一种可折叠减摇油箱装置及其减摇方法

By designing a foldable anti-roll fuel tank device, which uses a gas generator to unfold during a helicopter's water landing and folds up during flight, the problem of buoyancy performance and structural utilization after a helicopter's water landing is solved, achieving both anti-roll effect and space optimization.

CN117699026BActive Publication Date: 2026-07-17CHINA SPECIAL TYPE FLIER RES INST

Patent Information

Authority / Receiving Office
CN · China
Patent Type
Patents(China)
Current Assignee / Owner
CHINA SPECIAL TYPE FLIER RES INST
Filing Date
2023-12-29
Publication Date
2026-07-17

AI Technical Summary

Technical Problem

Existing technologies have failed to effectively improve the buoyancy and structural utilization of helicopters after water landings, and have failed to balance the space occupied by fuel tanks inside the helicopter with the anti-roll effect.

Method used

Design a foldable anti-roll fuel tank device that can be quickly deployed during a helicopter water landing using a gas generator and filling agent. It uses fuel to generate restoring torque to reduce roll motion. During normal flight, the fuel tank can be folded into the cabin without taking up space.

Benefits of technology

It improves the buoyancy of helicopters after water landing, reduces the amplitude of roll motion, and the fuel tank does not occupy cabin space during normal flight. The materials are lightweight and easy to install, saving design time.

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Abstract

本发明属于航行器水上迫降漂浮特性评估技术领域,具体涉及一种可折叠减摇油箱装置及其减摇方法。包括:可折叠减摇油箱电控单元(2)、点火器(3)、气体发生器(4)、充气剂(5)、圆形喷嘴(6)、可折叠减摇油箱(7),可折叠减摇油箱(7)包括固有展开段(9)和折叠段(10),箱内燃油(8)存放于固有展开段(9)内,可折叠减摇油箱电控单元(2)启动后,触发点火器(3)工作达到反应温度后充气剂(5)迅速发生反应,所产生的气体通过圆形喷嘴(6)进入可折叠减摇油箱(7)中,折叠段(10)在充气剂(5)发生反应后迅速展开。
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