Gault05 Posted November 9, 2017 Posted November 9, 2017 Does changing the fuel switches on the f15 impact how it uses its fuel in-flight? Even if it has fuel tanks on board? Trying to get a better understanding of how its supposed to work is all. Case:NZXT S340 Mid Tower;Motherboard:MSi B550 Pro Series ATX;CPU:AMD Ryzen 5 5600 6-core with Wraith Stealth Cooler;Memory:Gigastone 64GB;Hard Drive:Barracuda 2TB Hard Drive; Sound:Asus Xonar DGX; Power:Corsair RMe 750w PSU; GPU: MSI GeForce Ventus 12GB w/OC Modules: Flaming Cliffs 2024, P-51D, Combined Arms, Black Shark 3, A-10C/2, WW2 Assets, F/A-18C, F-16C Viper, AH-64D, Supercarrier, China Assets Pack, Maps: Persian Gulf, Syria, Marianas, Sinai
Baz000 Posted November 10, 2017 Posted November 10, 2017 I think it just changes your fuel quantity indicator but not how the fuel is used
mvsgas Posted November 10, 2017 Posted November 10, 2017 (edited) Does changing the fuel switches on the f15 impact how it uses its fuel in-flight? Even if it has fuel tanks on board? Trying to get a better understanding of how its supposed to work is all. No, It only affects the Fuel quantity gauge. For more info on how it work on the E model, look here: http://www.f-15e.info/joomla/en/technology/fuel-system/93-fuel-quantity-indicator I will post if I find info on the C version. Fuel System The F-15C/D is equipped with an automatic system (fig. 10-1) that gauges and transfers fuel without crew input. It provides pressurized fuel to the engines under normal conditions, and gravity feeds fuel for limited engine operation during electrical or hydraulic system failure. The system is comprised of internal, external, and conformal fuel tanks, gauging units, pumps and plumbing [ATTACH]171911[/ATTACH] The fuel distribution (transfer) system uses three electric impeller type pumps; one in each internal wing tanks, and one in fuselage tank no. 1. Each auxiliary fuselage tank is equipped with an injector pump operated by transfer pump pressure. The system automatically transfers fuel from all tanks to fuselage tank no. 2 which feeds the right engine, and to tanks 3A and 3B which feed the left engine. The conformal tanks contain two electric impeller type fuel transfer pumps which transfer fuel to internal tanks. External tanks are pressurized by regulated engine bleed air during flight and transfer fuel to internal tanks. Fuel is transferred first from external tanks to any tank that will receive fuel, and normally external wing tanks transfer to the centerline tank, then to fuselage tank no.1. The fuel indicating system (fig. 10-3) shows total fuel aboard the aircraft in pounds. The fuel quantity indicator shows fuel aboard on the INTERNAL scale, and total fuel (internal, external, and conformal tanks) in the TOTAL LBS window. The fuel low level warning system senses low fuel quantity and lights the fuel low warning light on the Caution Lights Display Panel. A manual bingo setting on the fuel quantity indicator can be used to set a predetermined fuel level that will automatically stop fuel dumping and illuminate the BINGO FUEL light on the Caution Lights Display Panel. Fuel is stored in eight internal tanks (fig. 10-2); one in each wing and six in the center fuselage. Internal fuel capacity is 2,070 gallons. An additional 1500 gallons can be stored in conformal fuel tanks installed at the wing/fuselage intersection, and an additional 1800 gallons can be stored in inboard wing and centerline external tanks when installed. Internal and conformal tanks contain foam blocks to prevent explosion or fire, and all internal tanks are self-sealing. Tanks 2 and 3A are specially designed with a horizontal baffle that traps fuel for inverted flight. [ATTACH]171912[/ATTACH] Edited November 10, 2017 by mvsgas To whom it may concern, I am an idiot, unfortunately for the world, I have a internet connection and a fondness for beer....apologies for that. Thank you for you patience. Many people don't want the truth, they want constant reassurance that whatever misconception/fallacies they believe in are true..
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