Variant missile wing for air ship cruise missile and air ship cruise missile with variant missile wing

The invention provides a variant missile wing for an air-ship cruise missile, and belongs to the technical field of aircraft structure design, the variant missile wing comprises a missile wing framework, the missile wing framework comprises short rods and long rods, the middle parts of the two long...

Ausführliche Beschreibung

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Bibliographische Detailangaben
Hauptverfasser: SHANG LIYING, YANG CHENG, WANG RUNQING, XU SHENGMING, REN JIANGTAO, ZHANG CHAO, MING YALI
Format: Patent
Sprache:chi ; eng
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Beschreibung
Zusammenfassung:The invention provides a variant missile wing for an air-ship cruise missile, and belongs to the technical field of aircraft structure design, the variant missile wing comprises a missile wing framework, the missile wing framework comprises short rods and long rods, the middle parts of the two long rods are hinged to form a left wing main unit, the middle parts of the two long rods are hinged to form a right wing main unit, and the left wing main unit is connected with the right wing main unit; the left wing main unit and the right wing main unit are hinged to each other and are arranged on an air ship cruise missile body, the short rods are hinged to the left wing main unit, the two short rods are hinged to form a left wingtip hinge point, the short rods are hinged to the right wing main unit, and the two short rods are hinged to form a right wingtip hinge point. The missile wing skin is laid on the missile wing framework and used for providing lift force; and the auxiliary pull ropes are connected with the