FUEL DELIVERY
Number of patents in Portfolio can not be more than 2000
United States of America
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N/A
Issued Date -
Feb 20, 2025
app pub date -
Nov 4, 2024
filing date -
Nov 4, 2024
priority date (Note) -
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status (Latency Note)
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Abstract
A gas turbine engine for an aircraft includes a staged combustion system having pilot fuel injectors and main fuel injectors. The gas turbine engine further includes a fuel delivery regulator arranged to control delivery of fuel to the pilot and main fuel injectors, and a fuel characteristic determination module configured to determine one or more fuel characteristics of the fuel being supplied to the staged combustion system. A controller is configured to determine a staging point defining the point at which the staged combustion system is switched between pilot-only operation and pilot-and-main operation, the staging point being determined based on the determined one or more fuel characteristics, the controller being configured to control the staged combustion system according to the determined staging point.
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