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
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
Chapter2: Loads On Structures
Section: Chapter Questions
Problem 1P
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