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Lateral-drift-resistant damping system of all-hovering hovercraft

A technology of damping system and hovercraft, which is applied in the direction of air cushion, transportation and packaging, vehicle parts, etc. It can solve the problems of affecting the specific position of landing, losing amphibious performance, affecting the accuracy of the route, and achieving the effect of improving the stability of the course

Inactive Publication Date: 2014-08-06
SHANGHAI JIAO TONG UNIV
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  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

The skirt of the full-cushion hovercraft cannot provide sufficient lateral resistance during navigation, so the lateral drift is obvious when encountering crosswinds, which affects the accuracy of the route to a large extent and can even affect the specific location of landing
For sidewall hovercraft, although the rigid sidewalls on both sides can solve the problem of side drifting during navigation to a certain extent, it also makes it lose its amphibious performance

Method used

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  • Lateral-drift-resistant damping system of all-hovering hovercraft
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  • Lateral-drift-resistant damping system of all-hovering hovercraft

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Embodiment Construction

[0025] The implementation of the present invention will be illustrated by specific specific examples below, and those skilled in the art can easily understand other advantages and effects of the present invention from the contents disclosed in this specification.

[0026] see Figure 1 to Figure 4 . It should be noted that the structures, proportions, sizes, etc. shown in the drawings attached to this specification are only used to match the content disclosed in the specification, for those who are familiar with this technology to understand and read, and are not used to limit the implementation of the present invention. Limiting conditions, so there is no technical substantive meaning, any modification of structure, change of proportional relationship or adjustment of size, without affecting the effect and purpose of the present invention, should still fall within the scope of the present invention. The disclosed technical content must be within the scope covered. At the sa...

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Abstract

The invention provides a lateral-drift-resistant damping system of an all-hovering hovercraft. The system comprises damping plates mounted at the bottom of the hovercraft and a control system controlling the damping plates to rise to be folded or drop to be used, and the damping plates are arranged along the navigation direction of the hovercraft. By the lateral-drift-resistant damping system of the all-hovering hovercraft, when the hovercraft navigates, the damping plates can be put down, and direction stability of the hovercraft can be improved greatly; when the hovercraft needs to land, a driver can put the damping plates in a hull, and the hovercraft can land just like an ordinary all-hovering hovercraft and even navigates on land.

Description

technical field [0001] The invention relates to an anti-side drift damping system for a full-cushion lift hovercraft, relates to the relevant characteristics of the hovercraft, and belongs to the technical field of marine engineering. Background technique [0002] Hovercraft is a ship that uses high-pressure air to form an air cushion between the bottom of the ship and the water surface (or ground), so that all or part of the hull can be raised to achieve high-speed navigation. [0003] The full cushion lift hovercraft is a high-performance ship that uses cushion lift fans to inject compressed air into the bottom of the ship, forming an "air cushion" with the support surface, so that the hull completely leaves the support surface. The full lift hovercraft is propelled by an air propeller, and the bottom of the boat leaves the water surface when sailing, so it has unique amphibious properties and good speed. In the military, the hovercraft is the most ideal transportation eq...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B60V3/06
Inventor 易宏张裕芳李英辉陈炉云刘旌扬张天健
Owner SHANGHAI JIAO TONG UNIV
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