Angle-equipped cooling and positioning structure for flame tube head of aero-engine combustion chamber
A flame tube head and aero-engine technology, applied in the field of aero-engines, can solve the problems affecting the use of the flame tube, unfavorable cooling, unfavorable maintenance, etc., and achieve the effects of simple and feasible structure, increased life, and good cooling effect
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[0021] In order to make the object, technical solution and advantages of the present invention clearer, the present invention will be described in further detail below in conjunction with specific embodiments and with reference to the accompanying drawings.
[0022] The patent of the present invention will be introduced in detail below in conjunction with the accompanying drawings and specific implementation examples.
[0023] refer to figure 1 , is a schematic diagram of the cooling and positioning structure of the flame tube head of the aeroengine combustor, describing the outer casing 1, the diffuser 2, the inner casing 3, the nozzle 4, the electric nozzle 5, the flame tube outer ring 6, and the flame tube inner ring 7 , the relative positions of the cap 8, the swirler assembly 9 and the cooling positioning structure 10 of the flame cylinder head.
[0024] The cooling positioning structure 10 of the flame tube head is located behind the cap 8, and the swirler assembly 9 is...
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