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  • Chapter 5: Flight Instruments › Gyroscopic Systems › Pneumatic Systems

    obtained by evacuating the instrument case with a vacuum source and allowing filtered air to flow into the case through a nozzle to spin the wheel. Venturi Tube Systems Aircraft that do not have a pneumatic pump to evacuate ... instruments through filters built into the instrument cases. In this system, ice can clog the venturi tube and stop the instruments when they are most needed. Figure 5-27. A venturi tube system that provides necessary vacuum to operate…

  • Chapter 5: Flight Instruments › Gyroscopic Systems › Electrical Systems

    instrument failure. Direct current (D.C.) electrical instruments are available in 14- or 28-volt models, depending upon the electrical system in the aircraft. A.C. is used to operate some attitude gyros and autopilots. Aircraft with only D.C. electrical systems ... instruments via installation of a solid-state D.C. to A.C. inverter, which changes 14 or 28 volts D.C. into three-phase 115-volt, 400-Hz A.C. Figure 5-28. Single-engine instrument vacuum system using a steel-vane, wet-type…

  • Chapter 5: Flight Instruments › Gyroscopic Systems › Vacuum Pump Systems

    Steel vanes sliding in a steel housing need to be lubricated, but…