Damage energy absorption structure of helicopter tail protection ducted tail rotor

The invention relates to an energy absorption structure. The energy absorption structure is particularly used for a tail skid and a tail section of a helicopter deform together to absorb tail skid landing collision energy. The energy absorption structure is used for collision energy absorption of a...

Ausführliche Beschreibung

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Bibliographische Detailangaben
Hauptverfasser: WANG XIAOHONG, LI SHENGWEI, LIU MINGLIANG, ZHU HONGYAN, CAI CHUANJUN, LIU YONGSHENG, SUN XIUWEN, LI YE, HAO GANGYONG
Format: Patent
Sprache:chi ; eng
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Beschreibung
Zusammenfassung:The invention relates to an energy absorption structure. The energy absorption structure is particularly used for a tail skid and a tail section of a helicopter deform together to absorb tail skid landing collision energy. The energy absorption structure is used for collision energy absorption of a helicopter empennage duct and is provided with a side wall and a bottom wall; the side wall and thebottom wall are laminated boards; each laminated board is provided with at least three layers, and the end of the side wall is provided with a flange which is used for being fixedly connected with a lower structure of the duct. The structure solves the technical problems that an existing installation structure is provided with a tail skid connector, a support, a reinforcing element and other partsand is complex in structure, heavy, difficult to install and maintain and high in production cost. 本发明涉及种吸能结构,特别用于直升机尾橇和尾段共同变形吸收尾橇着陆撞击能量,该吸能结构用于直升机尾翼涵道的碰撞吸能,该吸能结构具有侧壁和底壁;所述的侧壁和底壁均为层压板;层压板至少3层;侧壁的端部具有翻边,所述的翻边用于与涵道下部结构固定连接。解决了现