초록 ▼

A redundancy monitor is presented which makes operational checks on the electronic overspeed control system used on aircraft turbine engines. The monitor is a small and lightweight device that can be permanently installed on the engine. Its function is to monitor both the speed pickups that count th

A redundancy monitor is presented which makes operational checks on the electronic overspeed control system used on aircraft turbine engines. The monitor is a small and lightweight device that can be permanently installed on the engine. Its function is to monitor both the speed pickups that count the revolutions per minute that the turbine shaft is turning and at the same time maintain a check on the performance of the circuitry which processes the data. The monitor includes a latching type BITE indicator which signifies redundant status of the speed pickups and a lamp which lights to indicate any failure in the output circuitry of the overspeed sensor system. A momentary-on type switch activates self test circuitry within the redundancy monitor.

대표청구항 ▼

In an overspeed control system for a gas turbine engine including: a power source; a speed sensing circuit consisting of at least two sensors operatively connected to the gas turbine engine to redundantly generate first signals proportional to the operational speed of said gas turbine engine; gating

In an overspeed control system for a gas turbine engine including: a power source; a speed sensing circuit consisting of at least two sensors operatively connected to the gas turbine engine to redundantly generate first signals proportional to the operational speed of said gas turbine engine; gating means connected to receive the first speed signals and transmit a second speed proportional thereto only if all of said redundant signals are present; means to generate a signal indicative of a predetermined overspeed condition; dual comparison circuits, each connected to receive the first speed signals and the predetermined overspeed condition signal, said dual comparison means connected in series to generate an overspeed signal when comparisons, by each of said circuits, of said predetermined signal to at least one of said first speed signals is each indicative of an engine overspeed condition, said dual comparison circuits generating internal signals indicative of proper operation of each of said circuits; and actuating means responsive to the overspeed signal to shut off the fuel supply to the gas turbine engine; a monitor for checking the proper functioning of the overspeed control system during normal operation of the gas turbine engine comprising: first means connected to the overspeed control system to receive the second speed signal and generate a first monitor signal in response thereto; speed sensing circuit indicating means connected to receive the first monitor signal and to provide a visual indication of the proper functioning of the speed sensing circuits; second means connected to the overspeed control system to receive the internal signals of the dual comparison circuits to generate a second monitor signal in response thereto; comparison circuit indicating means connected to receive the second monitor signal and to provide a visual indication of the proper functioning of the dual comparison circuits; and self test circuitry connected to actuate the first and second monitor signal generating means independent of the overspeed control system to check the proper functioning of the monitor.