Avionics calculator with integrated routing module, related communication network and communication installation, and aircraft comprising such a communication installation
First Claim
1. An avionic calculator, intended to be loaded on board an aircraft, the avionic calculator comprising:
- a protective casing andat least one module from among an information processing module able to execute at least one software application, an input/output management module and a power supply management module, each module being positioned inside the casing,wherein the avionic calculator further comprises;
a routing module positioned inside the casing, the routing module including several communication ports and being configured for transmitting at least one message from an input communication port to an output communication port, anda data transceiver module positioned inside the casing, the transceiver module being configured so as to be connected to at least one of the modules belonging to the group comprising;
the routing module positioned inside the casing,another routing module, external to the avionic calculator.
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Accused Products
Abstract
This avionic calculator, intended to be loaded on board an aircraft, the avionic calculator includes a protective casing and at least one module from among an information processing module able to execute at least one software application, an input/output management module and an electric power supply management module, each module being positioned inside the casing. The avionic calculator further includes a routing module positioned inside the casing, the routing module including several communication ports and being configured for transmitting at least one message from an input communication port to an output communication port.
11 Citations
20 Claims
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1. An avionic calculator, intended to be loaded on board an aircraft, the avionic calculator comprising:
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a protective casing and at least one module from among an information processing module able to execute at least one software application, an input/output management module and a power supply management module, each module being positioned inside the casing, wherein the avionic calculator further comprises; a routing module positioned inside the casing, the routing module including several communication ports and being configured for transmitting at least one message from an input communication port to an output communication port, and a data transceiver module positioned inside the casing, the transceiver module being configured so as to be connected to at least one of the modules belonging to the group comprising; the routing module positioned inside the casing, another routing module, external to the avionic calculator. - View Dependent Claims (2, 3, 4, 5, 6, 7, 8, 9, 10, 11, 12, 13, 14, 15, 16, 17, 18, 19, 20)
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Specification