Appeal No. 2000-0230 Application No. 08/761,671 Independent claim 1 is reproduced as follows: 1. 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 2Page: Previous 1 2 3 4 5 6 7 NextLast modified: November 3, 2007