#F01D11/14

OPEN ROTOR GAS TURBINE ENGINE WITH ADAPTIVE TURBINE CLEARANCE CONTROL SYSTEM AND METHOD

A gas turbine engine (20) disposed within a nacelle (40) is provided that includes an open rotor propulsion system (28), compressor (30), combustion (32), and turbine (34) sections, a lubrication syst…

DRIVE·Jun 10·1 min read

F01D11/14 RTX CORP [US]

SYSTEM AND METHOD FOR INSPECTING FAN BLADE TIP CLEARANCE RELATIVE TO AN ABRADABLE FAN CASE

A system (100) and method for inspecting fan blade clearances in a fan casing (210) are presented. The method includes manually installing a bracket (230) that includes a laser module (235) and an inc…

DRIVE·Apr 8·1 min read

F01D11/14 GEN ELECTRIC [US]

Gas turbine with compressor casing protected against cooling and Method to operate a gas turbine

The gas turbine comprises a turbine and a compressor with a compressor casing (14), whereby the compressor for the cooling of the turbine has a tapping line(16) for the bleed of compressed or partiall…

DRIVE·Aug 24·1 min read

F01D11/14 SIEMENS AG [DE]