The invention relates to the technical field of air refueling, in particular to an inflatable air refueling active stability augmentation taper sleeve which comprises an annular canopy surface, the annular canopy surface comprises an elastic canopy and a non-elastic canopy, the elastic canopy and the non-elastic canopy are both inflatable, the annular canopy surface is connected with an inflator pump, and the inflator pump is connected with an air pump. The inflation pump is connected with a flight control system, the volume of the inflated elastic canopy is larger than that of the non-elastic canopy, the annular canopy surface is connected with one end of a rib, and the other end of the rib is connected with a conical cup. By arranging the elastic canopy, the shape can be changed under the action of the inflator pump, so that the resistance of the taper sleeve is changed, the stability of the taper sleeve is improved, and the phenomenon of swinging of the taper sleeve is avoided. By arranging the non-elastic canopy, the taper sleeve can be kept in a certain shape, and control over the non-elastic canopy is facilitated. 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主动增稳锥套,包括环形伞衣面,所述环形伞衣面包括弹性伞衣和非弹性伞衣,所述弹性伞衣和非弹性伞衣均为充气式,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,所述弹性伞衣充气后体积大于所述非弹性伞衣,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。通过设置弹性伞衣,在充气泵的作用下能够改变形状,从而改变锥套的阻力增加锥套稳定性,解决锥套存在的飘摆现象。通过设置非弹性伞衣,使锥套能够保持一定形状,便于对非弹性伞衣的控制。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 active stability augmentation taper sleeve
一种充气式空中加油主动增稳锥套
2024-11-22
Patent
Electronic Resource
Chinese
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT |
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