Patent ID: 8011033

Claim:
An aircraft sink system with integrated waste disposal function for disposing of waste matter through a vacuum waste system, the sink system comprising: a common drain line; a sink for draining the waste matter through a sink drain line, said sink drain line being connected to said sink and used to drain material from said sink; a storage area in direct communication, without obstruction, with the sink drain line said storage area used for receiving and storing the waste matter from the sink; a bypass line for supplying air into the storage area; a vacuum blower connected to the common drain line, said vacuum blower able to apply suction on the common drain line to remove matter from the storage area; a first valve having an open position and a closed position for controlling the amount of air supplied by the bypass line into the storage area; a second valve having an open position and a closed position for restricting flow of the waste matter from the storage area when in the closed position and draining the waste matter from the storage area to the common line when in the open position; and a controller connected to said first valve and said second valve; the controller having control logic to direct operation of the system in a drain mode or a disposal mode; the control logic for directing operation of the system in the drain mode setting the first valve to the open position and the second valve to the closed position, activation the vacuum blower, and setting the second valve to the closed position to end the drain mode; the control logic for directing operation of the system in the disposal mode first activating the drain mode, which thereby activates the vacuum blower, setting the second valve to the open position and the first valve to the closed position and setting the first valve to the open position and the second valve to the closed position.