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Ice Protection Systems
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Detection
IceSight 2020
IceSight 2020E
IceSight RW
IceSight SAS
RCLASS
Ice Advisor
Icing Onset Sensor
Deicing
EIDI
Icewick
Heat Mat
Application
highway
vehicle
runway
pedestrian
Custom Development
Custom EIDI SPEED Calculation for GA Aircraft
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Enter Aircraft Parameters Below
Please use the form on the left to estimate system specifications. SPEED Design Program results are approximations. IDI does not guarantee accuracy of these example calculations.
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)
De-Icing Cycle Time:
15 second cycle
true checked> 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:
Aluminum
Carbon Fiber Composite
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)
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