RECONFIGURABLE TRANSPONDER
The technology of this application is generally directed to a method for temporary installation of a third military transponder while maintaining an existing dual civil transponder architecture. In one example embodiment, coax relays are installed between one of the civil transponders, the corresponding antennas, and the military transponder. A switch is installed to drive the coax relays and determine which transponder (e.g., civil or military) is connected to the antennas. The circuit breaker of the transponder not being used at the time can be pulled and collared to remove power to the equipment, and a software configuration loader card is used to configure the avionics.
1 . An aircraft, comprising:
avionics circuitry;
a first transponder;
a second transponder;
a third transponder;
a first relay;
a second relay;
a first antenna;
a second antenna; and
a switch, wherein
the first and second relay are configured for installation between the first transponder, the second transponder, and the third transponder, and the first and second antennas,
the switch is configured to enable the aircraft to operate in a first mode or a second mode,
in the first mode, the switch is configured to drive the first and second relays and connect the first and second transponders to the first and second antennas, and
in the second mode, the switch is configured to drive the first and second relays and connect the second and third transponders to the first and second antennas.
2 . The aircraft of claim 1 , wherein
the first transponder comprises a first civil transponder; and
the second transponder comprises a second civil transponder.
3 . The aircraft of claim 2 , wherein the third transponder comprises a military transponder.
4 . The aircraft of claim 1 , wherein the first relay and the second relay include coaxial relays.
5 . The aircraft of claim 1 , further comprising:
a first circuit breaker associated with the first transponder;
a second circuit breaker associated with the second transponder; and
a third circuit breaker associated with the third transponder, wherein
in the first mode, the third circuit breaker is set to disable power to the third transponder, and
in the second mode, the first circuit breaker or the second circuit breaker is set to disable power to the first transponder or the second transponder.
6 . The aircraft of claim 1 , wherein
a loader card enables flight software to operate in association with the first mode or the second mode, and
the loader card enables the flight software to operate in a civil mode, or operate in the civil mode and a military mode.
7 . The aircraft of claim 1 , further comprising a jumper harness enabling the aircraft to operate in a civil mode, or operate in the civil mode and a military mode.
8 . A system, comprising:
a first transponder;
a second transponder;
a third transponder;
a first relay;
a second relay;
a first antenna;
a second antenna; and
a switch, wherein
the switch is configured to enable the system to operate in a first mode or a second mode,
in the first mode, the switch is configured to drive the first and second relays and connect the first and second transponders to the first and second antennas, and
in the second mode, the switch is configured to drive the first and second relays and connect the second and third transponders to the first and second antennas.
9 . The system of claim 8 , wherein the first and second relay are configured for installation between the first transponder, the second transponder, and the third transponder, and the first and second antennas.
10 . The system of claim 8 , wherein
the first transponder comprises a first civil transponder; and
the second transponder comprises a second civil transponder.
11 . The system of claim 10 , wherein the third transponder comprises a military transponder.
12 . The system of claim 8 , wherein the first relay and the second relay include coaxial relays.
13 . The system of claim 8 , further comprising:
a first circuit breaker associated with the first transponder;
a second circuit breaker associated with the second transponder; and
a third circuit breaker associated with the third transponder, wherein
in the first mode, the third circuit breaker is set to disable power to the third transponder, and
in the second mode, the first circuit breaker or the second circuit breaker is set to disable power to the first transponder or the second transponder.
14 . The system of claim 8 , wherein a loader card enables flight software to operate in association with the first mode or the second mode.
15 . A transponder arrangement, comprising:
a first transponder;
a second transponder;
a third transponder;
a first relay;
a second relay; and
a switch, wherein
the switch is configured to enable an aircraft to operate in a first mode or a second mode,
in the first mode, the switch is configured to drive the first and second relays and connect the first and second transponders to first and second antennas, and
in the second mode, the switch is configured to drive the first and second relays and connect the second and third transponders to the first and second antennas.
16 . The transponder arrangement of claim 15 , wherein the first and second relay are configured for installation between the first transponder, the second transponder, and the third transponder, and the first and second antennas.
17 . The transponder arrangement of claim 15 , wherein
the first transponder comprises a first civil transponder;
the second transponder comprises a second civil transponder; and
the third transponder comprises a military transponder.
18 . The transponder arrangement of claim 15 , wherein the first relay and the second relay include coaxial relays.
19 . The transponder arrangement of claim 15 , wherein
the first transponder is associated with a first circuit breaker;
the second transponder is associated with a second circuit breaker; and
the third transponder is associated with a third circuit breaker, wherein
in the first mode, the third circuit breaker is set to disable power to the third transponder, and
in the second mode, the first circuit breaker or the second circuit breaker is set to disable power to the first transponder or the second transponder.
20 . The transponder arrangement of claim 15 , wherein a loader card enables flight software to operate in a civil mode, or operate in the civil mode and a military mode.