AM.III.K.S5
SkillInspect a turbine engine air intake anti-ice system.
From the FAA library
- Chapter 4: Helicopter Components, Sections, and Systems › Environmental Systems
disadvantage of this type of system is that power is required to compress the air or gas for the cooling function, thus robbing the engine of some of its capability. Some systems are restricted from use during takeoff and landings ... Piston-powered helicopters use a heat exchanger shroud around the exhaust manifold to provide cabin heat. Outside air is piped to the shroud and the hot exhaust manifold heats the air, which is then blown into the cockpit. This warm…
- Chapter 3. ICING EFFECTS, PROTECTION, AND DETECTION › 3-5. ANTI-ICING SYSTEMS › a. Bleed Air Systems
Bleed Air Systems. Bleed air systems are used for larger areas of the aircraft, such as engine nacelles and wing leading edges. Bleed air from turbine engines is the most common type of anti-icing protection for engine nacelles ... wings of transport and business turbojets. Hot air is distributed to piccolo tubes, which consist of a perforated pipe installed directly behind the airplane’s skin. Such hot air systems are quite effective in preventing the formation of ice. NOTE…
- Chapter 6: Lubrication & Cooling Systems › Turbine Engine Lubrication Systems
Turbine Engine Lubrication Systems Both wet- and dry-sump lubrication systems are used in gas turbine engines. Wet-sump engines store the lubricating oil in the engine proper, while dry-sump engines utilize an external tank mounted on the engine ... somewhere in the aircraft structure near the engine, similar to reciprocating piston engines mentioned earlier. Turbine engine’s oil systems can also be classified as a pressure relief system that maintains a somewhat constant pressure: the full flow type…