Status display system
First Claim
1. A status display system for aircraft for receiving signals from sensors/transducers monitoring a plurality of parameters and subsystems of said aircraft and for providing a display to identify faulty ones of the parameters or subsystems in a prioritized sequence;
- comprising;
a signal data converter (SDC) having input means for receiving said signals and output means; and
means for presenting indications of said faulty parameters and subsystems, said means for presenting having input means and output means;
said SDC output means being connected to said means for presenting input means;
said SDC comprising;
means for processing said signals to determine which parameters and subsystems are faulty and for determining the priority of faulty ones thereof; and
means for transmitting information to said means for presenting relating to said faulty parameters and subsystems and to the priorities thereof;
whereby, said means for presenting provides indications to identify the faulty parameters and subsystems in the prioritized sequence;
wherein said visual display means comprises at least upper and lower lines for presenting text; and
further including means for displaying the highest priority one of said faulty ones of said parameters on said upper line, and means for scrolling at least some of the remainder of said faulty ones of said parameters in order of priority on at least said lower line.
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Accused Products
Abstract
The invention relates to a status display system for aircraft which system receives signals from sensors/transducers monitoring a plurality of parameters and subsystems of the aircraft. The system then displays text identifying faulty ones of the parameters or subsystems in a prioritized sequence. With the system of the invention, only a single indicator is needed to identify a plurality of faults as compared to available systems wherein each parameter and subsystem is monitored by a separate device including a separate display. Thus, the present invention is an improvement over the prior art in that: (1) it requires less cockpit space for displaying faults, and; it presents faults in order of priority so that the pilot does not have to make decisions about the most important fault to attend to when, as in the prior art systems, faced with a plurality of fault indications on a plurality of fault indicators.
73 Citations
19 Claims
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1. A status display system for aircraft for receiving signals from sensors/transducers monitoring a plurality of parameters and subsystems of said aircraft and for providing a display to identify faulty ones of the parameters or subsystems in a prioritized sequence;
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comprising; a signal data converter (SDC) having input means for receiving said signals and output means; and means for presenting indications of said faulty parameters and subsystems, said means for presenting having input means and output means; said SDC output means being connected to said means for presenting input means; said SDC comprising; means for processing said signals to determine which parameters and subsystems are faulty and for determining the priority of faulty ones thereof; and means for transmitting information to said means for presenting relating to said faulty parameters and subsystems and to the priorities thereof; whereby, said means for presenting provides indications to identify the faulty parameters and subsystems in the prioritized sequence; wherein said visual display means comprises at least upper and lower lines for presenting text; and further including means for displaying the highest priority one of said faulty ones of said parameters on said upper line, and means for scrolling at least some of the remainder of said faulty ones of said parameters in order of priority on at least said lower line. - View Dependent Claims (2, 3, 4, 5, 6, 7, 8, 9, 10, 11, 12, 13, 14, 15, 16, 17, 18, 19)
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Specification