초록 ▼

A rotary aerofoil blade is provided with closed cycle sodium cooling. The blade has a shank portion which contains a chamber which is in turn partially occupied by an air cooled core member. The core member serves to condense sodium vapor from the aerofoil portion of the blade. Gutter members within

A rotary aerofoil blade is provided with closed cycle sodium cooling. The blade has a shank portion which contains a chamber which is in turn partially occupied by an air cooled core member. The core member serves to condense sodium vapor from the aerofoil portion of the blade. Gutter members within the chamber capture the condensed sodium as it is cenrifuged towards the aerofoil portion and direct it into a further chamber within the blade shank portion from when it flows into passages adjacent the external surface of the aerofoil portion. The high temperature of the aerofoil portion vaporizes the sodium which is then pumped by vapor pressure gradients back to cooled core member whereupon the cycle is repeated.

대표청구항 ▼

A closed cycle cooling system in a rotary aerofoil blade having an aerofoil portion, a root portion for the attachment of said aerofoil blade to the periphery of a rotary disc, and a shank portion interconnecting said aerofoil portion and said root portion, said closed cycle cooling system comprisin

A closed cycle cooling system in a rotary aerofoil blade having an aerofoil portion, a root portion for the attachment of said aerofoil blade to the periphery of a rotary disc, and a shank portion interconnecting said aerofoil portion and said root portion, said closed cycle cooling system comprising: a heat exchanger enclosed within said shank portion, a plurality of lengthwise extending passages interconnecting said heat exchanger and a chamber defined within the tip of said aerofoil portion, at least one of said passages being located in a central region of said aerofoil portion remote from the external surface thereof, the remainder of said passages being spaced adjacent to and over a substantial portion of the external surface of said aerofoil portion; a material partially filling said cooling system, said material being in the liquid state at the temperature at which said heat exchanger operates and in a vapor state at the temperatures at which said aerofoil portion operates, said heat exchanger comprising a chamber defined within said shank portion, the interior of said heat exchanger chamber and said tip portion being interconnected by said at least one passage located in the central region of said aerofoil portion, said shank heat exchanger chamber being partially occupied by a core member having an outer surface and an interior surface, said core member defining an interior chamber and including inlet means to permit a flow of cooling air to said interior chamber along said interior surface of said core member, and outlet means in said core member for permitting said cooling air to flow out of said core member; and liquid directing means for directing any condensed material within said shank heat exchanger chamber to the remainder of said passages interconnecting said heat exchanger and said tip chamber, and for preventing any such condensed material from being centrifugally urged into said at least one passageway in the central region of said aerofoil portion, said liquid directing means including a plurality of gutter members and a further chamber defined within said shank portion, said gutter members interconnecting said core member and said further chamber and being so disposed as to capture condensed material within said heat exchanger and direct said captured condensed material into said further chamber, said further chamber being interconnected in turn with said remainder of said passages adjacent the outer surface of said aerofoil portions so that any condensed material directed into said further chamber by said gutter members subsequently flows into said remainder of said passages adjacent the outer surface of said aerofoil portion.