Novel civil aviation navigation system

The invention discloses a novel civil aviation navigation system. The system comprises a navigator and an inserting and fixing rod fixedly arranged in the middle of the end face of the rear side of the navigator, an inserting and fixing cavity is arranged in the end face of the front side of an oper...

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Bibliographic Details
Main Author WU MINJUN
Format Patent
LanguageChinese
English
Published 13.04.2018
Subjects
AIRCRAFT
ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT
AVIATION
COSMONAUTICS
EQUIPMENT FOR FITTING IN OR TO AIRCRAFT
FLYING SUITS
PARACHUTES
PERFORMING OPERATIONS
TRANSPORTING
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Summary:The invention discloses a novel civil aviation navigation system. The system comprises a navigator and an inserting and fixing rod fixedly arranged in the middle of the end face of the rear side of the navigator, an inserting and fixing cavity is arranged in the end face of the front side of an operation platform, a conductive groove is formed in the rear side of the inserting and fixing cavity ina hollow through manner, a conductive block is fixedly arranged on the rear side wall of the conductive groove, a first cavity is arranged on the rear side of the conductive groove, locking and fixing cavities which are communicated with each other are symmetrically arranged on the left and right sides of the inserting and fixing cavity, locking and fixing sliding grooves are arranged on the rearsides of the locking and fixing cavities in a hollow through manner, the locking and fixing sliding grooves are communicated with the first cavity in a hollow through manner, a first power converteris arranged in the operatio
Bibliography:Application Number: CN2018155998