Disclosed is a brake disc 210a for an aircraft wheel brake comprising: a temperature sensing device 300 comprising a surface acoustic wave, SAW, sensor element and a sensor antenna, wherein: the temperature sensing device 300 is attached to the brake disc 210a by means of a ceramic adhesive 602 and one or more ceramic bolts 604. The brake disc 210a may be annular in form and have a hole through the centre to receive a torque tube 218, and a notch 605 intended to receive a spline of the torque tube. The temperature sensing device 300 may be mounted in the notch 605. Also disclosed is a method of attaching a temperature sensing device to a brake disc of an aircraft wheel brake.
Wheel brake and temperature sensing device
2023-11-29
Patent
Elektronische Ressource
Englisch