Small -size engine pedestal structure

• Main Authors: WANG NING, LI XIONGKUI, ZHANG CHAOYING, ZHANG XIAOHUI, XU SHANSHAN, HUANG CHENG, WEI KAI, GAO YING, TAN ZHI, AN RONGTAO, GUAN HONGREN, MENG DEHAO, WANG JINGCHAO
• Format: Patent
• Language: English
• Published: 27.01.2016
• Subjects: BLASTING; COMBUSTION ENGINES; HEATING; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS; JET-PROPULSION PLANTS; LIGHTING; MECHANICAL ENGINEERING; WEAPONS

The utility model discloses a small -size engine pedestal structure, its whole formula structure as an organic whole, middle be sleeve (6), sleeve (6) upper portion is provided with planar structure's engine flange dish (7), and the lower part is provided with the cabin body ring flange (8) of cambered surface, sets up a plurality of engines on the engine flange dish (7) and connects interface (1), sets up on the cabin body ring flange (8) a plurality of cabin body coupling interface (2), and open on the upper portion of sleeve (6) has pressure measurement line connection (3). The utility model has the advantages of: low -cost, production cycle short, resistant heatflash flows and axial loading, connects reliably, the cabin body that can adapt to different curved surfaces, different shapes uses, whole device light in weight, small, technology are simply, easily install, satisfy high temperature simultaneously and bear and warp minor requirement, its must play the rocket body structure and civilian in the aspect of have an extensive application prospect.