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Segmented adjustable oscillation wing plate

An adjustable and segmented technology, applied in the direction of rotary thrusters, etc., can solve the problem of low utilization rate of wave energy

Pending Publication Date: 2020-10-23
THE CHINESE UNIV OF HONG KONG SHENZHEN +1
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0005] In view of the deficiencies in the prior art above, the purpose of this application is to provide a segmented adjustable oscillating wing, which aims to solve the technical problem of low wave energy utilization of the existing oscillating wing

Method used

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  • Segmented adjustable oscillation wing plate
  • Segmented adjustable oscillation wing plate
  • Segmented adjustable oscillation wing plate

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Embodiment Construction

[0023] In order to facilitate the understanding of the present application, the present application will be described more fully below with reference to the relevant drawings. Preferred embodiments of the application are shown in the accompanying drawings. However, the present application can be embodied in many different forms and is not limited to the embodiments described herein. On the contrary, the purpose of providing these embodiments is to make the disclosure of the application more thorough and comprehensive.

[0024] Unless otherwise defined, all technical and scientific terms used herein have the same meaning as commonly understood by one of ordinary skill in the technical field to which this application belongs. The terminology used herein in the description of the application is only for the purpose of describing specific embodiments, and is not intended to limit the application.

[0025] like Figure 1-3 As shown, this embodiment provides a segmented adjustabl...

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Abstract

The invention relates to a segmented adjustable oscillation wing plate. Segmented type wing plates, a connecting plate and a limiting stop rod are included, the wing plates are arranged at the two sides of a propeller support and are symmetrically distributed. A bearing mounting hole, a wing plate limiting hole and a limiting groove are formed in the propeller support; a bearing is mounted in thebearing mounting hole; the connecting plate is provided with a wing plate clamping opening used for fixing the segmented type wing plate as well as a fixing transverse shaft and a limiting transverseshaft, the fixing transverse shaft and the limiting transverse shaft are located in the opposite sides of the wing plate clamping opening. The fixed cross shaft penetrates through a bearing and is fixed on the other connecting plate in the opposite side; the limiting transverse shaft penetrates through the wing plate limiting holes and is fixed to the other connecting plate in the opposite side, the segmented type wing plates are fixed to the connecting plates through the wing plate clamping openings, the limiting stop rod is arranged in the limiting grooves, and the rotating angles of the segmented type wing plates can be controlled through the limiting stop rod. The segmented adjustable oscillation wing plate prepared by the invention can effectively improve the utilization rate of waveenergy.

Description

technical field [0001] The invention relates to the field of wave-energy-driven unmanned ships, in particular to a section-adjustable oscillation wing. Background technique [0002] Wave-driven Unmanned Surface Vehicle (WUSV) is a sustainable unmanned marine environment observation platform that uses renewable wave energy to convert it into propulsion. Water quality monitoring, marine resource exploration and other fields. [0003] In order to convert wave energy into propulsion, wave energy-driven unmanned ships usually need to be equipped with shock flaps, which will continuously swing to the upper limit angle and lower limit when the unmanned ship body floats up and down in the waves. At this time, the wing plate at a certain angle of inclination interacts with the water flow in the vertical direction to generate propulsion in the forward direction of the unmanned ship. However, in the actual application process of the oscillating wing, the propulsion performance provid...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B63H1/06
CPCB63H1/06
Inventor 高岩林天麟谢律成
Owner THE CHINESE UNIV OF HONG KONG SHENZHEN
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