Integrated torque limiter/no-back device
A technology of torque limiter, reverse device, applied in the direction of transmission, brake type, mechanical brake, etc.
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[0012] figure 1 A typical slat actuation system 10 on an aircraft 11 is shown. The system is positioned on the left wing 12a and the right wing 12b of the aircraft 11 and includes a position indicating device 14, a power drive unit 16, a slat panel 18, a slat actuator 20, a slat panel linkage 22 and a torque shaft 30. Each slat panel 18 is connected to the wing 12a or 12b by two slat panel linkages 22 , wherein each linkage is connected to the slat actuation system 10 through a slat actuator 20 . Power drive unit 16 is connected to each slat actuator 20 by a torque shafting 30 .
[0013] Prior to flight or upon landing, power drive unit 16 powers slat actuator 20 to extend slat panel 18 away from wings 12a and 12b and into the airflow. The slat panel linkage 22 is used to extend the slat panel 18 and the position indicating device 14 works with the power drive unit 16 to hold the slat panel 18 in position. Once in flight, the power drive unit 16 powers the slat actuator 20...
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