초록 ▼

An aircraft having a user region therein within which pressurized air at selected pressures can be maintained using an environmental control system provided in the aircraft, and a utility region outside a utility boundary wall of the user region within which selected equipment for the aircraft is lo

An aircraft having a user region therein within which pressurized air at selected pressures can be maintained using an environmental control system provided in the aircraft, and a utility region outside a utility boundary wall of the user region within which selected equipment for the aircraft is located. An internal combustion engine, provided as an intermittent combustion engine, is provided in the utility region having an air intake coupled to combustion chambers therein and a rotatable output shaft also coupled to those combustion chambers for generating force with an air transfer duct extends between the user region and the air intake so as to be capable of conveying pressurized air to that air intake.

대표청구항 ▼

1. An aircraft having a user region therein bounded at least in part by boundary walls within which pressurized air at selected pressures can be maintained using an environmental control system provided in the aircraft, and a utility region outside a utility boundary wall of the user region within w

1. An aircraft having a user region therein bounded at least in part by boundary walls within which pressurized air at selected pressures can be maintained using an environmental control system provided in the aircraft, and a utility region outside a utility boundary wall of the user region within which selected equipment for the aircraft is located, the aircraft comprising: an internal combustion engine provided as an intermittent combustion engine in the utility region having an air intake coupled to combustion chambers therein and a rotatable output shaft also coupled to those combustion chambers for generating force;an air transfer duct extending between an opening in the utility boundary wall, so as to be capable of having pressurized air in the user region enter that air transfer duct at one end thereof, and also being connected to the air intake at an opposite end thereof so as to be capable of conveying pressurized air therein to that air intake;a supercharger capable of receiving air from the atmosphere through an emergency supply duct located in the utility region and providing compressed air in a supercharger duct interconnected to the air transfer duct to provide the compressed air to the air intake of the intermittent combustion engine;a radiator and a pair of hoses connected thereto and to coolant passageways in the intermittent combustion engine to allow circulation of a coolant between those passageways and the radiator to thereby cool that engine;a radiator fan that is rotatable to draw air through the radiator;a vent in the utility region through which the radiator fan draws air; anda heat removal duct extending from the radiator fan to an outlet vent in the utility region. 2. The aircraft of claim 1 wherein the user region has a passenger cabin and a cargo space therein. 3. The aircraft of claim 2 wherein the utility boundary wall is a cabin pressure bulkhead between the utility region and the user region. 4. The aircraft of claim 1 further comprising a primary electrical generator having a rotatable input shaft mechanically coupled through a coupler to the intermittent combustion engine output shaft and having an output conductor, the output conductor being electrically energized in response to rotation of the input shaft. 5. The aircraft of claim 1 wherein the supercharger duct is interconnected to the air transfer duct at a connection junction, there being a first check valve located between the utility boundary wall and the connection junction and a second check valve located between the supercharger and the connection junction with the first and second check valves each allowing air to flow in only one direction therethrough with that direction leading toward the intermittent combustion engine. 6. The aircraft of claim 4 wherein the supercharger is formed of a fan and an electric motor connected to the fan so as to be capable of rotating that fan, the electric motor being supplied electrical power by the primary electrical generator. 7. The aircraft of claim 4 further comprising a generator radiator and a pair of hoses connected thereto and to the primary electrical generator to allow circulation of a lubricant used in the primary electrical generator between that generator and the generator radiator to thereby cool that lubricant. 8. The aircraft of claim 7 wherein the radiator fan draws air through the engine radiator and the generator radiator. 9. An aircraft having: a user region pressurized by an environmental control system;a utility region having aircraft equipment;a boundary wall separating the utility region from the user region;an intermittent combustion engine in the utility region having an air intake and an output shaft;an air transfer duct extending between an opening in the utility boundary wall to transfer pressurized air in the user region to the air intake;an exhaust duct extending from the intermittent combustion engine to an opening in the aircraft to convey combustion products to the atmosphere outside the aircraft;an electrical generator coupled to the output shaft;an emergency supply duct located in the utility region to receive air from the atmosphere;a supercharger duct connecting the emergency supply duct to the air transfer duct;a supercharger disposed in the supercharger duct to provide compressed air to the air intake of the intermittent combustion engine;an engine radiator coupled to the intermittent combustion engine to allow circulation of a coolant between the engine radiator and the intermittent combustion engine;a fan rotatable by an electric motor to draw air through the engine radiator;a vent in the utility region through which the radiator fan draws air; anda heat removal duct extending from the radiator fan to an outlet vent in the utility region. 10. The aircraft of claim 9 wherein the supercharger comprises: a fan; andan electric motor connected to the fan and the electrical generator. 11. The aircraft of claim 9 and further comprising: a generator radiator connected to the electrical generator to allow circulation of a coolant between the generator radiator and the electrical generator. 12. The aircraft of claim 11wherein the fan is rotatable by the electric motor to draw air through the generator radiator. 13. A method for generating electrical power in an aircraft, the method comprising: operating an environmental control system to provide pressurized air in a user region of the aircraft;operating an intermittent combustion engine in a utility region of the aircraft using pressurized air from the user region that is passed through an air transfer duct connected to a boundary wall between the utility region and the user region;driving an electrical generator with the intermittent combustion engine;drawing electrical power from the electrical generator by aircraft operating devices in the aircraft;rotating a supercharger fan drawing electrical power from the electrical generator to draw air from the atmosphere into an emergency supply duct connected to a supercharger duct within the utility region;providing compressed air from the supercharger duct to the air transfer duct and the intermittent combustion engine;rotating a radiator fan drawing electrical power from the electrical generator to draw radiator air from an inlet vent in the utility region through a radiator fluidly coupled to the intermittent combustion engine; andforcing the radiator air through a heat removal duct extending from the radiator fan to an outlet vent in the utility region.