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Design of an Automatic Control Algorithm for Energy-Efficient ...

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8 System <strong>an</strong>d functionality integration 79<br />

to the passenger.<br />

� � � �������� ¡ ����� � ������ ¡ ������ � ���������<br />

with ����� � ������ � ��������� ��.<br />

Scaling <strong>an</strong>d weight<br />

¡ ���������<br />

(8.11)<br />

As scaling a figure based on the PMV, called the predicted percentage <strong>of</strong> dissatisfied (PPD)<br />

could be used. It is defined as<br />

is found.<br />

��� �� ���� ¡ � � �������¡���� ������¡��� � �<br />

This gives as result <strong>of</strong> the thermal com<strong>for</strong>t objective function<br />

������ � ��� ¡ ����<br />

(8.12)<br />

(8.13)<br />

In DIN 7730, appendix D [7], <strong>an</strong> implementation <strong>of</strong> a thermal com<strong>for</strong>t calculation<br />

8.1.3 Air speed com<strong>for</strong>t<br />

As mentioned in Section 2.2.2, the air speed itself c<strong>an</strong> cause discom<strong>for</strong>t. Using a different<br />

com<strong>for</strong>t model, this objective could be included in a general thermal aspect. Here it has<br />

to be implemented in a separate function.<br />

The air speed towards the passengers is calculated by the air volume going through<br />

the face-outlets divided by their area. When reaching the persons the maximum speed<br />

��������� is reduced with a dist<strong>an</strong>ce � (assuming circular outlets with a diameter �������)<br />

[16].<br />

��������� ���� ¡ �������<br />

�<br />

��������<br />

¡<br />

������������� ¡ ����<br />

The temperature ch<strong>an</strong>ge in the jet is not taken into account here.<br />

(8.14)<br />

Based on Figure 2.3 <strong>an</strong> air speed com<strong>for</strong>t area is defined. Similar to the fogging

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