Rudder body structure of aircraft
The utility model relates to a rudder body structure of an aircraft, which comprises a left rudder body and a right rudder body, an annular external connecting sleeve is arranged at the port of the left rudder body, an annular internal connecting sleeve is arranged at the port of the right rudder bo...
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| Format: | Patent |
| Sprache: | chi ; eng |
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| Zusammenfassung: | The utility model relates to a rudder body structure of an aircraft, which comprises a left rudder body and a right rudder body, an annular external connecting sleeve is arranged at the port of the left rudder body, an annular internal connecting sleeve is arranged at the port of the right rudder body, when the left rudder body and the right rudder body are spliced, the annular external connecting sleeve and the annular internal connecting sleeve are meshed with each other, the left rudder body and the right rudder body are convenient to disassemble and assemble, and the structure is simple. The installation of internal electronic components is convenient; besides, the interiors of the left rudder body and the right rudder body are hollow, a plurality of mounting plates are arranged in the left rudder body and the right rudder body, mounting openings are formed in the middles of the mounting plates, electronic component mounting cavities are formed between the adjacent mounting plates in the left rudder body |
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