Awesome explanation, thanks! But I wonder why Engine #2 is started with the help of Engine #1. I know it may be technical difficult but in case of some emergency (Engine #1 fails) we cannot start Engine #2 anymore. Why is there no backup from the APU possible for both engines?
I think you are wrong. It works according to Bernoulli's principle that states that in fluid dynamics an increase in the speed of fluid occurs simultaneously with a decrease in pressure or decrease in the fluid's potential energy1 This is what creates the lift for the plane!
Huh. I always figured there was a starter motor similar to a car to spin up the main engines. I had no idea the APU used waste gas to spin up the mains. That’s really cool. So there are fluid lines from the APU to each main engine? How big are they?
I’m an airline captain…and this is a pretty cool video… However, starting the 2nd engine with air from the first is NOT a normal procedure… With normal APU operation, both engines are started in the same manner… Cross-bleeding works fine(using air from the 1st to start the 2nd), but it’s not the norm….
Starter shutt off valve is the valve that opens when pilot selects "start" to allow the APU air to hit the air turbine starter motor mounted at around 6 PM position on each engine. Starter shutt of valve is a butterfly type valve mounted in the air ducting between APU and the air turbibe starter, it is electrically controlled. Air turbine starters are high speed low torque units, however a built in reduction gear system converts this high speed low torque to low speed high torque which is capable of rotating engine through a gearbox, also mounted on the engine. Leave me a note if some one is interested to learn more. Any topic, airplane related.