Equilibrating flow distributor
AssigneeJansen's Aircraft Systems Controls, Inc.
InventorsJerame James Powell, Harvey B. Jansen
Life of this patent
Estimating the term…
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AssigneeJansen's Aircraft Systems Controls, Inc.
InventorsJerame James Powell, Harvey B. Jansen
Estimating the term…
An equilibrating flow distributor for a gas turbine engine includes a balancing valve and multiple flow dividers, each with a movable valve or divider member. The balancing valve has an inlet receiving media at a first pressure area and an outlet defining a plurality of first metering orifices. The valve member defines at least one second metering orifice receiving the media at a second pressure area. Each flow divider has an inlet receiving the media through an associated one of the first metering orifices at a third pressure area and an outlet defining one of a plurality of third metering orifices receiving the media at a fourth pressure area. Each flow divider has a second pressure area in communication with second pressure area of the balancing valve. Flow through the fourth pressure area of each flow divider is substantially the same.
An equilibrating flow distributor for a gas turbine engine, comprising:
An equilibrating flow distributor for a gas turbine engine, comprising:
An equilibrating flow distributor for a gas turbine engine, comprising:
Dependencies are inferred from the claim text.