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An active flow control system for a wing-body fusion underwater glider

An active flow control, underwater glider technology, applied in motor vehicles, underwater ships, underwater operation equipment, etc., can solve problems such as increased drag coefficient, weakened detection ability or working time, and narrow interior space of the glider.

Active Publication Date: 2021-05-18
NORTHWESTERN POLYTECHNICAL UNIV
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

At present, the lift-to-drag ratio of wing-body fused underwater gliders can reach 15-20 through shape optimization. Further improvement of the lift-to-drag ratio
Moreover, only relying on shape optimization to increase the lift-to-drag ratio of an underwater glider will narrow the internal space of the glider, reducing its detection capability or working time.

Method used

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  • An active flow control system for a wing-body fusion underwater glider
  • An active flow control system for a wing-body fusion underwater glider
  • An active flow control system for a wing-body fusion underwater glider

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Embodiment Construction

[0018] The following will clearly and completely describe the technical solutions in the embodiments of the present invention with reference to the accompanying drawings in the embodiments of the present invention. Obviously, the described embodiments are only some, not all, embodiments of the present invention. Based on the embodiments of the present invention, all other embodiments obtained by persons of ordinary skill in the art without making creative efforts belong to the protection scope of the present invention.

[0019] The purpose of the present invention is to provide an active flow control system for wing-body fusion underwater glider, so as to solve the above-mentioned problems in the prior art and realize the flow control targets of different parts of the underwater glider under different flow control strategies.

[0020] In order to make the above objects, features and advantages of the present invention more comprehensible, the present invention will be further d...

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Abstract

The invention discloses an active flow control system for wing-body fusion underwater glider, which relates to the field of flow control, including an electromagnetic flow control actuator unit installed on the front end of the upper surface of the wing of the underwater glider, and an The position where the electromagnetic flow control actuator unit is installed on the surface is alternately provided with a steady jet port and a synthetic jet port; a steady jet flow control actuator unit is provided below the steady jet port, and a synthetic jet port is provided below the synthetic jet port. The flow control actuator unit; the electromagnetic flow control actuator unit, the steady jet flow control actuator unit and the synthetic jet flow control actuator unit are respectively connected with the signal processing and control system, and the signal processing and control system is connected with sensors, The sensor is fixedly arranged on the wing of the underwater glider. The invention can realize the flow control objectives of different parts on the underwater glider under different flow control strategies.

Description

technical field [0001] The invention relates to the field of active flow control, in particular to an active flow control system for a wing-body fusion underwater glider. Background technique [0002] Underwater Glider (UG) is a new type of underwater vehicle that uses net buoyancy and attitude angle adjustment to obtain propulsion. Compared with traditional underwater vehicles, underwater glider has the advantages of long range, strong continuous working ability and good economy. As an underwater unmanned intelligent mobile platform, underwater glider has broad application prospects and great potential value in the fields of exploring marine resources, marine scientific investigation and military affairs. According to the appearance, underwater gliders can be divided into two types: traditional rotary type and wing-body fusion type. Since the shape of the rotor shell cannot provide very high lift like hydrofoils, the maximum lift-to-drag ratio of traditional rotor gliders...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): B63G8/16B63B1/32
CPCB63B1/32B63G8/16Y02T70/10
Inventor 杜晓旭刘鑫宋保维潘光
Owner NORTHWESTERN POLYTECHNICAL UNIV
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