Invention Application
- Patent Title: CONTROLLING A COMPRESSOR OF A GAS TURBINE ENGINE
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Application No.: US15070268Application Date: 2016-03-15
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Publication No.: US20170268520A1Publication Date: 2017-09-21
- Inventor: Curtis William Moeckel , Andrew Breeze-Stringfellow , Peter John Wood , Eric Andrew Falk
- Applicant: General Electric Company
- Main IPC: F04D27/00
- IPC: F04D27/00 ; F02C9/20 ; F04D29/56 ; F02C9/18

Abstract:
An apparatus and method of controlling a multi-stage compressor of a gas turbine engine having a front-block of stages with variable stator vanes (VSVs), a rear block of stages downstream of the front-block, and a bleed air off-take from at least one of the stages. The method includes sensing the pressure of the bleed air from the bleed air off-take and adjusting the position of the VSV for the front-block.
Public/Granted literature
- US10408217B2 Controlling a compressor of a gas turbine engine Public/Granted day:2019-09-10
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