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The design of electrical, mechanical and fluid systems on aircraft is becoming increasingly integrated with the aircraft structure definition process. An example is the aircraft fuel quantity indication (FQI) system, of which the design is strongly dependent on the tank geometry definition.
Specifically, the approach accurately captures the gas-liquid interfaces inside 3D tanks with accounting of sloshing (surface angle variations) due to gravity and aircraft acceleration.
1 sty 2007 · In this project design methodologies for aircraft fuel system s are studied, with the aim of shortening the system development time. This is done by means of illustrative examples of how ...
The fuel flow control amongst tanks during the flight is addressed. A fuzzy management system is implemented that decides the best fuel distribution based on safety criteria (keeping...
ceptual design of aircraft fuel systems. The methods introduce automation early in the development process and increase understanding of how top requirements regarding the aircraft level impact low-level engineering parameters such as pipe diameter, pump size, etc. The morphological matrix and the house of quality matrix are quantified, which
19 gru 2023 · Based on the current form and the configuration of the existing aircraft fuel system, this text carried out structural design, through bold innovation and practice, designing a new aircraft fuel system pressure stabilization device, and its performance analysis. The theoretical basis is feasible and the prospect is broad.
4.2 Engine and APU Feed 59 4.2.1 Feed Tank and Engine Location Effects 59 4.2.2 Feed Pumping Systems 60 4.2.3 Feed Tank Scavenging 65 4.2.4 Negative g Considerations 65 4.2.5 Crossfeed 66 4.2.6 Integrated Feed System Solution 67 4.2.7 Feed System Design Practices 69 4.3 Fuel Transfer 70 4.3.1 Fuel Burn Scheduling 70 4.3.2 Wing Load Alleviation ...
