Civil aviation navigation device

A navigation device and civil aviation technology, applied in the electronic field, can solve the problems of reducing the service life of the receiver, troublesome installation and disassembly, etc., and achieve the effect of reducing the probability of damage without affecting the aesthetics

Inactive Publication Date: 2019-02-05
陈 宇翔
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0002] Civil aviation refers to the use of various types of aircraft to engage in all aviation activities other than military nature (including national defense, police and customs). It is called civil aviation. The basic requirement of civil aviation is safety and reliability, and navigation is an indispensable accessory in aviation. One, the civil aviation navigation device is divided into a single air navigation system, a hand-held air navigation

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  • Civil aviation navigation device
  • Civil aviation navigation device

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[0015] All the features disclosed in this specification, or all disclosed methods or steps in the process, except for mutually exclusive features and / or steps, can be combined in any manner.

[0016] Any feature disclosed in this specification, unless specifically stated, can be replaced by other equivalent or equivalent alternative features. That is, unless otherwise stated, each feature is just one example of a series of equivalent or similar features.

[0017] Such as Figure 1-2 As shown, a civil aviation navigation device of the device of the present invention includes a mounting cavity 11 arranged in an aircraft body 10 and an opening facing upward, and a receiver 35 that cooperates with the mounting cavity 11 and is used to receive signals. The device 35 is provided with a first sliding groove communicating with left and right, a first sliding block 36 is slidably installed in the first sliding groove, and a first connecting groove 42 is provided in the left end surface of ...

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Abstract

The invention discloses a civil aviation navigation device. The device includes an installation cavity arranged in an aircraft body and with an upward opening, and a receiver matching the installationcavity and used for receiving signals; the receiver is provided with a first sliding groove in left-right communication; a first sliding block is slidingly installed in the first sliding groove; theleft end face of the first sliding block is provided with first connecting grooves; first conducting strips electrically connected to electronic components inside the receiver are fixedly installed onthe inner wall of the first connecting grooves; the right end face of the receiver is provided with second connecting grooves; second conducting strips electrically connected to a receiving module inside the receiver are fixedly installed on the inner wall of the second connecting grooves; the top wall of the installation cavity is provided with a third connecting groove with an upward opening; athird conducting strip electrically connected to a storage battery is fixedly installed on the inner wall of the third connecting groove; and the left end wall of the installation cavity is providedwith a fourth connecting groove with an opening facing to right and matching the first sliding block.

Description

technical field [0001] The invention relates to the electronic field, in particular to a civil aviation navigation device. Background technique [0002] Civil aviation refers to the use of various types of aircraft to engage in all aviation activities other than military nature (including national defense, police and customs). It is called civil aviation. The basic requirement of civil aviation is safety and reliability, and navigation is an indispensable accessory in aviation. One, the civil aviation navigation device is divided into a single air navigation system, a hand-held air navigation system and an auxiliary air navigation system, and the airborne receiver is one of the essential components in the navigation system. Automatic monitoring of ground-based navigation operation status, while traditional airborne receivers are generally fixedly installed in the aircraft body, and are often removed during maintenance. The installation and disassembly are very troublesome, a...

Claims

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Application Information

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IPC IPC(8): H01R13/629H01R13/70H01R13/703H01R13/71H01Q1/08H01Q1/28B64D47/00
CPCH01R13/629B64D47/00H01Q1/084H01Q1/285H01R13/701H01R13/7036H01R13/71H01R2201/26
Inventor 陈宇翔
Owner 陈 宇翔
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