Method of repairing a mobile vane of a turbomachine, turbomachine vane and turbomachine comprising this vane
A technology of turbine blade and repair method, applied in the direction of blade support element, machine/engine, mechanical equipment, etc., can solve problems such as difficulty in implementing coating
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[0024] figure 1 The arrangement described in the EP 165860 patent is shown. The figure shows a rotor disk 1 of a turbine engine rotor with a flange on which a conical front cowl 3 is fastened. A plurality of approximately axial cavities 4 are machined on the rim of the rotor disk 1 using a broaching process. These cavities have a wedge-shaped cross-section matching the shape of the lower part 13' of the root 13 of the blade 10. The blade root 13 is that part of the blade 10 which is located below the platform 9 which forms the demarcation line of the gas flow. The locking key 11 slides over the lower portion 13' of the blade root 13, thereby locking the blade in the cavity. On the downstream face, the rim of the rotor disk has a radial flange 5 for securing a locking ring 7 and a sealing ring 8 by means of bolts 6 .
[0025] The locking ring 7 is provided with the same number of radially inward grooves 18 as the chambers, all facing the chambers. Furthermore, th...
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Abstract
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