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Aviation History
1962
1962 - 2023.PDF
36 FLIGHT International, 13 September 1962 ENGINE immmmtm and VIBRATION MONITORS Give immediate warning of incipient defects. Used for pre-flight checks, continu ous in-flight monitoring and routine maintenance. Highest order of reliability. ENGINE VIBRATION INDICATOR * The Engine Vibration Indicator has appli cation where vibration information only is required. Vibration levels are indicated on meters, excessive vibration operating a warning lamp which remains alight until reset. Amplifier containing up to 4 channels is contained in J ATR case. ^ ENGINE CONDITION ANALYSER Specified for B.O.A.C. De Havilland Comet4 fleet The Engine Condition Analyser provides a CRT display of temperature and vibration, using solid state high speed switching, in a form that can be assessed at a glance or measured accurately by the calibration arrangements provided. Temperature indications from thermocouples are displayed on the upper CRT against a base line representing datum temperature. Datums are pro vided for Take-off, Climb, Cruise and Descent. The amplitude of vibration is shown by taking levels from up to 8 transducers and displaying them, on the lower CRT. Amplifier/scanner unit may be mounted in any suitable place in the aircraft. The indicating meters, warning lamps and reset buttons can be supplied separately, as, for example, for the De Havilland Trident. ULTRA ULTRA ELECTRONICS LIMITED CONTROL AND INSTRUMENTATION GROUP WESTERN AVENUE • LONDLN • W3 • Telephone ACOrn 3434 CONTROL AND INSTRUMENTATION • COMMUNICATIONS -AUTOMATIC BUSINESS EQUIPME
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