Douglas W Guetter, Age 621426 N Omaha Cir, Mesa, AZ 85205

Douglas Guetter Phones & Addresses

1426 N Omaha Cir, Mesa, AZ 85205

Pinetop, AZ

4457 Allesandro Ct, Gilbert, AZ 85233

653 San Angelo St, Gilbert, AZ 85233

Sacramento, CA

Rancho Cordova, CA

Chandler, AZ

Maricopa, AZ

Santa Maria, CA

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Mentions for Douglas W Guetter

Publications & IP owners

Us Patents

System Having Termination For Data Loading Port

US Patent:
7564371, Jul 21, 2009
Filed:
Aug 28, 2006
Appl. No.:
11/511631
Inventors:
Cyro Allen Stone - Peoria AZ, US
Douglas W. Guetter - Gilbert AZ, US
Desi D. Stelling - Glendale AZ, US
Assignee:
Aviation Communication & Surveillance Systems - Phoenix AZ
International Classification:
G08B 21/00
US Classification:
340945
Abstract:
A subsystem of an avionics system is operated in a first mode for receiving software via a port; and in a second mode in accordance with a circuit that includes a terminator coupled to the port. By using the terminator to convey information regarding a desired configuration for operation in the second mode, communication and wiring is avoided between subsystems of the avionics system for conveying such information. In one implementation, operation in the second mode includes performing a collision avoidance function (e. g. , providing a TCAS advisory). Configuration information in accordance with the circuit may specify an arrangement of shared antennas between multiple transponders and/or mode changes related to using an antenna for a collision avoidance function in a hijack mode of operation.

System Having Termination For Data Loading Port

US Patent:
2004006, Apr 1, 2004
Filed:
Sep 30, 2002
Appl. No.:
10/260241
Inventors:
Cyro Stone - Peoria AZ, US
Douglas Guetter - Gilbert AZ, US
Desi Stelling - Glendale AZ, US
International Classification:
H02B001/056
US Classification:
439/043000, 361/600000, 700/017000
Abstract:
A subsystem of an avionics system is operated in a first mode for receiving software via a port; and in a second mode in accordance with a circuit that includes a terminator coupled to the port. By using the terminator to convey information regarding a desired configuration for operation in the second mode, communication and wiring is avoided between subsystems of the avionics system for conveying such information. In one implementation, operation in the second mode includes performing a collision avoidance function (e.g., providing a TCAS advisory). Configuration information in accordance with the circuit may specify an arrangement of shared antennas between multiple transponders and/or mode changes related to using an antenna for a collision avoidance function in a hijack mode of operation.

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