Adjustable mounting assembly for tension member driven device

An assembly for an aircraft propulsion system, comprising:

• a housing;
• a rotor next to the housing;
• and
• a system including a mechanical load, a belt drive, a cradle, a first bracket, a second bracket and an adjustment link;
• the mechanical load operatively coupled to the rotor through the belt drive, and the mechanical load supported by and fixed to the cradle;
• the cradle extending longitudinally between a first end and a second end, the cradle extending laterally between a first side and a second side, the cradle coupled to the housing through the adjustment link at the first side, and the cradle pivotally coupled to the first bracket and the second bracket at the second side;
• the first bracket disposed next to the first end and fixed to the housing independent of the second bracket;
• the second bracket disposed next to the second end and fixed to the housing independent of the first bracket;
• and
• the adjustment link configured to change a distance between the housing and the cradle to adjust a tension of the belt drive.

An assembly for an aircraft propulsion system, comprising:

• a housing;
• a rotor next to the housing;
• and
• a system including a mechanical load, a belt drive, a cradle, a bracket and an adjustment link;
• the mechanical load operatively coupled to the rotor through the belt drive, and the mechanical load supported by and fixed to the cradle;
• the cradle extending laterally between a first side and a second side, the cradle pivotally coupled to the bracket at the second side;
• the bracket fixed to the housing independent of the adjustment link;
• and
• the adjustment link configured to change a distance between the housing and the cradle to adjust a tension of the belt drive, a first end of the adjustment link pivotally mounted to the cradle, and a second end of the adjustment link pivotally mounted to the housing.