves ( each side )
|
1,4------------2,3 ( brake control valves)