Patent ID: 7104499

Claim:
A system for rechargeable compressed air supplemental thrust for an aircraft, comprising: an air intake, operable to receive air from the atmosphere and deliver the received air to a compressor; a first valve coupled to the air intake and operable to regulate the delivery of air from the air intake to the compressor based on control signals from a control unit; the compressor coupled to the first valve and operable to reduce the volume of air received from the air intake to generate compressed air for delivery to a tank based on control signals from the control unit; a second valve coupled to the compressor and operable to regulate delivery of compressed air from the compressor to the tank based on control signals from the control unit; the tank coupled to the second valve and operable to receive the compressed air from the compressor and store the compressed air; a third valve coupled to the tank and operable to regulate the delivery of air from the tank to a first nozzle based on control signals from the control unit; the first nozzle located off any wing and coupled to the third valve and operable to receive compressed air from the tank, further operable to release the compressed air to the atmosphere to provide thrust for the aircraft in a first direction; a fourth valve coupled to the tank and operable to regulate the delivery of air from the tank to a second nozzle; the second nozzle located off any wing and coupled to the fourth valve and operable to receive compressed air from the tank, further operable to release the compressed air to the atmosphere to provide thrust in a second direction; and a positioning unit coupled to the first and second nozzles and operable to position the nozzles in the first and second directions based on control signals from the control unit.