CPC F03D 13/30 (2016.05) [F03D 1/0675 (2013.01); G01M 5/0025 (2013.01); G01M 5/0075 (2013.01); F05B 2230/10 (2013.01); F05B 2240/302 (2013.01); F05B 2260/301 (2013.01); F05B 2260/83 (2013.01); F05B 2280/6003 (2013.01)] | 19 Claims |
1. A method for testing a rotor blade component of a rotor blade for a wind power installation, the method comprising:
dividing a rotor blade component of the rotor blade into a plurality of rotor blade component segments, and
forming a plurality of cutouts in a connection interface at a connection end of a first rotor blade component segment of the plurality of rotor blade component segments,
wherein:
the connection interface has a thickness corresponding to at least 1.5 times a diameter of one or more of the plurality of cutouts, and/or
the connection interface has a thickness of at least 2 cm, and/or
the connection interface has a depth which corresponds to at least 2 times a diameter of one or more of the plurality of the cutouts, and/or
the connection interface has a depth of at least 10 cm.
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