Example 23.19. A concentric spring for an aircraft engine valve is to exert a maximum force of 5000 N under an axial deflection of 40 mm. Both the springs have same free length, same solid length and are subjected to equal maximum shear stress of 850 MPa. If the spring index for both the springs is 6, find (a) the load shared by each spring, (b) the main dimensions of both the springs, and (c) the number of active coils in each spring. Assume G = 80 kN/mm² and diametral clearance to be equal to the difference between the wire diameters.

Mechanics of Materials (MindTap Course List)
9th Edition
ISBN:9781337093347
Author:Barry J. Goodno, James M. Gere
Publisher:Barry J. Goodno, James M. Gere
Chapter2: Axially Loaded Members
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Example 23.19. A concentric spring for an aircraft engine valve is to exert a maximum force of 5000 N
under an axial deflection of 40 mm. Both the springs have same free length, same solid length and are
subjected to equal maximum shear stress of 850 MPa. If the spring index for both the springs is 6, find
(a) the load shared by each spring, (b) the main dimensions of both the springs, and (c) the number of
active coils in each spring. Assume G = 80 kN/mm²2 and diametral clearance to be equal to the difference
between the wire diameters.
Transcribed Image Text:Example 23.19. A concentric spring for an aircraft engine valve is to exert a maximum force of 5000 N under an axial deflection of 40 mm. Both the springs have same free length, same solid length and are subjected to equal maximum shear stress of 850 MPa. If the spring index for both the springs is 6, find (a) the load shared by each spring, (b) the main dimensions of both the springs, and (c) the number of active coils in each spring. Assume G = 80 kN/mm²2 and diametral clearance to be equal to the difference between the wire diameters.
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