摘要:
The present application provides an automated beverage dispenser for dispensing a beverage and ice into a cup. The automated beverage dispenser may include an ice dispensing station with an ice auger and a weight sensor, a beverage dispensing station, and a control device. The control device instructs the ice auger to fill the cup with a predetermined amount of ice and instructs the beverage dispensing station to fill the cup with a predetermined amount of the beverage in response to a weight of the cup as determined by the weight sensor.
摘要:
The present application provides an automated beverage dispenser using a number of cups and a number of lids. The automated beverage dispenser may include a lid stack with the number of lids, a lidding mechanism, and a positioning device for maneuvering the lidding mechanism so as to remove one of the number of lids from the lid stack and to attach the lid to one of the number of cups.
摘要:
An inlet door assembly and method for reducing noise from an auxiliary power unit (APU) contained within an aircraft housing is provided. The inlet assembly includes an inlet duct, an actuator, and a door. The inlet duct is configured to extend from the auxiliary power unit to the aircraft housing and has a sidewall that defines a flow passage through which APU noise propagates. The actuator is disposed at least partially within the inlet duct. The door coupled to the actuator. The actuator is also configured to selectively rotate the door between at least a first position, in which at least a portion of the door deflects APU noise in a first direction, and a second position, in which at least a portion of the door deflects the APU noise in a second direction.
摘要:
An inlet door assembly and method for reducing noise from an auxiliary power unit (APU) contained within an aircraft housing is provided. The inlet assembly includes an inlet duct, an actuator, and a door. The inlet duct is configured to extend from the auxiliary power unit to the aircraft housing and has a sidewall that defines a flow passage through which APU noise propagates. The actuator is disposed at least partially within the inlet duct. The door coupled to the actuator. The actuator is also configured to selectively rotate the door between at least a first position, in which at least a portion of the door deflects APU noise in a first direction, and a second position, in which at least a portion of the door deflects the APU noise in a second direction.
摘要:
An inlet door assembly and method for reducing noise from an auxiliary power unit (APU) contained within an aircraft housing is provided. The inlet assembly includes an inlet duct, an actuator, and a door. The inlet duct is configured to extend from the auxiliary power unit to the aircraft housing and has a sidewall that defines a flow passage through which APU noise propagates. The actuator is disposed at least partially within the inlet duct. The door coupled to the actuator. The actuator is also configured to selectively rotate the door between at least a first position, in which at least a portion of the door deflects APU noise in a first direction, and a second position, in which at least a portion of the door deflects the APU noise in a second direction.