Plane air refueling auxiliary device

Abstract

The invention discloses a plane air refueling auxiliary device. A double-layer oil feeding hose is composed of an outer-layer protective sleeve and an inner-layer oil conveying pipe; an oil feeder conical sleeve is composed of a conical handle and an umbrella cover which are fixedly connected; the conical handle inside the umbrella sleeve is provided with a camera device and an infrared range sensor; the middle of the conical handle is provided with an axial oil feeding hole; the outer-layer protective sleeve is connected with an external ring of the conical handle; the inner-layer oil conveying pipe is connected with the oil feeding hole in the middle of the conical handle; a flat cable and an exhaust hose are arranged between the outer-layer protective sleeve and the inner-layer oil conveying pipe. The position of the oil feeder conical sleeve is controlled by oil feeder operating personnel; by virtue of controlling the gas-flow rate in unit time, the stress of the oil feeder conical sleeve is changed, position offset of the oil feeder conical sleeve is easily realized, and the operation of regulating the position of the oil feeder conical sleeve by the oil feeder operating personnel is more convenient and safer than that of regulating the position of an airplane by the oil feeder operating personnel; by virtue of active homing control, the plane air refueling butt joint time is reduced and the flight requirement difficulty for plane air refueling is reduced.

Description

technical field [0001] The invention belongs to the technical field of aircraft aerial refueling, and in particular relates to an aircraft aerial refueling auxiliary device. Background technique [0002] In the prior art, when the aircraft is refueling in the air, the oil delivery machine releases the hose out of the machine, and the pilot of the oil receiver machine adjusts the position of the oil receiver machine after receiving the signal, so as to put the oil receiver pipe into the drogue sleeve of the oil receiver machine Internally, since the speed difference and height difference between the receiving aircraft and the tanker are strictly regulated, the pilot's control action of the receiving aircraft must be very stable and accurate. This has extremely high requirements for the pilot of the receiver aircraft, and it is also very difficult to operate. Contents of the invention [0003] In order to overcome the deficiencies of the prior art, the present invention pro...

AI Technical Summary

Problems solved by technology

[0002] In the prior art, when the aircraft is refueling in the air, the oil delivery machine releases the hose out of the machine, and the pilot of the oil receiver machine adjusts the position of the oil receiver machine after receiving the signal, so as to put the oil receiver pipe into the drogue sleeve of the oil receiver machine Internally, since the speed difference and altitude difference between the receiving aircraft and the tanking aircraft are strictly regulated, the pilot's control action of the receiving aircraft must be very stable and accurate

This has extremely high requirements for the pilot of the oil receiving aircraft, and it is also very difficult to operate

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