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25 kwi 2017 · Schematic diagram of the F-15 Eagle. This image was uploaded in the JPEG format even though it consists of non-photographic data. This information could be stored more efficiently or accurately in the PNG or SVG format.
gas generator fuel flow (WFGG), augmentor core and duct fuel flow (WF), segment sequence valve position, and exhaust nozzle position (AJ). Dual sensors and position transducers are used as shown to achieve redundancy in key parameters as indicated by the (2).
The F-15 control system is powered by three separate hydraulic systems: Power Control One (PC-1) driven by the left engine. Power Control Two (PC-2) driven by the right engine, and a Utility system which contains two pumps, one on each engine.
The initial F100-PW-100 variant generates nearly 24,000 lbf (107 kN) of thrust in full afterburner and weighs approximately 3,000 lb (1,361 kg), achieving its target thrust-to-weight ratio of 8 and providing the F-15 with its desired thrust-to-weight ratio of greater than 1:1 at combat weight.
HYDRAULIC PUMP For ease of maintenance, the F-15 pump was designed as a plug-in type. The intake, outlet, and case drain fluid flows are directed to the spline-drive end of the pump where they pass through quick disconnect couplings.
The JetLegend F-15 is a well-proven plane that goes together very quickly and is very easy to fly. It has a very scale like appearance in the air, and with larger engines, can provide performance to satisfy just about any pilot. With smaller engines, it is a perfect, strong, stable introduction to turbine model jet flying.
Please view our partial parts list for the F-15 or contact us for a complete list of parts and component capabilities with F-15 fuel systems, hydraulics, actuators, landing gear, wheels, brakes, avionics, instruments, and more surplus parts and categories.
