COMPLEX ELECTRONIC DISPLAY SYSTEM FOR LIGHT MULTI- PURPOSE AIRCRAFT

FIELD: aircraft instrumentation engineering. SUBSTANCE: proposed system includes multi-functional color displays, collimator indicator on windshield and multi-functional control console connected with on-board digital computer by means of multiplex and reserve radial information exchange channels. O...

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Bibliographische Detailangaben
Hauptverfasser:	DEMCHENKO O.F, NIKITIN V.N, SOROKIN V.F, SUSLOV V.D, POPOVICH K.F, EFANOV A.G, PERMINOV A.G, SHKOLIN V.P, TASKAEV R.P
Format:	Patent
Sprache:	eng
Schlagworte:	AIRCRAFT ARRANGEMENTS FOR MEASURING TWO OR MORE VARIABLES NOT COVEREDIN A SINGLE OTHER SUBCLASS ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT AVIATION CALCULATING COMPUTING COSMONAUTICS COUNTING ELECTRIC DIGITAL DATA PROCESSING EQUIPMENT FOR FITTING IN OR TO AIRCRAFT FLYING SUITS MEASURING MEASURING NOT SPECIALLY ADAPTED FOR A SPECIFIC VARIABLE MEASURING OR TESTING NOT OTHERWISE PROVIDED FOR PARACHUTES PERFORMING OPERATIONS PHYSICS TARIFF METERING APPARATUS TESTING TRANSPORTING
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Beschreibung
Zusammenfassung:	FIELD: aircraft instrumentation engineering. SUBSTANCE: proposed system includes multi-functional color displays, collimator indicator on windshield and multi-functional control console connected with on-board digital computer by means of multiplex and reserve radial information exchange channels. On-board digital computer is also connected with mode parameter sensors. Multifunctional color displays (no less than three displays) are fully interchangeable; they provide pilot with complete pilotage navigational information in case of failure of one of them and minimum scope of information in case of failure of two of them. EFFECT: enhanced operational reliability. 3 cl, 2 dwg