The invention discloses a flying backpack for a low-altitude single aircraft, and relates to the field of manned aircrafts. The problems that an existing jet-propelled aircraft garment is large in self weight, inconvenient in pose adjustment and prone to hurting pilots are solved. An oil supply system is installed in a shell, an electrical system is installed on the upper end face of the shell, and a backpack micro turbine engine is installed on the lower portion of the shell. The shell comprises a back plate and a flying back covering part, the back plate is a plate body, a plurality of lightening holes are formed in the upper portion of the back plate, the back plate is made of aluminum alloy, penetrating holes are formed in the periphery of the back plate, and the middle of the safety belt is fixedly installed in the middle of the back plate through bolts and olecranon hooks. A strap of the safety belt penetrates through the penetrating-connecting hole and then is connected with the body of the pilot, the flying back covering part is a shell cover and covers the back plate, and a filiform net is arranged on the lower portion of the flying back covering part. The invention is used in aircrafts.
一种低空单人飞行器使用的飞行背包,它涉及载人飞行器领域。本发明解决了现有的喷气式飞机服存在自身重量铰大、位姿调整不便和易对飞行员造成伤害的问题。本发明的供油系统安装在壳体内部,电气系统安装在壳体的上端面上,背包微型涡轮发动机安装在壳体的下部;壳体包括背板和飞行背覆盖件,背板为板体,其中,背板的上部开设有多个减重孔,且背板采用铝合金制成,背板的四周开设有穿接孔,安全带的中部通过螺栓和鹰嘴钩固定安装在背板的中部,安全带的背带穿过穿接孔之后与飞行员的身体连接,飞行背覆盖件为壳体罩,飞行背覆盖件盖装在背板上,飞行背覆盖件的下部设有丝状网。本发明用于飞行器中。
Flight backpack for low-altitude single aircraft
一种低空单人飞行器使用的飞行背包
25.04.2025
Patent
Elektronische Ressource
Chinesisch
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