Fuel manifold for turbine

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United States of America Patent

PATENT NO 8573245
SERIAL NO

13282705

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ATTORNEY / AGENT: (SPONSORED)

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Abstract

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A fuel manifold for turbine engines, such as the large turbines used for generating electrical power, has a housing with straight internal porting for routing fuel and purge media streams to the combustion area of the turbine. A pressure balanced fuel valve regulates fuel using a poppet actuator. A piston section of the actuator dynamically seals off actuation pressure from the fuel. A valve section of the actuator dynamically seals off a vented area from the fuel and regulates fuel flow through the valve. The piston section has internal porting to a collector tube within the vented area for directing media leaked past the piston seal(s) to a vent port, and thereby prevent mixing of the fuel and actuation media.

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Patent Owner(s)

Patent OwnerAddress
JANSEN'S AIRCRAFT SYSTEMS CONTROLS INC2303 WEST ALAMEDA DRIVE TEMPE AS 85282

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Inventor(s)

Inventor Name Address # of filed Patents Total Citations
Jansen, Harvey B Mesa, US 38 463

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