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Test platform for shipboard helicopter landing auxiliary equipment and operation method thereof

A technology of auxiliary equipment and test platform, which is applied in the direction of aircraft component testing, shutdown devices, etc., can solve the problems of inefficient, time-saving, safe and accurate shipboard helicopter landing auxiliary equipment quality, performance testing, etc., to improve test efficiency , Reduce the difficulty of operation, save manpower and material resources

Active Publication Date: 2021-02-09
YANSHAN UNIV
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

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Problems solved by technology

[0003] The purpose of the present invention is to solve the problem that the existing technology cannot efficiently, time-saving, safely and accurately test the quality and performance of the shipboard helicopter landing auxiliary equipment

Method used

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  • Test platform for shipboard helicopter landing auxiliary equipment and operation method thereof
  • Test platform for shipboard helicopter landing auxiliary equipment and operation method thereof
  • Test platform for shipboard helicopter landing auxiliary equipment and operation method thereof

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Embodiment Construction

[0033] The technical solutions of the present invention will be clearly and completely described below through specific embodiments. Apparently, the described embodiments are only some of the embodiments of the present invention, but not all of them. Based on the embodiments of the present invention, all other embodiments obtained by persons of ordinary skill in the art without creative efforts fall within the protection scope of the present invention.

[0034] Such as Figure 1-7 As shown, the test platform of a shipborne helicopter landing auxiliary equipment includes: landing auxiliary equipment (2), a simulation platform (3), a test platform base (16), a double-cylinder parallel hydraulic cylinder (11), The transmission assembly (10), beam assembly (1), bracket (5), single rod hydraulic cylinder (4), track (24) captures the mechanical claw (17); the track (24) is installed on the test platform base (16 ), the landing auxiliary equipment (2) is installed on the surface of...

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Abstract

The invention relates to the technical field of mechanical equipment performance testing, in particular to a test platform for shipboard helicopter landing auxiliary equipment and an operation methodthereof. A double-cylinder parallel hydraulic cylinder drives a carrier landing auxiliary device to simulate the action of a carrier landing auxiliary device approaching the helicopter, the action ofa helicopter feeler lever is simulated through a single-rod hydraulic cylinder and the double-rod hydraulic cylinder, so that the function of testing the performance of the landing auxiliary equipmentis realized; the whole process is automatically controlled, so that the test process is simpler to operate, and manpower and material resources are saved.

Description

technical field [0001] The invention relates to the technical field of performance testing of mechanical equipment, in particular to a test platform for shipboard helicopter landing auxiliary equipment and an operation method thereof. Background technique [0002] At present, with the research and development of helicopter technology, the application of helicopters in offshore operations is becoming more and more extensive, and various equipment to ensure the safety of helicopter take-off and landing have emerged, one of which is the ship-borne helicopter landing auxiliary equipment. The shipboard helicopter landing auxiliary equipment can be moved to the place where the helicopter lands, and the probe rod protruding from the helicopter can be grasped by the mechanical claw on the shipboard helicopter landing auxiliary equipment, and the helicopter can be fixed on the ship. However, the inspection of the quality and performance of the ship-borne helicopter landing aids still...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B64F5/60B64F1/02
CPCB64F5/60B64F1/02
Inventor 张祝新刘谦赵丁选赵坤杨鹏程田旭孙朋朋
Owner YANSHAN UNIV