Apparatus for mixing high and low pressure air from a jet engine
AssigneeThe Boeing Company
InventorsLarry L. Linscheid, Philip M. Mueller
Life of this patent
Estimating the term…
Abstract
An apparatus for mixing high and low pressure air from a jet engine and introducing the air to an air duct of the air conditioning system of an aircraft. The apparatus provides a plurality of high pressure nozzles inside an air-mixing chamber. By controlling the opening and closing of the nozzles individually, a stepped area ratio of high pressure air with low pressure air is provided for regulating the temperature of the mixed air to the air conditioning system of the aircraft while the aircraft is taking-off, climbing, cruising at various altitudes and landing.
Claims7
An apparatus for mixing high and low pressure air from a jet engine and introducing the mixed air to an air duct of the air conditioning system of an aircraft, the apparatus comprising:
- a low pressure air supply line adapted for connection at one end to the low pressure bleed air of the jet engine;
- a high pressure air supply line adapted for connection at one end to the high pressure bleed air of the jet engine;
- an air-mixing chamber having an inlet section connected to the other end of the low pressure supply line and an outlet section adapted for connection to the air duct;
- a high pressure air supply bypass line connected to the high pressure air supply line and adapted for connection to the air duct;
- a bypass valve connected to the high pressure air supply bypass line;
- a plurality of high pressure nozzles connected to nozzle valves, the nozzle valves connected to the other end of the high pressure air supply line, the ends of the high pressure nozzles received in the air-mixing chamber for mixing high pressure air with the low pressure air;
- a temperature control connected to the nozzle valves for opening and closing the nozzle valves, the control also connected to the bypass valve for opening and closing the bypass valve;
- and
- a temperature sensor adapted for connection to the air duct for sensing the temperature of the mixed air, the sensor also connected to the temperature control for regulating the temperature control.
The apparatus for mixing high and low pressure air from a jet engine and introducing the mixed air to an air duct of the air conditioning system of an aircraft, the apparatus comprising:
- a low pressure air supply line adapted for connection at one end to the low pressure bleed air of the jet engine;
- a high pressure air supply line adapted for connection at one end to the high pressure bleed air of the jet engine;
- an air-mixing chamber having an inlet section connected to the other end of the low pressure air supply line, the inlet section flared inwardly into a venturi section, the venturi section connected to an outwardly flared outlet section, the outlet section adapted for connection to the air duct;
- a high pressure air supply bypass line connected to the high pressure air supply line and adapted for connection to the air duct;
- a bypass valve connected to the high pressure air supply bypass line;
- a first, a second, and a third high pressure nozzle, the nozzles connected to a first nozzle valve, a second nozzle valve, and a third nozzle valve, respectively, the nozzle valves connected to the high pressure air supply line, the ends of the nozzles positioned in the air-mixing chamber for mixing the high pressure air with the low pressure air;
- a temperature control connected to the nozzle valves for opening and closing the nozzle valves, the control also connected to the bypass valve for opening and closing the bypass valve;
- and
- a temperature sensor adapted for connection to the air duct for sensing the temperature of the mixed air, the sensor also connected to the temperature control for regulating the temperature control.
Dependencies are inferred from the claim text.