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- Politecnico di Milano
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- Aerospace Engineering
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- Impianti e Sistemi Aerospaziali
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Lab 4 v3 impianto combustibile relazione
Study material for Impianti e Sistemi Aerospaziali, shared by the Studwiz community and reviewed by moderators.
Impianti e Sistemi AerospazialiOther
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POLITECNICO DI MILANO Facoltà di Ingegneria Dipartimento di Scienze e Tecnologie Aerospaziali Corso di Impianti e Sistemi Aerospaziali LABORATORIO n. 4 FUEL SYSTEM: CROSSFEED TRANI ROBERTO matricola 958130 cod. persona 10711328 Academic Year 2021-2022 [2] Abstract The case study of this report is the fuel system of a twin-engine aicraft. It consists in two pumps, two reservoirs, two distribution lines connected to each other by a crossfeed valve. The purpose is to analyze the scheme of a given system and choose the pump capable of satisfyng the demands of the motor s both in case of normal operation and in the event of a fault in one of the two pumps. [3] Index 1 List of symbols ........................................................................................................................................... 1 2 Problem analysis ........................................................................................................................................ 2 2.1 Problem description .......................................................................................................................... 2 2.2 Method of resolution ........................................................................................................................ 3 2.2.1 Pressure losses .......................................................................................................................... 3 2.2.2 Operating range ......................................................................................................................... 3 2.2.3 Choice method .......................................................................................................................... 3 2.3 Problem data…
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