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Muhammad Istiaque Haider and Nathan Salowitz

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1 Muhammad Istiaque Haider and Nathan Salowitz
Residual Stresses Produced by Nickel Titanium after Undergoing Constrained Recovery Muhammad Istiaque Haider and Nathan Salowitz Department of Mechanical Engineering, University of Wisconsin - Milwaukee

2 Truck Steering Brackets
Motivation Vehicles face damage from fatigue, impacts, and overload events Truck steering knuckle stress concentrations Strength and fatigue issues prevent use of lighter weight materials Helicopter components face high cycle fatigue Armor faces damage from high velocity, projectile impacts Truck Steering Brackets Helicopters

3 Solution: Self-Healing Material
Micro-cracks Atomic diffusion Encapsulated adhesive Fracture SMA fiber composites Paradigm shift in design for realiaility

4 Limitations SMA cast in parent geometry
Intentionally (thermally cycling wire) Through manufacturing (casting in metal or exothermic epoxy reaction) At best returning fracture faces to adjacent positions Assuming no unrecovered strain No resulting load carrying capability

5 Approach: Residual Loads
Create residual loads in low temperature Martensitic state (after actuation, in un-actuated state) © Lagoudas

6 Approach Constrained recovery with return to low temperature state (martensite) results in residual loads- Post Constrained Recovery Residual Stress (PCRRS). Explore properties past constrained recovery Application of small strain Re-application of full (pre-working) strain Validation of the result for multiple formulations Microstructural analysis (ongoing) Publications in 2017 SMASIS and JIMSS

7 Methods Dynalloy Flexinol 90 NiTi
Ms = 75˚C Mf = 65 ˚C As = 90˚C Af = 110˚C TA Instruments Q800 Dynamic Mechanical Analyzer Integrated heating and cooling capabilities and Thermal extremes of 20 C and 115 C Maximum strains of 3.4, 3.9, 4.4 & 5.0% Note: temps up to 150 explored but found not to make a difference

8 Post Constrained Recovery Residual Stress (PCRRS) Generation
0) Thermally cycle free material Strain NiTi 3.4% strain Return to 0 stress state 0 stress, recoverable strain Hold strain & heat to 115 C “Blocking stress” Hold strain and cool to 23 C Residual Stress

9 Interest in Martensite
Approximate phase diagram Superimposed experimental data 1 3 6 7 5 4 2 8 Ms As Af Mf Manufacturer published transition temperatures Slope of transition lines approximated Point: data of interest thoroughly in martensite region Max temp of 115C used, tests were performed up to 150 with the same results

10 Continue Testing- 0.5% Small Strain Application
Cyclic small strains 0.5% Linear elastic Modulus between loading (early 1) & relaxation (3) Variation over 4 cycles < 20 MPa Decreasing trend (settling) 1 3 6 7 5 4 2 8 10 Consistent & stabilizing values suggest the small strain cycling is not inducing detwinning

11 Further Investigation with Exposure to Repeated 0
Further Investigation with Exposure to Repeated 0.5% Strain Application To clarify the cause and nature of the reduction of the PCRRS two more experiments was done- Subjected to a repeated thermomechanical cycle to train them and reduce potential variation that could be caused by grain boundary stabilization from cycle to cycle. Investigated the material response when subjected to a series of sets of 0.5% strain cycles followed by another thermal cycle and then more 0.5% strain cycles

12 Effects on Training Repeated cycling, or training, of SMAs can reduce variation in the stress- strain relation between thermal cycles. Samples were trained by exposing to thermal cycling (heating and cooling) in a fixed stress. To stabilize the hysteric response, this cycles were repeated for 20 cycles. Samples were later subjected to the same o.5% small strain application.

13 Effects on Training Comparison between the trained and untrained samples’ behavior beyond the PCRRS point is analyzed. Trained specimens produced slightly smaller initial PCRRS. After 0.5% strain application, the residual stress still decreased after each cycle. The trend even showed the same slope, or reduction in stress from cycle to cycle in the trained and untrained samples.

14 Regeneration of PCRRS Initial PCRRS could be recovered by subsequently exposing the sample to thermal actuation and constrained recovery. The thermal cycle through the reverse and forward transformations restored the residual stress with small, 10% variation. Repeating the full sequence of loads stabilized the material response by the 3rd full thermomechanical sequence.

15 Future Work Testing on other formulations Microstructural analysis
Theoretical development Extrapolation to other applications

16 Vision Generate residual compression in materials to inhibit fatigue damage Generate crack closing loads: Inhibit crack growth Generate residual strength in cracked structures

17 Integrate Technologies to Create Closed Loop System
Vision: SHM2 Integrate Technologies to Create Closed Loop System Structural health monitoring to initiate and evaluate self-healing materials Improved self-healing materials designed to support structural health monitoring

18 Acknowledgement Funding from the University of Wisconsin – Milwaukee
Advanced Structures Laboratory seed funding, contact Nathan Salowitz UWF SURF program Materials provided by Dynalloy SMArt Program Materials provided by SAES Getters S.p.A. SAES® Smart Materials (SSM)

19 Thanks!


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