产品概况:
Each multi rotor steel brake assembly is composed of one brake cylinder, one pressure-plate assembly with replaceable steel wear pads, two or more rotating discs (rotors) with sintered-friction material on a steel core, one or more stationary discs (stators) with replaceable wear pads, one torque-tube assembly with replaceable wear pads, along with necessary nuts, washers, and bolts.
Braking action begins to occur when hydraulic pressure is applied to the brake via the pilot’s or co-pilot’s master cylinders. As the hydraulic pressure reaches the brake it forces the pistons outward against the pressure plate assembly (with wear pads), which compresses the brake stack (rotors and stationary discs) against the torque tube assembly (with wear pads). This generated frictional force is transferred to the wheel/tire through the rotors, which have drive slots to engage the main wheel, and thus slows the aircraft.
The multi rotor steel brake assembly can be used with either a flange-driven or tubewell-driven wheel assembly, depending upon the initial design and application.
APPLICATIONS:
Primarily general aviation business aircraft or other higher gross weight aircraft requiring specific performance characteristics.
FEATURES AND ATTRIBUTES:
• Weight optimized for each application
• Robust design
• Live technical support
• Worldwide distributor network for commercial applications
OPTIONAL FEATURES: Designed to meet aircraft specifications and design parameters.
性能特点:
设计的局限性
| |
252,344 ft-lbs to 2,375,410 ft-lbs design landing KE; 531,043 ft-lbs to 5,900,000 ft-lbs rejected takeoff KE |
最大操作压力(psi)
| |
590 psi to 3000 psi |
材料
| |
Aluminum housing |
重量
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5.29 to 35.80 lbs per brake assembly |