Maintenance computer system for an aircraft
First Claim
1. A maintenance computer system for an aircraft, including a network that is partitioned into a secured avionics zone and an open zone, the system comprising:
- a first computer hosting a first software module, said first computer being accommodated in the avionics zone; and
a second computer hosting a second software module, said second computer being accommodated in the open zone, and linked to the first computer via a unidirectional link going from the avionics zone to the open zone;
the first software module configured to follow a fault-finding logic tree, and the second software module configured to present an electronic maintenance document and to automatically and synchronously generate a presentation of pages of the electronic maintenance document associated respectively with nodes of the tree when the first module follows a path along the fault-finding tree.
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Accused Products
Abstract
A maintenance computer system for an aircraft, including a network partitioned into a secured avionics zone and an open zone. The system includes a first software module accommodated in the avionics zone and a second software module accommodated in the open zone, the first module configured to follow a fault-finding logic tree, and the second module configured to present an electronic maintenance document, with the path along the fault-finding logic tree followed by the first module automatically and synchronously generating a presentation by the second module of pages of the maintenance document associated respectively with nodes of the tree.
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Citations
9 Claims
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1. A maintenance computer system for an aircraft, including a network that is partitioned into a secured avionics zone and an open zone, the system comprising:
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a first computer hosting a first software module, said first computer being accommodated in the avionics zone; and a second computer hosting a second software module, said second computer being accommodated in the open zone, and linked to the first computer via a unidirectional link going from the avionics zone to the open zone; the first software module configured to follow a fault-finding logic tree, and the second software module configured to present an electronic maintenance document and to automatically and synchronously generate a presentation of pages of the electronic maintenance document associated respectively with nodes of the tree when the first module follows a path along the fault-finding tree. - View Dependent Claims (2, 3, 4, 5, 6, 7, 8, 9)
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Specification