Aircraft rotor motor support

The invention relates to the technical field of aircrafts, in particular to an aircraft rotor motor bracket, comprising: an assembly cavity comprising a bottom wall and a side wall on one side, the assembly cavity being used for sleeving an aircraft rotor support arm; a through hole is formed in the...

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Bibliographic Details
Main Author DENG YUNDI
Format Patent
LanguageChinese
English
Published 10.06.2022
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Summary:The invention relates to the technical field of aircrafts, in particular to an aircraft rotor motor bracket, comprising: an assembly cavity comprising a bottom wall and a side wall on one side, the assembly cavity being used for sleeving an aircraft rotor support arm; a through hole is formed in the bottom wall of the assembly cavity; the motor mounting surface intersects with the bottom wall of the assembly cavity and is connected with the bottom wall of the assembly cavity, and a motor mounting position is preset on the motor mounting surface; the electronic speed controller mounting surface is intersected and connected with the bottom wall of the assembling cavity, and an electronic speed controller mounting position is preset on the electronic speed controller mounting surface; and the motor mounting surface and the electronic speed controller mounting surface are oppositely arranged and are positioned on two sides of the through hole. The device is ingenious in design and novel in structure, can provide
Bibliography:Application Number: CN202210360770