A supercharger includes a magnetic flux switching motor and a wheel. The motor includes a rotor; a stator stores the rotor therein and includes stator projecting portions projecting inward in a radial direction from an internal circumferential portion toward the rotor; a field source provided in a field slot formed between the stator projecting portions to generate a magnetic field of a constant direction; an armature coil provided in an armature slot; and a controller applying a single-phase current to the armature coil and changing a direction of the applied single-phase current to change a direction of a magnetic field generated from the armature coil and rotate the rotor. The wheel is attached to the rotor, and rotates together with rotation of the rotor to compress the air.

An auxiliary power unit for an aircraft, having a compressor, an intercooler including first conduit(s) having an inlet in fluid communication with the compressor outlet and second conduit(s) configured for circulation of a coolant therethrough, an engine core having an inlet in fluid communication with an outlet of the first conduit(s), and a bleed conduit in fluid communication with the outlet of the first conduit(s) through a bleed air valve. The auxiliary power unit may include a generator in driving engagement with the shaft of the engine core to provide electrical power for the aircraft. A method of providing compressed air and electrical power to an aircraft is also discussed.

An auxiliary power unit for an aircraft, having a compressor, an intercooler including first conduit(s) having an inlet in fluid communication with the compressor outlet and second conduit(s) configured for circulation of a coolant therethrough, an engine core having an inlet in fluid communication with an outlet of the first conduit(s), and a bleed conduit in fluid communication with the outlet of the first conduit(s) through a bleed air valve. The auxiliary power unit may include a generator in driving engagement with the shaft of the engine core to provide electrical power for the aircraft. A method of providing compressed air and electrical power to an aircraft is also discussed.

A radial compressor has an iris diaphragm mechanism for a pressure-charging device of an internal combustion engine. The radial compressor has a bearing assembly, in which a rotor shaft is rotatably mounted, having a compressor impeller arranged in a compressor housing for conjoint rotation on the rotor shaft and having a fresh air supply channel for carrying a fresh air mass flow to the compressor impeller. The iris diaphragm mechanism is upstream of the compressor impeller, allowing variable adjustment of a flow cross section for the fresh air mass flow for admission to the compressor impeller, at least over a partial region. For this purpose, the iris diaphragm mechanism has multiple lamellae which each have a plate style lamella main body and a pin style actuating element as integral constituent parts of the respective lamella.

A radial compressor has an iris diaphragm mechanism for a pressure-charging device of an internal combustion engine. The radial compressor has a bearing assembly, in which a rotor shaft is rotatably mounted, having a compressor impeller arranged in a compressor housing for conjoint rotation on the rotor shaft and having a fresh air supply channel for carrying a fresh air mass flow to the compressor impeller. The iris diaphragm mechanism is upstream of the compressor impeller, allowing variable adjustment of a flow cross section for the fresh air mass flow for admission to the compressor impeller, at least over a partial region. For this purpose, the iris diaphragm mechanism has multiple lamellae which each have a plate style lamella main body and a pin style actuating element as integral constituent parts of the respective lamella.

A compressor for an internal combustion engine supercharging device is disclosed, having a compressor housing in which a compressor wheel is arranged on a rotor shaft; and an air-feed channel for conducting an air flow to the compressor wheel. The compressor has a throttle module, having an iris diaphragm mechanism arranged upstream of the compressor wheel, multiple lamellae and which closes or opens a diaphragm aperture by the lamellae, allowing variable adjustment of a cross-section for the air flow to the compressor wheel. A throttle module housing at least partially delimits the air-feed channel and in and/or on which the iris diaphragm mechanism is mounted. An actuator is mounted on the throttle module housing and mechanically coupled to the iris diaphragm mechanism for actuation thereof. The throttle module is formed as a structural unit separate from the compressor housing and flange-mounted on the compressor housing by the throttle module housing.

A compressor for a charging device of an internal combustion engine has a compressor impeller arranged for conjoint rotation on a rotor shaft. An air supply channel conducts an air mass flow to the compressor impeller. An iris diaphragm mechanism is upstream of the compressor impeller and has multiple lamellae to close or to open a diaphragm aperture to vary a flow cross section for the air mass flow for flow against the compressor impeller. A housing at least partially delimits the air supply channel. The iris diaphragm mechanism is located in the housing. An actuator is mechanically coupled to the iris diaphragm mechanism via an opening in the housing for the purpose of actuating the iris diaphragm mechanism, wherein the actuator is arranged on the housing such that the opening is closed off by the actuator.

A radial compressor comprising an iris diaphragm mechanism for a charging device of an internal combustion engine. The charging device comprises a radial compressor and a lamella for the iris diaphragm mechanism. The radial compressor has an impeller which is rotationally fixed to a rotatably mounted rotor shaft; and a fresh air supply channel for conducting a fresh air mass flow to the impeller. An iris diaphragm mechanism is arranged upstream of the impeller such that a flow cross-section for the fresh air mass flow for admission to the impeller can be variably adjusted at least over a sub-region. The iris diaphragm mechanism comprises several lamellae, wherein each lamella has a lamella base body with an inner edge portion for delimiting the diaphragm aperture, and the inner edge portion of each lamella has an inner edge, which is blunt-edged, on a side facing away from the impeller.

Methods and systems are provided for a boosted internal combustion engine. In one example, a system may include an intake system for supplying charge air, a compressor arranged in the intake system, a first shut-off element arranged in the intake system upstream of an impeller of the compressor, a bypass line that branches off from the intake system upstream of the first shut-off element and that rejoins the intake system upstream of the impeller, a second shut-off element arranged in the bypass line, a compressed air line that opens into the bypass line downstream of the second shut-off element, and a third shut-off element arranged in the compressed air line. A map width of the compressor may be increased by providing airflow to the impeller via the bypass line during low mass flow conditions, and impeller acceleration may be expedited by providing compressed air via the compressed air line.

Methods and systems are provided for a boosted internal combustion engine. In one example, a system may include an intake system for supplying charge air, a compressor arranged in the intake system, a first shut-off element arranged in the intake system upstream of an impeller of the compressor, a bypass line that branches off from the intake system upstream of the first shut-off element and that rejoins the intake system upstream of the impeller, a second shut-off element arranged in the bypass line, a compressed air line that opens into the bypass line downstream of the second shut-off element, and a third shut-off element arranged in the compressed air line. A map width of the compressor may be increased by providing airflow to the impeller via the bypass line during low mass flow conditions, and impeller acceleration may be expedited by providing compressed air via the compressed air line.