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Volume 2, Issue 1, 2011, Full Text - 5th International Conference on ...

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Sustainable C<strong>on</strong>structi<strong>on</strong> and Design <str<strong>on</strong>g>2011</str<strong>on</strong>g><br />

Table 1. Overview of how the interacting forces and slip are applied in full scale experiments<br />

Fatigue force Normal force Slip<br />

Dovetail<br />

c<strong>on</strong>necti<strong>on</strong><br />

Applied by actuator<br />

Due to actuator<br />

Due to geometry and<br />

fatigue force<br />

Bolted or<br />

riveted lap<br />

c<strong>on</strong>necti<strong>on</strong><br />

Applied by actuator<br />

Pre stress bolt or rivet<br />

Due to geometry and<br />

applied forces<br />

Wire rope Applied by actuator Pre stress by dead weight<br />

Due to geometry and<br />

fatigue force<br />

Wire rope<br />

c<strong>on</strong>necti<strong>on</strong><br />

Applied by actuator<br />

Pre stress by dead weight<br />

Due to geometry and<br />

applied force<br />

Press-fit<br />

c<strong>on</strong>necti<strong>on</strong>s<br />

Applied by electric motor<br />

and geometry<br />

Press fit geometry<br />

Due to geometry and<br />

applied forces<br />

Splined<br />

coupling<br />

Applied by actuator<br />

Pre stress by spring system<br />

Due to geometry and<br />

applied forces<br />

Threaded<br />

c<strong>on</strong>necti<strong>on</strong>s<br />

Applied by electric motor<br />

and geometry<br />

Pre stress in threaded<br />

c<strong>on</strong>necti<strong>on</strong><br />

Due to geometry and<br />

applied forces<br />

Leaf spring<br />

Applied by actuator<br />

Pre stress of leaf spring<br />

package<br />

Due to geometry and<br />

applied forces<br />

The next two paragraphs give more details about two full scale test rigs. The first test rig is used to test<br />

dovetail c<strong>on</strong>necti<strong>on</strong>s, a typical c<strong>on</strong>necti<strong>on</strong> technique in aircraft engines, steam turbines and other turbines.<br />

The sec<strong>on</strong>d test rig is developed to test wire ropes that are used as overhead c<strong>on</strong>ductors.<br />

3.1 Dovetail c<strong>on</strong>necti<strong>on</strong>s<br />

Modern aircraft engines (turboprop) are based <strong>on</strong> a turbo machine, fluid energy is c<strong>on</strong>verted into<br />

mechanical energy by means of a blade. The blade transfers the energy <strong>on</strong>to the rotor through a dovetail<br />

c<strong>on</strong>necti<strong>on</strong>. Due to the wedge-formed shape of the dovetail and the interacting forces <strong>on</strong> the blade, a slip<br />

arises between the blade and the rotor [13-15].<br />

A full scale experiment of a dovetail c<strong>on</strong>necti<strong>on</strong> is shown in Figure 3. The specimens have the shape of a<br />

dovetail c<strong>on</strong>necti<strong>on</strong>. The <strong>on</strong>ly force that is applied during the experiment is F, working in vertical directi<strong>on</strong>.<br />

There are two c<strong>on</strong>tact areas between the blade and the rotor, notice that this test rig has replaceable parts<br />

in the upper block. The dovetail c<strong>on</strong>necti<strong>on</strong> is failed due to fretting fatigue, a crack initiated in the c<strong>on</strong>tact<br />

area, and propagated through the specimen (crack in Figure 3).<br />

Figure 3. Dovetail fretting fatigue experimental setup with failed specimen [14].<br />

44<br />

Copyright © <str<strong>on</strong>g>2011</str<strong>on</strong>g> by Laboratory Soete

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