Heat shielding device for fuel gas guide piece, particularly gas turbine structure piece
A guiding structure and heat shielding technology, which is applied in the cooling of gas turbine devices, jet propulsion devices, turbine/propulsion devices, etc., can solve the problem of high construction cost
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[0034]Fig. 1 has shown a heat shielding device 5 of the present invention, wherein on a support structure 10, be provided with the heat shield 20 of a plurality of adjacent planar coverings; Fig. 2 has shown the structure of a heat shield and its support structure A cross-section, wherein the cross-section is approximately the mid-section of the thermal shield. For example for lining a hot flue gas chamber, such as a combustion chamber 15, rows of heat shields (as shown in FIG. 2 ) are usually arranged adjacent to each other on the support structure 10 .
[0035] The heat shield 5 can be used, for example, as an inner lining of a combustion chamber 15 of a gas turbine in order to prevent damage to the support structure during operation of the gas turbine.
[0036] To reduce the thermal load, the side of the heat shield 20 facing away from the combustion chamber 15 is cooled by means of cold air.
[0037] At least two adjacent heat shields 20a, 20b form a cooling air channel 3...
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