Patent Application
20050022530
This invention relates to land based gas turbines used for power generation and, specifically, to a device that protects liquid fuel from convective, conductive and radiation heat transfer loads.
It has been found that heat loading into the fuel components of the gas turbine engine are sufficient to form coke within the components, resulting in loss of turbine performance. The inventors are aware of no prior attempts to solve this problem.
This invention relates to a device that is designed to provide an increase in thermal resistance between the gas turbine liquid fuel system components and one of the primary heat sources, thus providing a reduction in heat transfer into the fuel component that leads to increased operational performance of those components.
In the exemplary embodiment, the thermal isolation device includes an assembly of three thin, flat cylindrical columns and three plates. The columns provide structural support for the isolation device and the liquid fuel system components that are attached to the isolation device. The flat plates, arranged substantially perpendicularly to the columns and spaced from each other along the axes of the columns, provide desired surface area for convective cooling. The three plates are spaced equidistantly from one another, and the number of plates may vary. The device is adapted for integration with a gas turbine combustor assembly, for example, between the combustor end cover and the liquid fuel distributor valve.
The height of the isolation device is sized to provide adequate increase in conductive path length for increased thermal resistance. The plates are sized to be as large as possible so as to provide maximum surface area for cooling as well as to provide the maximum shielding of radiation heat loading from the end cover to the liquid fuel distributor valve, while being limited by geometric restrictions due to adjacent componentry on the current combustion end cover assembly and the limitations of additional structural concerns due to vibration.
Accordingly, in one aspect, the present invention relates to a thermal isolation device for a gas turbine combustor assembly comprising a plurality of substantially flat plates secured in spaced relationship by a plurality of columns, at least one column incorporating a bolt hole for use in securing the device between a pair of combustor components.
In another aspect, the invention relates to a thermal isolation device for a gas turbine combustor assembly comprising at least three substantially flat and substantially triangular-shaped plates secured in spaced, substantially parallel relationship to at least three columns.
The invention will now be described in connection with the drawings identified below.
With reference initially to
The three cooling plates 24, 26 and 28 are approximately 0.100 inches in thickness, and their plan view geometry is approximately triangular, with truncated corners at 30, 32. The cooling plates 24, 26 and 28 generate a maximum footprint or coverage on the end cover, limited only by structural vibration concerns.
The plates 24, 26 and 28 are secured, by brazing for example, to respective radial flanges 34, 36 and 38, best seen in
The length or height of the columns 12, 14 and 16 is determined so as to provide increased conduction length and hence less heat transfer into the liquid fuel distributor valve 40 from the combustion end cover 42. In the exemplary embodiment, the thermal isolation device 10, including the columns and plates, is made of stainless steel.
The columns 12, 14 and 16 are arranged so as to accommodate the mounting flange and bolt pattern of the liquid fuel component parts. In the exemplary embodiment, the component parts include a liquid fuel distributor valve 40 best seen in
It will be appreciated that the triangular shape of the plates is dictated to a large extent by the shape of the mounting flange or other surface of the fuel component to which it is to be attached and its associated bolt pattern. Both the shape and number of plates may vary, depending on specific applications. For example, for a square mounting flange on a distributor valve with a four bolt pattern, the device 10 could be modified to include square plates and four columns arranged to match the four bolt pattern.
The main advantage of a thermal isolation device 10 is an increase in thermal resistance resulting in a sufficient reduction and operational temperatures of the liquid fuel distributor valve so as to lower the liquid fuel temperature and thus result in higher operational efficiency. The isolation device 10 is designed to be an addition to a current system, but requires only minimal changes to the existing components such as fuel tubes, etc.
While the invention has been described in connection with what is presently considered to be the most practical and preferred embodiment, it is to be understood that the invention is not to be limited to the disclosed embodiment, but on the contrary, is intended to cover various modifications and equivalent arrangements included within the spirit and scope of the appended claims.
