FIELD: space vehicle jet engine.
SUBSTANCE: web(2) subjected to the action of thermal loads has at least the first layer (5) and the second layer (6), which is positioned closer than the first layer to the heat source and through which the heat is transferred to the first layer. The offered web is featured by the fact that the first and second layers (5, 6) cam perceive the considerable part of the load acting on the web, the second layer (6) features a greater heat conduction and/or lower thermal expansion as compared with the first layer (5).
EFFECT: reduced thermal deformations arising in the web (2) under the action of heat load.
2 cl, 3 dwg
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