Structures that can do more than just support:

Smart Structures & Materials

This class of materials allows for the straightforward implementation of functions within load-bearing mechanical structures. While in artifacts such as machines or buildings, these functions are realized by adding actuators or sensors, smart structures provide these functions alongside mechanical load in a very simple and elegant manner. An example is an aerodynamic wing structure made of shape memory metal, which undergoes significant deformation with temperature changes. Instead of complex structural solutions to alter the aerodynamic shape, such as aerodynamic flaps, smart materials render these technical elements unnecessary.
Among the well-known smart materials are shape memory alloys, plastics, magnetostrictive metals, and piezoelectric materials. Piezoelectric materials have a crucial advantage: they can be shaped by changing an electric voltage and can be easily commanded by electronic control. Additionally, they are inherently very fast.
Smart materials have been extensively utilized in research projects and tested in technology demonstrators. Shape memory materials have been studied in programs aiming to realize aircraft wings that avoid the aerodynamic drawbacks of flaps, such as the opening of gaps in the wing during flap operation. In helicopter blades, piezoelectric materials have been investigated to enable rapid shape changes of the rotor blade during rotation. These fast-responding aerodynamic profiles facilitate the suppression of vibrations and noise. Due to their rapid response, piezoelectric materials are ideally suited for combating body sound vibrations in machinery or noise-reducing structures.

Application examples from the aviation sector

Trailing Edge Servo Flap": Piezoelectric actuators (in red) with hub translation control aerodynamic flaps in a high-speed rotor blade.
Application: Fast rotor blade control of a helicopter EC135.
Morphing rotor blade with structurally integrated piezo actuators.

Grohmann B, Maucher C, Jänker P (2006) Actuation concepts for morphing helicopter rotor blades. In: Proceedings of the 25th international congress of the aeronautical sciences (ICAS 2006), Hamburg, Germany, 3–8 September, pp. 1–10.
Active strut with piezo actuators.

Jaenker P, Kloeppel V, Konstanzer P, et al. (2008) Piezo active vibration and noise control in helicopters. In: Proceedings of the 26th international congress of the aeronautical sciences, Anchorage, Alaska, 14–19 September, pp. 1–10.
The three piezo actuators can dynamically extend the strut. In a control system microphone - amplifier - strut, the propagation of body sound vibrations can be effectively isolated. Application: Suspension of the gearbox in a helicopter. The drive unit of the helicopter model EC135 is a rigidly connected unit, consisting of rotor, two turbines, and a gearbox. This unit is rigidly connected to the cell with 7 struts.
TVA Tuneable Vibration Absorber for A400M.
Application: Anti-Noisesystem for reductio of cabin noise (Airbus A400M )Active leaf spring made of composite material with integrated piezo actuators.  

P Konstanzer, M Grunewald, P Janker, S StormProceedings of the 25th international congress of the aeronautical sciences …, 2006•icas.org

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Constitutive Equations of Piezoelectricity

In the linear theory of the piezoelectric effect, a description of the small-signal behavior was developed (for further information see * 1 * 2). This theory does not include...
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Expansion and Force generation of Piezo Stacks

The real piezo actuator deviates significantly from a linear behavior in large-signal operation and the expansion shows a pronounced hysteresis behavior. There...
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Electrical Behavior of Piezo Actuators

Piezoelectric actuators exhibit electrical behavior similar to capacitors. This behavior is overlaid with the piezoelectric effect, which couples mechanical and electrical...
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Design Principles of Linear Piezo Actuators

There are two fundamental designs of piezoelectric actuators: I) Direct actuation with stacks. The most advancedadvanced type of piezo stacks is the...
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Guidelines for Sizing a Piezo Actuator

The feasibility of a planned application can be roughly assessed by comparing the application requirements with the characteristics of piezo stacks...
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Main Load Cases for Piezo Actuators

The linear constitutive equation of piezoelectricity describes a mechanically linear-elastic material with the superimposed effect of an electrically induced...
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Installation and Handling of Piezo Stacks

Piezo stack actuators are designed for uniaxial loading. A preload mechanism is often essential to achieve the best performance and a long service...
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