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ASSEMBLY APPARATUS FOR BENT PLATE OF SOLID ROCKET MOTOR AND ASSEMBLY METHOD FOR BENT PLATE OF SOLID ROCKET MOTOR
ASSEMBLY APPARATUS FOR BENT PLATE OF SOLID ROCKET MOTOR AND ASSEMBLY METHOD FOR BENT PLATE OF SOLID ROCKET MOTOR
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机译:固体火箭发动机弯板的装配方法及固体火箭发动机弯板的装配方法。
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摘要
The present invention is a bent plate assembly device of a solid propulsion engine that is assembled to a combustion pipe of a solid propulsion engine and places a vent plate in which a plurality of gas outlets for transferring heat and pressure of an igniter into the combustion pipe are placed in an assembly position in the combustion pipe, A bent plate adsorption part adsorbed on, and a bent plate coupling part where the adsorption plate member is located therein and is coupled with a bent plate through a gas outlet of the bent plate to facilitate the assembly of the bent plate when assembling the front igniter of a solid propulsion engine To improve the productivity of the propulsion engine by reducing the working time, and to stably position the vent plate in the deep combustion pipe, preventing accidents of falling of the vent plate in the combustion pipe during assembly and stably vent plate By assembling, it is possible to uniformly manage the assembly quality of the propulsion engine.
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