Aircraft Dimensions:
Protected Wingspan (ft):
Protected Tailspan (ft):
Protected Vertical Stabilizer (ft):
Wing Chord Length (ft):
V/H Stabilizer Chord Length (ft):
Powerbus:
Aircraft has 270V DC Power Onboard
System should be powered on 28V DC
Ice Protection:
5% Chordwise Protection
10% Chordwise Protection
20% Chordwise Protection
System Electronics Configuration:
Centralized (Co-located DCU and ESBs)
Distributed (ESBs and High Current isolated to Wing and Tail)
| Please use the form left to estimate system specifications.
SPEED Design Program results are approximations. IDI does not guarantee
accuracy of these example calculations.
|
De-Icing Cycle Time:
15 second cycle
30 second cycle
60 second cycle
Clean Shed Ice Thickness:
(Maximum Residual Ice)
1/32 inch (60 Joule Actuator)
1/16 inch (30 Joule Actuator)
1/8 inch (15 Joule Actuator)
Actuator Installation Method
Actuators Bonded to Underside of Stock Leading Edge Structure with Brackets
Stock Leading Edge Structure Recessed for Actuators and Erosion Skin
..............Leading Edge Erosion Skin Type:
..............Leading Edge Erosion Skin Thickness (inches):
..............Include Leading Edge Erosion Skin in De-Ice System Weight
Ice Detector Count:
No Sensors
Single Sensor
Dual Sensors (Wing and Tail)
Quad Sensors (2 Wing and 2 Tail)
Your E-Mail Address:
