Helicopter rear horizontal tail wing structure with supporting rods

The invention provides a helicopter rear horizontal tail wing structure with supporting rods. The horizontal tail wing structure comprises a flat tail wing main body structure 1, two side end plates 2, supporting rod assemblies 3, first supporting rod joint assemblies 4, a second supporting rod join...

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Bibliographic Details
Main Authors LIU MINGLIANG, MEN KUNFA, ZHANG HUAN, LIU YONGSHENG, GAO RUIRUI, HAO GANGYONG
Format Patent
LanguageChinese
English
Published 14.02.2020
Subjects
AEROPLANES
AIRCRAFT
AVIATION
COSMONAUTICS
HELICOPTERS
PERFORMING OPERATIONS
TRANSPORTING
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Summary:The invention provides a helicopter rear horizontal tail wing structure with supporting rods. The horizontal tail wing structure comprises a flat tail wing main body structure 1, two side end plates 2, supporting rod assemblies 3, first supporting rod joint assemblies 4, a second supporting rod joint assembly 7 and supporting rod joint fairings 5, and the two side end plates 2 are two ends of theflat tail wing main body structure 1 respectively; the second supporting rod joint assembly 7 is riveted with the flat tail wing main body structure 1, and the first supporting rod joint assemblies 4are fixedly connected with a vertical tail wing rear beam of a helicopter; the second supporting rod joint assembly 7 is positioned at the pressure center position of the flat tail wing main body structure 1; one end of each supporting rod assembly 3 is connected with the second supporting rod joint assembly 7, and the other end of each supporting rod assembly 3 is connected with the correspondingfirst supporting rod joint
Bibliography:Application Number: CN201910971039