A power supply system includes a regulated power source that has an a synchronous machine, a flywheel with the shaft connected thereto, an electrical generator electrically connected through a switch to the synchronous machine of the regulated power source, an engine having a main shaft coupled to the shaft of the electrical generator, a power supply, and a switch connected between the electrical generator, the power supply and the regulated power source. The switch transfers power from the regulated power source to the electrical generator so as to cause the electrical generator to rotate the shaft in order to rotate the shaft of the engine during engine start-up.

A power supply system includes a regulated power source that has an a synchronous machine, a flywheel with the shaft connected thereto, an electrical generator electrically connected through a switch to the synchronous machine of the regulated power source, an engine having a main shaft coupled to the shaft of the electrical generator, a power supply, and a switch connected between the electrical generator, the power supply and the regulated power source. The switch transfers power from the regulated power source to the electrical generator so as to cause the electrical generator to rotate the shaft in order to rotate the shaft of the engine during engine start-up.

The present invention relates to a heat exchanger for cooling an electrical element and a heat exchanger assembly for cooling an electrical element, and more particularly, to a heat exchanger for cooling an electrical element and a heat exchanger assembly for cooling an electrical element into which the electrical element may be easily inserted and in which both surfaces of the electrical element and a tube through which a coolant flows are formed to contact each other to improve cooling performance.

The electrical machine according to the invention is a dual machine, and comprises a first machine which can be reversed and a second machine functioning through induction between two windings. The second machine can be used for de-icing a propeller, the induction-receiving winding being mounted on the propeller shaft. The first electrical machine can function as an electrical engine to taxi the aircraft. In certain embodiments, the winding mounted on the stator is common to the two machines and different magnetic flows are utilised to control them. A separate functioning of the two machines and a very good integration into the aircraft engine, with space-saving and low mass, are possible.

The electrical machine according to the invention is a dual machine, and comprises a first machine which can be reversed and a second machine functioning through induction between two windings. The second machine can be used for de-icing a propeller, the induction-receiving winding being mounted on the propeller shaft. The first electrical machine can function as an electrical engine to taxi the aircraft. In certain embodiments, the winding mounted on the stator is common to the two machines and different magnetic flows are utilised to control them. A separate functioning of the two machines and a very good integration into the aircraft engine, with space-saving and low mass, are possible.

A lamination for use in an integrated drive generator is formed from a plurality of plates having a body including a pair of opposed cylindrical surfaces. Non-cylindrical ditches are defined circumferentially intermediate the pair of cylindrical surfaces. A plurality of passages are formed in an outer periphery of the cylindrical surfaces including relatively large holes extending through a slot to the outer periphery. Grooves are formed intermediate the relatively large holes.

A hybrid propulsion system includes a heat engine configured to drive a heat engine shaft. An electric motor is configured to drive an electric motor shaft. A transmission system includes at least one gearbox. The transmission system is configured to receive rotational input power from each of the heat engine shaft and the electric motor shaft and to convert the rotation input power to output power.

A hybrid propulsion system includes a heat engine configured to drive a heat engine shaft. An electric motor is configured to drive an electric motor shaft. A transmission system includes at least one gearbox. The transmission system is configured to receive rotational input power from each of the heat engine shaft and the electric motor shaft and to convert the rotation input power to output power.

A vehicle includes a first rotating electric machine, a second rotating electric machine, a power transmission device and an accommodation case. The rotating electric machine accommodation portion and the power transmission device accommodation portion are partitioned by a partition wall. The partition wall includes a first rotating electric machine accommodation wall, a second rotating electric machine accommodation wall, and a step wall which extends in the axial direction from the second rotating electric machine accommodation wall to the first rotating electric machine accommodation wall. The step wall is at least partially overlapped with the second rotating electric machine in the axial direction, and a distance between an outermost diameter portion of the second rotating electric machine and the step wall is shorter than a distance between the outermost diameter portion of the second rotating electric machine and an outermost diameter portion of the first rotating electric machine.

A vehicle includes a first rotating electric machine, a second rotating electric machine, a power transmission device and an accommodation case. The rotating electric machine accommodation portion and the power transmission device accommodation portion are partitioned by a partition wall. The partition wall includes a first rotating electric machine accommodation wall, a second rotating electric machine accommodation wall, and a step wall which extends in the axial direction from the second rotating electric machine accommodation wall to the first rotating electric machine accommodation wall. The step wall is at least partially overlapped with the second rotating electric machine in the axial direction, and a distance between an outermost diameter portion of the second rotating electric machine and the step wall is shorter than a distance between the outermost diameter portion of the second rotating electric machine and an outermost diameter portion of the first rotating electric machine.