Active control hose air refueling system and airplane with same

An aerial refueling and active control technology, which is applied to aircraft parts, transportation and packaging, can solve the problems of difficult operation and high pressure, and achieve the effect of improving docking efficiency and success rate

Pending Publication Date: 2022-07-22
SHENYANG AIRCRAFT DESIGN INST AVIATION IND CORP OF CHINA
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

In these two aerial refueling methods, the operation difficulty and pressure of the refueling crew or the pilot of the refueling aircraft are very high

Method used

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  • Active control hose air refueling system and airplane with same

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Embodiment Construction

[0023] In order to make the implementation purpose, technical solutions and advantages of the present application clearer, the technical solutions in the embodiments of the present application will be described in more detail below with reference to the accompanying drawings in the embodiments of the present application. Throughout the drawings, the same or similar reference numbers refer to the same or similar elements or elements having the same or similar functions. The described embodiments are some, but not all, of the embodiments of the present application. The embodiments described below with reference to the accompanying drawings are exemplary, and are intended to be used to explain the present application, but should not be construed as a limitation to the present application. Based on the embodiments in this application, all other embodiments obtained by those of ordinary skill in the art without creative work fall within the protection scope of this application. Th...

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PUM

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Abstract

The invention belongs to the technical field of air refueling, and particularly relates to an active control hose air refueling system and an airplane with the same. The active control hose aerial refueling system comprises a refueling hose, a refueling connector, a drag parachute, an electric steering engine and a binocular vision sensor. The refueling joint is mounted at one end of the refueling hose; the drag parachute and the refueling connector are coaxially arranged and fixedly connected. The refueling hose is coaxially sleeved with an electric steering engine, the electric steering engine is close to the drag parachute, and a pneumatic rudder is installed on the electric steering engine; the binocular vision sensor is fixedly installed in the drag parachute, and the binocular vision sensor is used for feeding back a relative position signal between the drag parachute and the oil receiving probe to the electric steering engine. Through the relative position feedback of the binocular vision sensor, the electric steering engine and the pneumatic rudder are used for actively controlling the refueling hose, the butt joint of the oil receiving probe and the refueling connector is assisted, and the butt joint efficiency and success rate are remarkably improved.

Description

technical field [0001] The present application belongs to the technical field of aerial refueling, and particularly relates to an active control hose aerial refueling system and an aircraft having the same. Background technique [0002] Aerial refueling technology is the effectiveness enhancer of modern aircraft, which can effectively increase the mission radius and endurance of the aircraft, so as to achieve continuous and long-range deterrence. [0003] At present, there are two types of aerial refueling technologies in the world, hard aerial refueling and soft aerial refueling. The U.S. military adopts a hard refueling system. During the refueling process, the tanker is active, and the oiler visually controls the hard pipe to connect with the oil receiver. The air refueling system in my country is a soft refueling system. When refueling, the hose floats naturally under the action of gravity and aerodynamic force after being put down, and swings with the air flow. In the...

Claims

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Application Information

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IPC IPC(8): B64D39/02
CPCB64D39/02
Inventor 陈星伊卢元杰赵航逯美超
Owner SHENYANG AIRCRAFT DESIGN INST AVIATION IND CORP OF CHINA
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