By A. L. Bolsunovsky
Plane layout four (2001) 193–219
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Extra info for Flying wing - problems and decisions
Indicator. /min. and at the same time it rotates a smaller pointer against the inner scale indicating thousands of revelmin. 3 High-range long- scale displays. ( U ) Concentric scales; ( b ) fined and rotating scdes; (c) common scale, triple pointers; (d) split pointer. 3 (b), we find a method which is empioyed in a certain type of airspeed indicator; in its basic concept it is similar to the one just described. In this design, however, a single pointer rotates against a circular scale and drives a second scale instead of a pointer.
Engine No. G. T. M. 89 90 88 90 3 4 is from bottom to top or from left to right. In the field of aircraft instruments there are very few applications of the straight scale and pointer displays, as they are not suitable for the monitoring of the majority of quantities to be measured. However, they do possess characteristics which can contribute to the saving of panel space and improved observational accuracy, particularly where the problems of grouping and monitoring a large number of engine instruments is concerned.
As will be noted, it combines a gyro horizon directive display, and thereby eliminates the need for a pilot having to monitor the indications of two separate instruments. 1 1 (c). Thus, the pilot is directed t o 'fly the aircraft up' in order t o intercept the beam. Similarly, if the aircraft is to the right of the localizer beam the localizer pointer will be deflected t o the left thus directing the pilot to 'fly the aircraft left'. As the pilot responds to the instrument's directives the pointers move back to their centre positions indicating that the aircraft is in the correct approach position for landing.
Flying wing - problems and decisions by A. L. Bolsunovsky