Elevator control quadrant. The quadrant sketched here is part of control system for the wing-elevator of a commercial aircraft. It is to made of a light alloy (aluminum or magnesium) with the shape showr Figure 5. It weighs about 5 kg. The minimum section thickness is 5 m and (apart from the bearing surfaces) the requirements on surface fin and precision are not strict: surface finish s10 um and precision s0.5 m The bearing surfaces require a surface finish <1um and a precision <0

Structural Analysis
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ISBN:9781337630931
Author:KASSIMALI, Aslam.
Publisher:KASSIMALI, Aslam.
Chapter2: Loads On Structures
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Elevator control quadrant. The quadrant sketched here is part of the
control system for the wing-elevator of a commercial aircraft. It is to be
made of a light alloy (aluminum or magnesium) with the shape shown in
Figure 5. It weighs about 5 kg. The minimum section thickness is 5 mm,
and (apart from the bearing surfaces) the requirements on surface finish
and precision are not strict: surface finish s10 um and precision s0.5 mm.
The bearing surfaces require a surface finish s 1 um and a precision s 0.05
mm. A production run of 100-200 is planned. choice the suitable
processes to produce this part.
Transcribed Image Text:Elevator control quadrant. The quadrant sketched here is part of the control system for the wing-elevator of a commercial aircraft. It is to be made of a light alloy (aluminum or magnesium) with the shape shown in Figure 5. It weighs about 5 kg. The minimum section thickness is 5 mm, and (apart from the bearing surfaces) the requirements on surface finish and precision are not strict: surface finish s10 um and precision s0.5 mm. The bearing surfaces require a surface finish s 1 um and a precision s 0.05 mm. A production run of 100-200 is planned. choice the suitable processes to produce this part.
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