A solid rocket motor nozzle assembly connection sealing structure
A technology for engine nozzles and solid rockets, which is applied to rocket engine devices, machines/engines, mechanical equipment, etc. It can solve problems such as temperature shock resistance, high impact, and limited structural space, and achieve high connection strength and connection reliability. High, simple processing effect
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[0016] figure 1 Among them, the present invention includes a nozzle housing 1, a sealant 2 for sealing the connection gap, a retaining ring 3 for connection and fixing, and a nozzle expansion section 4 for limiting the throat liner and converting energy. The stop ring 3 is placed in the concave annular installation groove and the limit groove corresponding to the nozzle expansion section 4, the sealant 2 is basically evenly applied on the corresponding surface of the nozzle expansion section 4, and then the stop ring 3 and The corresponding thread of the nozzle housing 1 enables the nozzle expansion section 4 to be firmly connected to the rear section of the nozzle housing 1, and enables the sealant 2 applied on the nozzle expansion section 4 to be evenly distributed on the corresponding curved surface , to fill up the corresponding curved surfaces of the nozzle housing 1 and the nozzle expansion section 4 that need to be sealed. During the installation and docking process of...
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