High efficiency heat transfer structure
AssigneeAlstom Gas Turbines Limited
InventorPeter Senior
Life of this patent
Estimating the term…
Abstract
A heat transfer structure for the efficient cooling of a heated surface such as the combustor wall of a gas turbine has a high heat transfer coefficient and can therefore operate at a relatively low pressure loss. A cooling jacket is formed around the heated surface by means of an apertured wall parallel to and spaced from the heated surface. Cooling fluid such as air flows into the cooling jacket through the apertures and impinges as air jets on the heated surface. The heat transfer coefficient is greatly increased by flow diversion features associated with the apertures which act as Coanda surfaces to divert the air jets so that they impinge obliquely and turbulently on the heated surface and establish subsequent turbulent sinuous cross-flows of the cooling air on the heated surface.
Claims9
A heat transfer structure comprising:
- an impingement surface from which heat is to be removed by a coolant impinging thereon;
- outer wall means having an outer surface which acts as a boundary of a plenum chamber containing pressurized coolant and an inner surface confronting and spaced from the impingement surface to define a cavity between the impingement surface and the outer wall means;
- coolant inlet means;
- coolant outlet means;
- the coolant inlet means comprising an array of apertures in the outer wall means for generating a corresponding array objects of coolant fluid for impingement on the impingement surface, thereby establishing a flow of coolant fluid from the plenum chamber into the heat transfer structure and over the impingement surface to the coolant outlet means;
- and
- flow diversion means associated with each of the apertures in the outer wall means to divert the impingement jets and establish an oblique impingement of the coolant fluid upon the impingement surface, wherein each said flow diversion means has an exterior surface which protrudes into the cavity from a location on the inner surface of the outer wall means adjacent an associated aperture, each associated aperture being located outside of the respective flow diversion means to direct the coolant fluid over the exterior surface of the flow diversion means, each said flow diversion means being inclined away from each associated aperture.
A heat transfer structure for a gas turbine engine combustor, the heat transfer structure facilitating efficient heat transfer away from the combustor and comprising:
- a surface to be cooled comprising a wall of the combustor,
- cooling jacket means spaced from said surface to define a cavity between said surface to be cooled and an inner surface of said cooling jacket means,
- plenum chamber means surrounding said cooling jacket means,
- means connecting said plenum chamber means to a supply of pressurized coolant fluid comprising at least one of steam and air,
- rows of impingement cooling holes in said cooling jacket means for directing jets of coolant fluid from said plenum chamber means onto said surface,
- flow deflection means associated with each said impingement cooling hole for deflecting said jets of coolant fluid and establishing a turbulent flow of coolant fluid over said surface, said flow deflection means comprising Coanda surfaces each of which induces a reduction in pressure on one side of an associated impingement hole so as to induce oblique impingement of said jets of coolant fluid onto said surface, said impingement cooling holes and associated flow deflection means in each row being offset with respect to impingement cooling holes and flow deflection means in each adjacent row, whereby heat transfer is augmented by induced sinuous cross-flows of cooling air over said surface, and
- means connecting said cooling jacket to an inlet of said combustor, whereby during operation of said combustor, coolant fluid heated in said heat transfer structure is used in a combustion process, wherein each said flow deflection means has an exterior surface which protrudes into said cavity from a location on said inner surface of said cooling jacket means adjacent an associated impingement cooling hole, each associated impingement cooling hole being located outside of the respective flow deflection means to direct the coolant fluid over the exterior surface of the flow deflection means, each said flow deflection means being inclined away from each associated impingement cooling hole.
Dependencies are inferred from the claim text.