Hybrid ACARS communication system
View Patent ↗The invention concerns a communication system via ACARS messages intended to be placed onboard an aircraft, said system comprising a router ( 310, 310′ ) adapted to route said messages from and to a plurality of VHF, HF, SATCOM sub-networks. The system comprises a switch ( 360, 365 ) and an AoIP conversion gateway ( 380 ), the switch being connected to an HF or SATCOM transceiver module ( 340, 350 ) by means of a first two-way link ( 341, 351 ), and to said AoIP gateway by means of a second two-way link ( 381 ), the switch being adapted to select said first two-way link when it lies in a first switch position and the second two-way link when it lies in a second switch position, the switch lying in the second switch position if the aircraft is on the ground or less than a predetermined distance from the ground, otherwise it lies in the first position.
1. A communication system via ACARS messages intended to be placed onboard an aircraft, said system comprising a router adapted to route said messages from and to a plurality of VHF, HF, SATCOM sub-networks, wherein the communication system comprises a switch and an AoIP conversion gateway, the switch being connected to an HF or SATCOM transceiver module by means of a first two-way link, and to said AoIP gateway by means of a second two-way link, the switch being adapted to select said first two-way link when it lies in a first switch position, and the second two-way link when it lies in a second switch position, the switch being in the second switch position if the aircraft is on the ground or less than a predetermined distance from the ground, otherwise it lies in the first switch position.
2. The communication system according to claim 1 , further comprising a sensor adapted to determine whether the weight of the aircraft is on its wheels.
3. The communication system according to claim 1 , further comprising a sensor adapted to detect whether the door of the aircraft is open or closed.
4. The communication system according to claim 1 , further comprising a sensor adapted to measure the distance of the aircraft from the ground and of comparing this distance with said predetermined value.
5. The communication system according to claim 1 , further comprising a sensor adapted to determine whether the aircraft engines are or are not switched off.
6. The communication system according to claim 1 , wherein the first and second two-way links each consist of a pair of unidirectional buses conforming to standard ARINC 429 and of opposite directions.
7. The communication system according to claim 1 , wherein the switch is connected to said router by means of a third two-way link, the third link being connected to the first link if the switch lies in the first switch position and to the second link if it lies in the second switch position.
8. The communication system according to claim 1 , wherein the switch is integrated in said router, the first two-way link being connected to a first input/output interface and the second two-way link being connected to a second input/output interface of said router, the switch selecting the first interface when it lies in the first switch position and selecting the second interface when it lies in the second switch position.
9. The communication system according to claim 8 , wherein said transceiver module and said conversion gateway are connected to the sensor and configured as master/slave, said gateway declaring itself as master and said transceiver module as slave to said router, if the sensor detects that the aircraft is on the ground or less than a predetermined distance from the ground, and said transceiver module declaring itself as master and said gateway as slave to said router in the opposite case.
10. An aircraft equipped with a a communication system via ACARS messages intended to be placed onboard an aircraft, said system comprising a router adapted to route said messages from and to a plurality of VHF, HF, SATCOM sub-networks, wherein the communication system comprises a switch and an AoIP conversion gateway, the switch being connected to an HF or SATCOM transceiver module by means of a first two-way link, and to said AoIP gateway by means of a second two-way link, the switch being adapted to select said first two-way link when it lies in a first switch position, and the second two-way link when it lies in a second switch position, the switch being in the second switch position if the aircraft is on the ground or less than a predetermined distance from the ground, otherwise it lies in the first switch position.