Bomble70
Mechanical
- Jun 25, 2014
- 4
Hi,
I'm looking for some advice/guidance as the attached problem is outside my experience as I'm a Manufacturing Engineer. Currently, I've been asked to assess the assembly of design whereby a component is retained within a casing by means of a retaining spring (comprised of 3 tabs). The parts are designed and supplied by a 3rd party and supplied to us for assembly into our design.
Based on the operating environment, the component needs a retaining force of ~44N under a minimum spring deflection of 0.3mm so we need an spring stiffness of ~49N/mm (44/3*0.3). However, due to the tolerances, the deflection can be 1.1mm so the retaining force is ~162N.
My concern isn't the force applied on the component under the min/max assembly gap but whether the deflection on the spring is feasible without breaking the tab (the spring is manufactured from beryllium copper with a yield stress of 190MPa). My instinct tells the current design isn't feasible but I don't have the experience to prove it!!.
I've attached a copy of the spring tab geometry but don't know how to determine the spring stiffness for the design and hence stress in the tab - I searched the forum for examples and found some threads that cover similar problems where the spring rate is determined using strain energy??
Hopefully, I defined the assembly issue but let me know if you need any further details.
Thanks for any help & advice
B70
I'm looking for some advice/guidance as the attached problem is outside my experience as I'm a Manufacturing Engineer. Currently, I've been asked to assess the assembly of design whereby a component is retained within a casing by means of a retaining spring (comprised of 3 tabs). The parts are designed and supplied by a 3rd party and supplied to us for assembly into our design.
Based on the operating environment, the component needs a retaining force of ~44N under a minimum spring deflection of 0.3mm so we need an spring stiffness of ~49N/mm (44/3*0.3). However, due to the tolerances, the deflection can be 1.1mm so the retaining force is ~162N.
My concern isn't the force applied on the component under the min/max assembly gap but whether the deflection on the spring is feasible without breaking the tab (the spring is manufactured from beryllium copper with a yield stress of 190MPa). My instinct tells the current design isn't feasible but I don't have the experience to prove it!!.
I've attached a copy of the spring tab geometry but don't know how to determine the spring stiffness for the design and hence stress in the tab - I searched the forum for examples and found some threads that cover similar problems where the spring rate is determined using strain energy??
Hopefully, I defined the assembly issue but let me know if you need any further details.
Thanks for any help & advice
B70