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Jet engine comprising an afterburner cooled by a ventilation flow with variable flow
Jet engine comprising an afterburner cooled by a ventilation flow with variable flow
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机译:喷气发动机,包括加力燃烧器,该加力燃烧器通过可变流量的通风流冷却
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摘要
The after body (15) has a diaphragm forming assembly (40) with two annular plates (46, 50) in contact with one another. A section of a passage corresponds to mutual covering zones between slots (48) of the plate (46) and slots (52) of the plate (50). The assembly is designed such that dilatation of thermal protection liner (26) under the effect of thermal constraints causes a radial displacement towards exterior of the plate (50) with respect to the plate (46) leading to increase of width of passage section (74) defined by the slots.
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