Fuel System; General Description; Gas Fuel System Components; Off-Skid Block And Vent Valve - Siemens SGT-400 Operator's Manual

Turbine package
Table of Contents

Advertisement

Fuel System

The fuel system is designed to deliver fuel to the combustion system at the correct pressure and
flow required for the applicable power demand.

General Description

The schematic diagrams of the Fuel System can be found in this Manual Volume.
The fuel system comprises:
Off-skid Components
block and vent valve assembly (XV30, XV31)
demister (if applicable)
filter/coalescer (if applicable)
On-skid components
gas fuel supply strainer (XF94)
two block valves (XV6, XV7)
vent valve (XV212)
main fuel control valve/actuator assembly (XV150, XM26)
pilot fuel control valve/actuator assembly (XV149, XM27)
electronic control unit
system monitoring and control instrumentation
pipeline trace heating (if applicable).

Gas Fuel System Components

Off-Skid Block and Vent Valve

The block and vent valve assembly is located in the customers gas supply line. The assembly
comprises of a block valve (XV30) and a vent valve (XV31). Both valves are controlled by
pneumatically operated rotary actuators. Air is directed to the actuators by solenoid valves
(SOL12 and SOL11) respectively. When the situation demands, the block valve closes to prevent
gas entering the on-skid fuel system and the vent valve opens to vent the interconnecting
pipework.
The block valve is spring loaded to fail in the 'closed' position. The vent valve is spring loaded to
fail in the 'open' position.
Turbine Package Operators Manual
Turbine Package System Overview
1-15
Chapter 1

Hide quick links:

Advertisement

Table of Contents
loading

Table of Contents