초록 ▼

A rotary combustion engine (12) with a self-cooling system comprises a heat exchanging interface for discharging excess heat from the rotary combustion engine (12), and a direct drive fan (44) integrated on the rotary engine output shaft (26) for providing a flow of forced air over the heat exchangi

A rotary combustion engine (12) with a self-cooling system comprises a heat exchanging interface for discharging excess heat from the rotary combustion engine (12), and a direct drive fan (44) integrated on the rotary engine output shaft (26) for providing a flow of forced air over the heat exchanging interface.

대표청구항 ▼

The invention claimed is: 1. A compound cycle engine compnsing a compressor and a turbine section, at least one rotary combustion engine mechanically linked to said turbine section in order to provide a common output, and a cooling system for removing excess heat from said rotary combustion engine,

The invention claimed is: 1. A compound cycle engine compnsing a compressor and a turbine section, at least one rotary combustion engine mechanically linked to said turbine section in order to provide a common output, and a cooling system for removing excess heat from said rotary combustion engine, said cooling system including a fan integrated to and directly driven by an output shaft of said at least one rotary combustion engine, and a toroidal cooler extending about an axis of said output shaft of the rotary combustion engine, wherein said toroidal cooler is located radially outwardly about the rotary combustion engine, wherein said at least one rotary combustion engine is laterally mounted with respect to said compressor and turbine sections, and wherein said output shaft of said at least one rotary combustion engine is angularly disposed relative to an axis of said compressor and turbine sections. 2. A compound cycle engine as defined in claim 1, wherein said fan draws air radially inwardly through said toroidal cooler. 3. A compound cycle engine as defined in claim 1, wherein said toroidal cooler is concentrically mounted to the rotary combustion engine. 4. A compound cycle engine as defined in claim 1, wherein a coolant is circulated by a pump through cooling passages defined in the engine casing in order to pick up excess heat and then fed to the heat exchanger before being recirculated back into the rotary combustion engine. 5. A compound cycle engine as defined in claim 1, wherein the fan draws air axially over parts of the rotary combustion device. 6. A compound cycle engine as defined in claim 1 wherein a pump is provided to circulate oil through the rotary combustion engine to extract excess heat therefrom. 7. A compound cycle engine as defined in claim 1, wherein said at least one rotary combustion engine is mounted at right angles to said compressor and turbine section. 8. A compound cycle engine as defined in claim 1, wherein said cooling system has an air inlet which is located outboard of an air inlet of the compressor section. 9. A compound cycle engine as defined in claim 8, wherein the air inlet of the at least one rotary combustion engine is laterally disposed relative to the air inlet of the compressor section. 10. A compound cycle engine as defined in claim 1, wherein the output shaft of said at least one rotary combustion engine is connected to said turbine section via a bevel gear. 11. A compound cycle engine comprising a compressor and a turbine section, at least one rotary combustion engine mechanically linked to said turbine section in order to provide a common output, and a cooling system for removing excess heat from said rotary combustion engine, said cooling system including a fan integrated to and directly driven by an output shaft of said at least one rotary combustion engine, and a toroidal cooler extending about an axis of said output shaft of the rotary combustion engine, wherein said toroidal cooler is located radially outwardly about the rotary combustion engine, wherein said cooling system has an air inlet which is located outboard of an air inlet of the compressor section, and wherein the air inlet of the at least one rotary combustion engine is laterally disposed relative to the air inlet of the compressor section.