Aviation bus differential crystal oscillator test system
An aviation bus and test system technology, applied in the direction of measuring electricity, measuring devices, measuring electrical variables, etc., can solve problems such as inability to check electrical components, imperfect testing, and inability to fully guarantee the normal communication of aviation bus devices.
Patent Information
- Authority / Receiving Office
- CN · China
- Patent Type
- Applications(China)
- Current Assignee / Owner
- Publication Date
- 2021-09-07
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Abstract
Description
Technical field
[0001] The present invention relates to the field of aeronautical technology communications bus, in particular to a differential oscillator avionics bus test system. Background technique
[0002] As an important part of aviation bus avionics system, the communication between the various avionics subsystems to ensure flight safety has important significance. Differential oscillator as an aviation bus important components of the normal communication system plays an important role.
[0003] In recent years, the gradual emergence of a differential oscillator in our line of sight, as well as a growing number of electronic engineers would prefer differential oscillator, with the advantages of the development of information technology, a differential crystal high-performance, low-power, low-noise, making it many design suitable solution.
[0004] However, due to harsh natural environment experienced aircraft in flight which, from low to high, have Quartz "thermal hystere...
Examples
Embodiment Construction
[0023] Next, the technical solutions in the embodiments of the present invention will be apparent from the embodiment of the present invention, and it is clearly described, and it is understood that the described embodiments are merely embodiments of the present invention, not all of the embodiments. Based on the embodiments of the present invention, there are all other embodiments obtained without making creative labor without making creative labor premises.
[0024] See Figure 1-2 The present invention provides a technical solution:
[0025] One kind of a differential oscillator avionics bus test system includes a power supply and an oscilloscope 9, further comprising a FPGA chip 5 and 10, inside incubator 10 is provided with a thermostat mounting station 3 crystal, crystal mounting station 3 and 4 by ZDB differential collecting probe 8 is connected to the oscilloscope. 9 fit, FPGA chip 5 is electrically connected to a zero delay buffer. 4, FPGA chip 5 is electrically connected ...