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Self test avionics equipment
   
Document Number
US Patent 4970510
Issued Date
November 13, 1990
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Abstract
A self test avionics equipment is provided for use on an aircraft as part of a traffic collision avoidance system. The equipment has a radio frequency (RF) section and an integral test system. The RF section has an input/output unit, a transmitter and a receiver. The input/output unit has a local oscillator with a directional coupler, a two-way divider connected to the coupler, and an attenuator connected through a modulator to the coupler. The mixer and two-way divider each have an output coupling connector. The attenuator has an output pin switch connector. The transmitter has a modulator/amplifier portion, a spectrum filter connected to the modulator/amplifier portion, and a harmonic filter connected to the spectral filter. The harmonic filter has an ouput coupling connector. The test system comprises three dirctional coupler circuits and a pin switch circuit. The three directional coupler circuits are respectively coupled to the three output coupling connectors, respectively from the mixer, the two-way divider and the harmonic filter. A pin switch circuit connects to the pin switch connector.
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Self test avionics equipment - US Patent 4970510 Drawing
Drawing from US Patent 4970510
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Number of Claims:
4
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Owner
Honeywell Inc. (Minneapolis, MN)
Published
November 13, 1990
Application Number
07/453,731
Filed
December 20, 1989
US Classification
340/945   340/514 455/67.11 455/73 701/31
Int'l Classification
G08G   5/04   (20060101)   G08G   5/00   (20060101)   H04B   17/00   (20060101)  
Assistant Examiner
Attorney/Law Firm
USPTO Field of Search
340/945   340/961   340/514   364/424.03   364/424.06   455/67   455/226  
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Description
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