Patent ID: 6400283
Filing Date: 2002-06-04
Classification: G01C,G01D

Abstract:
An altitude and vertical speed indicator for aircraft, the indicator comprising:first and second sensors for measuring an altitude and a vertical speed of the aircraft, respectively, and for supplying signals representing the altitude and the vertical speed; processing means for processing the signals supplied by said first and second sensors to produce processed signals; and display means, comprising a display screen, for displaying on the display screen an altitude indication and a vertical speed indication representing the processed signals, the display means comprising: altitude indication means for displaying on the display screen the altitude indication; and vertical speed indication means, in line with said altitude indication means, for displaying on the display screen the vertical speed indication; said altitude indication means and said vertical speed indication means being coupled such that the vertical speed indication is at all times in line with a future altitude indication which represents a future altitude corresponding to the vertical speed; wherein: said altitude indicator means comprises a graduated scale mobile past a fixed marker; said vertical speed indicator means comprises a pointer rotatable about a point of intersection of a straight line segment through said fixed marker and a straight line segment through said pointer and pointing towards said mobile graduated scale, an angle defined by said fixed marker and said pointer being representative of the vertical speed; and said display means further comprises means for displaying an artificial horizon and an altimeter on the display screen, the pointer being disposed between the artificial horizon and the altimeter and pointing towards the altimeter.