The invention relates to the technical field of aerial refueling, in particular to an inflatable aerial refueling variable-resistance taper sleeve which comprises an annular canopy surface, the interior of the annular canopy surface is hollow, the annular canopy surface is connected with an inflator pump, the inflator pump is connected with a flight control system, the annular canopy surface is connected with one end of a rib, and the other end of the rib is connected with an air inlet. And the other end of the umbrella rib is connected with a conical cup. The opening degree of the annular canopy surface is controlled through the inflator pump, and the resistance characteristic of the taper sleeve is changed, so that the oiling machine can carry out aerial oiling at different heights and speeds, and the posture of the taper sleeve is controlled to enable the oiling taper sleeve to be in a relatively stable posture in the aerial oiling process. And by arranging the umbrella ribs, the strength of the taper sleeve is improved, and meanwhile the refueling hose can be guided to facilitate refueling.
本发明涉及空中加油技术领域,具体涉及一种充气式空中加油变阻力锥套,包括环形伞衣面,所述环形伞衣面内部为空心设置,所述环形伞衣面连接有充气泵,所述充气泵连接有飞控系统,所述环形伞衣面连接有伞骨的一端,所属伞骨另一端连接有锥杯。通过充气泵控制环形伞衣面张开的程度,实现改变锥套的阻力特性,从而使得加油机能在不同高度及速度下进行空中加油并且控制锥套的姿态使加油锥套在空中加油过程中处于相对稳定的姿态。通过设置伞骨,在给锥套增加强度的同时还能对加油软管起到引导作用便于加油的进行。
Inflatable air refueling variable-resistance taper sleeve
一种充气式空中加油变阻力锥套
2024-11-22
Patent
Electronic Resource
Chinese
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT |
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